TW201005175A - Engine, partition member, and production method of the partition member - Google Patents
Engine, partition member, and production method of the partition member Download PDFInfo
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- TW201005175A TW201005175A TW98115746A TW98115746A TW201005175A TW 201005175 A TW201005175 A TW 201005175A TW 98115746 A TW98115746 A TW 98115746A TW 98115746 A TW98115746 A TW 98115746A TW 201005175 A TW201005175 A TW 201005175A
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- 238000005192 partition Methods 0.000 title claims abstract description 27
- 238000004519 manufacturing process Methods 0.000 title claims description 10
- 239000000446 fuel Substances 0.000 claims abstract description 110
- 238000004891 communication Methods 0.000 claims abstract description 71
- 238000002347 injection Methods 0.000 claims abstract description 49
- 239000007924 injection Substances 0.000 claims abstract description 49
- 238000007789 sealing Methods 0.000 claims abstract description 29
- 238000002485 combustion reaction Methods 0.000 claims abstract description 17
- 239000011347 resin Substances 0.000 claims description 26
- 229920005989 resin Polymers 0.000 claims description 26
- 238000009413 insulation Methods 0.000 claims description 8
- 239000007921 spray Substances 0.000 claims description 8
- 239000004734 Polyphenylene sulfide Substances 0.000 claims description 6
- 229920000069 polyphenylene sulfide Polymers 0.000 claims description 6
- 238000000638 solvent extraction Methods 0.000 claims description 4
- 239000005011 phenolic resin Substances 0.000 claims description 3
- 239000000057 synthetic resin Substances 0.000 claims description 3
- 229920003002 synthetic resin Polymers 0.000 claims description 3
- 230000013011 mating Effects 0.000 claims 2
- 238000005507 spraying Methods 0.000 claims 1
- 238000004544 sputter deposition Methods 0.000 claims 1
- 238000000889 atomisation Methods 0.000 abstract description 16
- 230000002093 peripheral effect Effects 0.000 description 27
- 238000001816 cooling Methods 0.000 description 10
- 239000000463 material Substances 0.000 description 9
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 8
- 239000002184 metal Substances 0.000 description 7
- 230000000694 effects Effects 0.000 description 6
- 239000003502 gasoline Substances 0.000 description 5
- 238000011144 upstream manufacturing Methods 0.000 description 5
- 230000009467 reduction Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 230000003111 delayed effect Effects 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 150000002221 fluorine Chemical class 0.000 description 2
- 229910052731 fluorine Inorganic materials 0.000 description 2
- 239000011737 fluorine Substances 0.000 description 2
- 239000003292 glue Substances 0.000 description 2
- 238000001746 injection moulding Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000004904 shortening Methods 0.000 description 2
- 239000000725 suspension Substances 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 238000001721 transfer moulding Methods 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 235000009854 Cucurbita moschata Nutrition 0.000 description 1
- 240000001980 Cucurbita pepo Species 0.000 description 1
- 235000009852 Cucurbita pepo Nutrition 0.000 description 1
- 238000013019 agitation Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 238000000748 compression moulding Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000000498 cooling water Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 239000000806 elastomer Substances 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- -1 for example Substances 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 239000003595 mist Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 210000003516 pericardium Anatomy 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 239000012783 reinforcing fiber Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000000565 sealant Substances 0.000 description 1
- 235000020354 squash Nutrition 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- ANRHNWWPFJCPAZ-UHFFFAOYSA-M thionine Chemical compound [Cl-].C1=CC(N)=CC2=[S+]C3=CC(N)=CC=C3N=C21 ANRHNWWPFJCPAZ-UHFFFAOYSA-M 0.000 description 1
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- Fuel-Injection Apparatus (AREA)
Abstract
Description
201005175 六、發明說明: 【發明所屬之技術領域】 引擎之分隔構件 本發明係關於一種引擎及一種用於一 【先前技術】 匕知一種引擎,立中一嫩姐4 u '、,,,、’噴射户配置接近於一進氣閥201005175 VI. Description of the invention: [Technical field of the invention] Separator of the engine The present invention relates to an engine and an engine for use in a prior art, a middle-aged sister 4 u ',,,,, 'The injector configuration is close to an intake valve
開口且-輔助空氣供應口面向該燃料噴射器之一喷射口附 近。作為-揭示此種技術之文件,已知下文專利文件卜 一在該引擎中’該燃料噴射器經由-轉接器附裝至一汽缸 ^另一方面’ 一節流本體提供於一進氣管中間,且兩個 節流閥分別以一可;&3 Β -Γ B日人, J打開及可閉合方式安裝於該節流本體 中。-打開於該兩個節流閥之間的旁路管之—端側連接至 該節流閥,且該旁路管之另一端開口至一形成於該轉接器 之尖端。[5刀之外周邊側處之流人室中。引人至該流入室之 辅助空氣經由-開口於該轉接器之該尖端部分處之連通孔 吹向該燃料噴射器之該噴射口附近。 [先前技術文件] [專利文件] [專利文件1]第WO2005/098231A1號國際公開申請案 【發明内容】 [本發明欲解決之問題] 同時’從一環境保護觀點出發,人們一直探尋改良燃料 霧化效率以減少引擎燃料消耗。就此而言,在先前技術 中’人們尚未渴望地考量影響燃料霧化效率之轉接器及其 周邊之細節。 14030I.doc 201005175 本發明係基於上述環境* 良燃料霧化效率之引擎。 1曰在梃供種能夠改 [解決該等問題之方法] 作為—種用於達成上述目的之 Λ 4士似+ * 發明引擎,其特徵 ° ,案1之本 盆田认 成妹私用包含如下之結構:-汽缸體, = : = ί含納:活塞一,其與該汽 Α ’",、燒至該,飞缸蓋具有一主通道之至少一 4以用於經由—進氣_ 口將進氣以至㈣燒室中; 喷射n,其安裝於該仏蓋上且具有—詩將燃料 =進氣閥開口噴射之噴射口;-室,該噴射π位於其 ’-旁路通道’其—端與該主通道之—中間部分連通且 端”該至連通’一分隔構件,其具有:一沿該燃料噴 、,之t射方向延伸以徑向分隔該室同時環繞該喷射口 =筒狀壁部分,-在該燃料噴射口附近形成於該筒狀壁部 分中之連通孔;及第一與第二密封部分#等用於在沿該 嘴射方向位於該連通孔之後方及前方之位置處於形成該室 之壁表面與該分隔構件之一外表面之間進行密封。 [本發明作用] 因此’本發明之引擎可改良燃料霧化效率。 【實施方式】 在下文中,將參照圖1至u來解釋本發明之實施例丨、2 及3。在實施例1、2及3中’作為本發明之一引擎之一個實 例,將例示一安裝於一摩托車上之引擎。對下文說明中所 使用之「前」、「後」、「左」及「右」之描述係基於自 140301 Joe -6 - 201005175 一坐在一摩托車之一車座上之騎乘者看去之方向而界定。 <實施例1> 圖1顯示一上面施加有一根據實施例i之引擎12〇之整個 摩托車100。首先,將解釋摩托車100之整個結構,且隨後 k 將詳細說明實施例1之引擎120。 1.摩托車之整個結構 如圖1中所示,摩托車1〇〇配備有一底骨型車底架(下文 中簡稱為「車底架」)110。車底架11〇係由以下構成:_ 參 頭管111、一脊骨部分112及一車座導執in,其等自前側 (圖1中之右側)朝後侧(圖之左侧)按此次序配置' 一轉向軸103以一可左右旋轉方式附裝至頭管u。一把 手103a連接至轉向軸103之上端。一以可旋轉方式支承— 前輪1〇1之前又102進一步連接至轉向轴1〇3。前又1〇2具有 一擋泥板106,該檔泥板具有一覆蓋自前輪1〇1之上部分至 其後部分之範圍的形狀。 脊骨部分112配置於摩托車100之軸線上,亦即,配置於 沿前後方向延伸之中心線上。脊骨部分112之前端側緊固 至頭管111,且其後側傾斜地向下、向後延伸。一空氣濾 清器140、-進氣管141及—引擎12()以—懸掛方式緊固至、 脊骨部分U2之下部分。因此,引擎12。大錢位於摩托車 100之軸距之中心部分處。 車座導軌113亦配置於摩托車100之轴線上亦即,配置 於沿前後方向延伸之令心線上。車座導軌113之前端側連 接至脊骨部分之後端部分,且其後端側傾斜地向後、 140301.doc 201005175 向上延伸。一車座114配置於車座導軌113上方。在座導軌 113之前端侧處’提供一向下延伸之後臂托架(未圖解闡 釋)。一用於以可旋轉方式支承一後輪104之後壁1〇5之一 前端側由該後臂托架以可擺動方式支承。一懸掛部分丨i 8 提供於車座導軌1丨3之後端側與後臂105之後端側之間以吸 收自後臂105傳輸至車底架11〇之振動。 車底架110具有一具有從上方完全覆蓋車底架11〇之形狀 之車身罩115及一具有一從頭管1丨丨之前面覆蓋空氣濾清器 140及引擎120之右側及左側之形狀之前罩115a。 2.引擎結構 在實施例1中,為簡化說明,例示並解釋一四沖積單汽 虹引擎。然而’本發明之引擎不僅限於該結構。此外,本 發明可適用於氣冷型引擎及水冷型引擎兩者,且因此將進 行以下說明而不將冷卻類型限制至其中任何一者。 如圖1中所示’引擎120具有一汽缸體122、--體緊固 至汽缸體122之前側之汽缸蓋121及--體緊固至汽缸體 i22之後端側之曲軸箱123。 如圖2中所示,汽缸體122具有一形成於其中之汽缸膛 122a。作為汽缸膛122a之一中心轴線之汽缸轴線a設定為 沿前後方向大致水平。在汽缸膛122a中,一活塞124以可 滑動方式插入。 引擎120之冷卻類型可係一氣冷類型或一水冷類型。在 其中引擎120之冷卻類型係一氣冷類型之情況下,複數個 自汽缸體122之外周邊表面向外凸出之散熱片(未圖解闡釋) 140301.doc 201005175 提供至汽缸體122。另一方面,在其中引擎丨2〇之冷卻類型 係一水冷類型之情況下,一經形成以環繞汽缸膛丨22a且構 成為致使冷卻水在其中循環之水套(未圖解閣釋)提供至汽 缸體122。引擎120構成為由該等散熱片或該水套冷卻從而 . 防止過度溫升。 、 曲軸箱123(參見圖1)裝設在結構上係習知之一曲轴(未圖 解闡釋)及一傳動裝置(未圖解闡釋)。如圖2中所示,活塞 124藉由一連桿125連接至曲轴(未圖解闡釋活塞124在汽 © 虹膛122a中之往復移動致使曲軸經由連桿125之旋轉移 動。然後,驅動力經由該傳動裝置或一鏈條(未顯示)傳輸 至後輪104以旋轉後輪104。 在一其中一形成於後表面121a之側處之燃燒凹入部分 121b閉合汽缸膛122a之狀態下,汽缸蓋121緊固至汽缸體 122之前側。燃燒凹入部分121b、汽缸膛122a及活塞124形 成一燃燒室C。 汽缸蓋121具有一經由一進氣閥開口 128與一燃燒室C連 籲 通之進氣口 131及一經由排氣閥開口 127與燃燒室C連通之 排氣口 129。一汽缸蓋罩I21d附裝至汽缸蓋121之前表面。 • 在形成於汽缸蓋121之正面與汽缸蓋罩121d之間的空間 „ 中,配置一排氣搖臂134、一進氣搖臂135、一凸輪133a等 等。 進氣口 131形成為一自汽缸蓋121中之燃燒凹入部分12lb 向上彎曲之形狀,或一自進氣閥開口 128沿一大致垂直於 汽缸軸線A之方向(大致垂直方向)彎曲且向上延伸至汽缸 140301.doc -9- 201005175 蓋121之頂面之形狀。 進氣口 131構成用於經由進氣閥開口 128將進氣引入至燃 燒室C之主通道之一部分。進氣口 131具有一開口於汽缸蓋 121之上表面處之外部連接開口 131a。一與進氣口 131—起 構成主通道之一部分之筒狀節流本體160連接至此外部連 接開口 13 1 a。 在節流本體160中,提供一位於靠近進氣口 13 1之側處之 第一節流閥161及一位於遠離進氣口 131之側處之第二節流 閥162。下文所提及之旁路通道180之一上游端開口 180b(譯者注:正確地180a)與位於第一與第二節流閥161與 162之間的進氣口 131之内壁表面連通。 第一及第二節流閥161及162由相應搖臂轴161a及162a以 可搖擺方式支承。儘管稍後將進行詳細說明,但第一及第 二節流閥161及162藉由根據騎乘者之節流操作以可搖擺方 式來回移動相應搖臂轴161 a及162a來改變開度。因此,調 節自節流本體160流至進氣口 131之進氣之流動速率及欲自 上游端開口 180b(譯者注:正確地18〇a)經由旁路通道18〇引 入至室174中之輔助空氣之流動速率。 如圖1中所示,構成主通道之其餘部分之進氣管141連接 至節流本體160之上部分》進氣管141沿脊骨部分ιΐ2之下 表面傾斜地向前向上延伸並連接至空氣濾清器14〇。 如圖2中所示,在汽缸蓋121之汽缸軸線A上方,具有一 進氣閥132。進氣閥132具有:__閥頭ma,其用於打開並 閉合進氣㈣口128;—閥桿⑽,其用於導引閥頭in 14030l.doc -10- 201005175 以實施沿一垂直於進氣閥開口 128之方向之前進及後退移 動;及一閥彈簧132d ’其用於沿一閉合進氣閥開口 128之 方向推動閥頭132a。閥桿132b相對於汽缸轴線A呈一規定 角度傾斜地向上傾斜。 另一方面,排氣口 129自排氣閥開口 127傾斜地向下延伸 至汽缸蓋121之底面。燃燒室C中之燃燒氣體自排氣閥開口 127經由排氣口 129引入至汽缸蓋121之底面側並隨後經由 例如在結構上係習知之一排氣管(未圖解闡釋)及一消音器 (未圖解解釋)向外排放。 在汽缸蓋121之汽缸軸線a下方,具有排氣閥13〇 ^排氣 閥130具有:一間頭13〇a,其用於打開並閉合排氣閥開口 127 ; 一閥桿130b,其用於導引閥頭130a以實施沿一垂直 於排氣閥開口 127之方向之前進及後退移動;及一閥彈簧 130d,其用於沿一閉合排氣閥開口 127之方向推動閥頭 130a。閥桿l30b相對於汽缸軸線a呈一規定角度傾斜地向 下傾斜。 在此實施例中,當引擎12〇自該側看去時,進氣闊及 排氣閥130配置於與作為__對稱轴之汽红轴線a大致線對稱 位置處在進氣閥132之闊彈菁132d與排氣間㈣之間彈 簧130d之間以可旋轉方式提供一凸輪軸133,其通常用 於進氣及排氣閥且具有凸輪133a。 在凸輪軸133與進 延氣閥132之間’配置有進氣搖臂135。 進氣搖臂135在其女m . 、大致中心位置處由進氣搖臂轴135a以可 旋轉方式支承至汽i 蓋121。在凸輪轴133與排氣閥13〇之 140301.doc -11- 201005175 間,配置有排氣搖臂134。排氣搖臂134在其大致中心位置 處由進氣搖臂轴134a以可旋轉方式支承至汽缸蓋12ι。 進氣搖臂135及排氣搖臂134中之每一者之一端部分與凸 輪133a接觸。與曲轴同步之凸輪軸U3之旋轉移動致使進 氣搖臂135及排氣搖臂134之另一端部分按相應預定時序下 推相應閥桿130b及132b,從而克服相應閥彈簧13〇(1及132(1 之推動力而移動閥頭13〇3及132&。因此,進氣閥132及排 氣閥130與活塞124之往復移動同步按預定時序打開並閉合 進氣閥開口 128及排氣閥開口 127。 3.對燃料噴射器之詳細說明The opening and the auxiliary air supply port face the vicinity of one of the fuel injectors. As a document revealing such a technique, it is known that the following patent document discloses that in the engine, the fuel injector is attached to a cylinder via an adapter, and the throttle body is provided in the middle of an intake pipe. And the two throttle valves are respectively installed in the throttle body in a can open and closable manner by a Japanese; J; - the end side of the bypass pipe opened between the two throttle valves is connected to the throttle valve, and the other end of the bypass pipe is open to a tip formed at the adapter. [5 knives outside the peripheral side of the flow room. Auxiliary air introduced into the inflow chamber is blown toward the vicinity of the injection port of the fuel injector via a communication hole opening at the tip end portion of the adapter. [Prior Art Document] [Patent Document] [Patent Document 1] International Publication No. WO2005/098231A1 [Summary of the Invention] [Problems to be Solved by the Invention] At the same time, from the viewpoint of environmental protection, people have been searching for improved fuel mist. Efficiency to reduce engine fuel consumption. In this regard, in the prior art, 'people have not eagerly considered the details of the adapter and its surroundings that affect the efficiency of fuel atomization. 14030I.doc 201005175 The present invention is based on the aforementioned environment* engine for good fuel atomization efficiency. 1曰 梃 梃 梃 能够 能够 [ [ [ [ 梃 梃 梃 梃 梃 梃 梃 作为 作为 Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ Λ The following structure: - cylinder block, = : = ί 纳: piston one, which is associated with the car '", burned to, the fly-cylinder cap has at least one 4 of a main passage for passing-intake _ mouth will be in the air into the (four) burning chamber; spray n, which is mounted on the lid and has the injection port of the fuel = inlet valve injection; - chamber, the injection π is located in its 'bypass channel 'the end portion communicates with the intermediate portion of the main passage and the end portion is connected to the 'dividing member' having a partition member extending along the fuel injection direction to radially partition the chamber while surrounding the injection port a cylindrical wall portion, a communication hole formed in the cylindrical wall portion in the vicinity of the fuel injection port; and first and second sealing portions # and the like for locating the communication hole in the nozzle direction The front position is sealed between the wall surface forming the chamber and the outer surface of one of the partition members [Effect of the Invention] Therefore, the engine of the present invention can improve fuel atomization efficiency. [Embodiment] Hereinafter, embodiments 丨, 2, and 3 of the present invention will be explained with reference to Figs. 1 to u. In Embodiments 1, 2 And 3 as an example of an engine of the present invention, an engine mounted on a motorcycle will be exemplified. Descriptions of "front", "back", "left" and "right" used in the following description. It is based on the direction of the rider who sits on one of the motorcycles of 140301 Joe -6 - 201005175. <Embodiment 1> Fig. 1 shows an entire motorcycle 100 to which an engine 12 according to Embodiment i is applied. First, the entire structure of the motorcycle 100 will be explained, and then the engine 120 of Embodiment 1 will be described in detail. 1. The entire structure of the motorcycle As shown in Fig. 1, the motorcycle 1 is equipped with a bottom-bottom vehicle undercarriage (hereinafter simply referred to as "undercarriage") 110. The undercarriage 11 is composed of the following: _ a head tube 111, a spine portion 112, and a seat guide in, which are pressed from the front side (the right side in FIG. 1) toward the rear side (the left side of the figure). Sequence Configuration 'A steering shaft 103 is attached to the head pipe u in a left-right rotation manner. A hand 103a is coupled to the upper end of the steering shaft 103. It is rotatably supported - before the front wheel 1〇1 is further connected to the steering shaft 1〇3. The front panel 1 has a fender 106 having a shape covering a range from a portion above the front wheel 1〇1 to a rear portion thereof. The spine portion 112 is disposed on the axis of the motorcycle 100, that is, disposed on a center line extending in the front-rear direction. The front end side of the spine portion 112 is fastened to the head pipe 111, and its rear side is inclined downwardly and rearwardly. An air cleaner 140, an intake pipe 141, and an engine 12 () are fastened to the lower portion of the spine portion U2 in a suspension manner. Therefore, the engine 12. Big money is located at the center of the wheelbase of the motorcycle 100. The seat rail 113 is also disposed on the axis of the motorcycle 100, that is, on the center line extending in the front-rear direction. The front end side of the seat rail 113 is connected to the rear end portion of the spine portion, and the rear end side thereof is obliquely extended rearward, 140301.doc 201005175. A seat 114 is disposed above the seat rail 113. At the front end side of the seat rail 113, a downwardly extending rear arm bracket (not illustrated) is provided. A front end side of the wall 1〇5 for rotatably supporting a rear wheel 104 is swingably supported by the rear arm bracket. A suspension portion 丨i 8 is provided between the rear end side of the seat rail 1丨3 and the rear end side of the rear arm 105 to absorb the vibration transmitted from the rear arm 105 to the undercarriage 11〇. The undercarriage 110 has a body cover 115 having a shape completely covering the undercarriage 11 from above, and a front cover having a shape of a right side and a left side of the air filter 140 and the engine 120 before the head pipe 1 is covered. 115a. 2. Engine Structure In Embodiment 1, a four-integrated single steam engine is illustrated and explained for simplicity of explanation. However, the engine of the present invention is not limited to this structure. Furthermore, the present invention is applicable to both air-cooled engines and water-cooled engines, and thus the following description will be made without limiting the cooling type to any one of them. As shown in Fig. 1, the engine 120 has a cylinder block 122, a cylinder head 121 that is fastened to the front side of the cylinder block 122, and a crankcase 123 that is fastened to the rear end side of the cylinder block i22. As shown in Fig. 2, the cylinder block 122 has a cylinder bore 122a formed therein. The cylinder axis a, which is a central axis of the cylinder bore 122a, is set to be substantially horizontal in the front-rear direction. In the cylinder bore 122a, a piston 124 is slidably inserted. The type of cooling of the engine 120 can be either an air-cooled type or a water-cooled type. In the case where the cooling type of the engine 120 is an air-cooled type, a plurality of fins (not illustrated) that protrude outward from the outer peripheral surface of the cylinder block 122 are provided to the cylinder block 122. On the other hand, in the case where the type of cooling of the engine is a water-cooling type, a water jacket (not illustrated) that is formed to surround the cylinder bore 22a and configured to cause cooling water to circulate therein is supplied to the cylinder. Body 122. The engine 120 is configured to be cooled by the fins or the water jacket to prevent excessive temperature rise. The crankcase 123 (see Fig. 1) is mounted on a structurally known crankshaft (not illustrated) and a transmission (not illustrated). As shown in Fig. 2, the piston 124 is coupled to the crankshaft by a link 125 (not illustrated to reciprocate movement of the piston 124 in the steam rainbow rainbow 122a to cause the crankshaft to move via rotation of the link 125. Then, the driving force is thereby A transmission or a chain (not shown) is transmitted to the rear wheel 104 to rotate the rear wheel 104. In a state in which the combustion concave portion 121b formed at the side of the rear surface 121a closes the cylinder bore 122a, the cylinder head 121 is tight It is fixed to the front side of the cylinder block 122. The combustion concave portion 121b, the cylinder bore 122a and the piston 124 form a combustion chamber C. The cylinder head 121 has an air inlet which is connected to a combustion chamber C via an intake valve opening 128. 131 and an exhaust port 129 communicating with the combustion chamber C via the exhaust valve opening 127. A cylinder head cover I21d is attached to the front surface of the cylinder head 121. • Between the front surface formed on the cylinder head 121 and the cylinder head cover 121d In the space „, an exhaust rocker arm 134, an intake rocker arm 135, a cam 133a, and the like are disposed. The air inlet 131 is formed in a shape that is bent upward from the combustion concave portion 12lb in the cylinder head 121, or One from the intake valve opening 128 A shape that is generally perpendicular to the direction of the cylinder axis A (substantially perpendicular) and extends upwardly to the shape of the top surface of the cylinder 140301.doc -9-201005175 cover 121. The air inlet 131 is configured to be advanced via the intake valve opening 128 The gas is introduced into a portion of the main passage of the combustion chamber C. The intake port 131 has an external connection opening 131a that opens at the upper surface of the cylinder head 121. A cylindrical section that forms part of the main passage together with the intake port 131 The flow body 160 is connected to the external connection opening 13 1 a. In the throttle body 160, a first throttle valve 161 located at a side close to the air inlet 13 1 and a side located away from the air inlet 131 are provided. The second throttle valve 162. One of the bypass passages 180 mentioned below has an upstream end opening 180b and an air inlet between the first and second throttle valves 161 and 162. The inner wall surfaces of the 131 are in communication. The first and second throttle valves 161 and 162 are swingably supported by the respective rocker shafts 161a and 162a. Although will be described in detail later, the first and second throttle valves 161 and 162 by operating according to the rider's throttling The swinging manner moves the corresponding rocker shafts 161a and 162a back and forth to change the opening degree. Therefore, the flow rate of the intake air flowing from the throttle body 160 to the intake port 131 is adjusted and the opening is intended to be from the upstream end 180b. The ground 18〇a) the flow rate of the auxiliary air introduced into the chamber 174 via the bypass passage 18. As shown in Fig. 1, the intake pipe 141 constituting the rest of the main passage is connected to the upper portion of the throttle body 160. The intake pipe 141 extends obliquely forward and upward along the lower surface of the spine portion ι 2 and is connected to the air cleaner 14A. As shown in Fig. 2, above the cylinder axis A of the cylinder head 121, there is an intake valve 132. The intake valve 132 has: a valve head ma for opening and closing the intake (four) port 128; a valve stem (10) for guiding the valve head in 14030l.doc -10- 201005175 to implement a vertical The direction of the intake valve opening 128 is advanced and retracted; and a valve spring 132d' is used to urge the valve head 132a in a direction to close the intake valve opening 128. The valve stem 132b is inclined obliquely upward at a predetermined angle with respect to the cylinder axis A. On the other hand, the exhaust port 129 extends obliquely downward from the exhaust valve opening 127 to the bottom surface of the cylinder head 121. The combustion gas in the combustion chamber C is introduced from the exhaust valve opening 127 to the bottom side of the cylinder head 121 via the exhaust port 129 and then via an exhaust pipe (not illustrated) and a muffler (for example) Unillustrated) discharged outward. Below the cylinder axis a of the cylinder head 121, there is an exhaust valve 13. The exhaust valve 130 has a head 13a for opening and closing the exhaust valve opening 127, and a valve stem 130b for The valve head 130a is guided to move forward and backward in a direction perpendicular to the exhaust valve opening 127; and a valve spring 130d is used to urge the valve head 130a in a direction to close the exhaust valve opening 127. The valve stem l30b is inclined obliquely downward at a predetermined angle with respect to the cylinder axis a. In this embodiment, when the engine 12 is viewed from the side, the intake air and exhaust valve 130 is disposed at the intake valve 132 at a substantially line symmetrical position with the steam red axis a as the symmetry axis. A cam shaft 133 is rotatably provided between the wide elastic cyanine 132d and the exhaust chamber (four) between the springs 130d, which is generally used for the intake and exhaust valves and has a cam 133a. An intake rocker arm 135 is disposed between the cam shaft 133 and the intake air valve 132. The intake rocker arm 135 is rotatably supported by the intake rocker shaft 135a to the steam i cover 121 at a substantially central position thereof. An exhaust rocker arm 134 is disposed between the camshaft 133 and the exhaust valve 13 140 140301.doc -11- 201005175. The exhaust rocker arm 134 is rotatably supported to the cylinder head 12i by the intake rocker shaft 134a at its substantially central position. One end portion of each of the intake rocker arm 135 and the exhaust rocker arm 134 is in contact with the cam 133a. The rotational movement of the cam shaft U3 synchronized with the crankshaft causes the other end portions of the intake rocker arm 135 and the exhaust rocker arm 134 to push down the corresponding valve stems 130b and 132b at respective predetermined timings, thereby overcoming the corresponding valve springs 13 (1 and 132). (1) The driving force moves the valve heads 13〇3 and 132&. Therefore, the intake valve 132 and the exhaust valve 130 open and close the intake valve opening 128 and the exhaust valve opening in synchronization with the reciprocating movement of the piston 124 at a predetermined timing. 127. 3. Detailed description of the fuel injector
如圖3及4中以一放大方式所示,在汽缸蓋121中之進氣 口 131與進氣閥132之間,形成有一含納部分137,其具有 開口於汽缸蓋121之外表面處之一端及開口於進氣口 ΐ3ι之 内壁表面處之另一端。含納部分137形成呈一具有一作為 一中心軸線之軸線S1之多階梯式大致錐形孔形狀,且開Z 於進氣口 131之内壁表 -_ «^ 孑目^ 開於/飞缸蓋121之外表面處之一端側漸縮。燃料喷身 170經由一與汽缸蓋121分開形成之轉接器1〇(一作為^ 明之一結構元件之分隔構件)附裝至含納部分Η?。在一 安裝於含納部分137中之狀態下,線轴S1與轉接器1(^ 心轴線重合。 燃料喷射器170具有As shown in an enlarged manner in FIGS. 3 and 4, an intake portion 137 having an opening at the outer surface of the cylinder head 121 is formed between the intake port 131 and the intake valve 132 in the cylinder head 121. One end and the other end open at the inner wall surface of the air inlet ΐ3ι. The containing portion 137 is formed in a multi-stepped substantially conical hole shape having an axis S1 as a central axis, and the Z is opened on the inner wall of the air inlet 131 - _ «^ ^目 ^ Open / fly cylinder cover One end side of the outer surface of 121 is tapered. The fuel injection body 170 is attached to the containing portion via an adapter 1 (which is a separate member of a structural member) formed separately from the cylinder head 121. In a state of being mounted in the containing portion 137, the bobbin S1 coincides with the adapter 1 (the engine axis is coincident. The fuel injector 170 has
本體17 2之一端側處; :一燃料喷射器本體172,其具有_ 噴射口 171,其形成於燃料噴射器 及一燃料供應軟管連接部分172a, 140301.doc -12· 201005175 其自燃料噴射器本體172之另一端側凸出。燃料噴射器i7〇 在結構上係習知的且因此將簡化說明。如圖3中所示,噴 射口 171經形成以在一其中該燃料喷射器經由轉接器附 裝至含納部分137之狀態下轴線S1成為中心軸線。沿軸線 S1向前推進之方向係燃料喷射器17〇之一嘴射方向。 軸線S1沿經過圓形排氣閥開口 128之中心或其附近之方 向定向。更特定而言,軸線S1設定呈適當位置及角度以使 自喷射口 17〗噴射之燃料與流過進氣口 131之進氣之燃料_ 空氣混合物致使空氣運動,例如燃燒室c中之滾動氣流。 此處,沿轴線81朝進氣閥開口 128推進之方向界定為2軸 線S1朝前方向前方(燃料喷射器17〇之喷射方向)且相反方 向界定為一軸線81方向後方(與燃料喷射器170之嘴射方向 相反之方向)。 如圖6及7中所示’轉接器1〇係一樹脂一體模製件,兑呈 有一凸緣19及—形成呈-多階梯式筒狀狀之筒狀壁部; 11。One end side of the body 17 2; a fuel injector body 172 having an injection port 171 formed in the fuel injector and a fuel supply hose connection portion 172a, 140301.doc -12· 201005175 The other end side of the body 172 is convex. The fuel injector i7 is conventionally known in construction and thus will be simplified. As shown in Fig. 3, the injection port 171 is formed to become a central axis in a state in which the fuel injector is attached to the containing portion 137 via the adapter. The direction in which the axis S1 advances is the direction in which the fuel injector 17 is in the nozzle direction. The axis S1 is oriented in a direction passing through the center of the circular exhaust valve opening 128 or in the vicinity thereof. More specifically, the axis S1 is set at an appropriate position and angle such that the fuel injected from the injection port 17 and the fuel-air mixture flowing through the intake port 131 cause the air to move, such as the rolling airflow in the combustion chamber c. . Here, the direction of advancement along the axis 81 toward the intake valve opening 128 is defined as the 2 axis S1 forward facing forward (injection direction of the fuel injector 17A) and the opposite direction defined as an axis 81 rearward (with the fuel injector) 170 mouth shot in the opposite direction). As shown in Figs. 6 and 7, the adapter 1 is a resin integrally molded member, which is formed with a flange 19 and a cylindrical wall portion formed in a multi-stepped cylindrical shape;
凸緣帅對於轴線81沿—徑向向外方㈣P 僅沿-狀徑向向外方向凸出之伸長平板形狀。在凸㈣ 之凸出細長部分中,一鎧豎;, 〇_τ… 鎖緊孔19a平行於軸線S1穿透。在 凸緣19中’在心沿轴㈣之鎖緊孔…之對置側上之部 分處,形成一自後方側沿軸線81方向朝前方側凹 部分19b。 筒狀壁部分11包括:一筒站士古 肖狀大直彼部分12’其赴鄰於凸 緣19 ; 一筒狀小直徑部分14,其在 罝瓜上小於大直徑部分 140301.doc -13· 201005175 12;及一多階梯式錐形筒狀中間部分13,其位於大直徑部 分12與小直徑部分14之間。大直徑部分12、中間部分13及 小直徑部分14同軸地形成。 在大直徑部分12上,形成有一第一安裝槽,其具有 一凹入於外表面上且沿外表面周向延伸之正方形截面形 狀。在第一安裝槽31&中,裝配有—密封環31b,其係一在 耐熱性方面極佳之氟系列像膠〇型環。第一安裝槽3u與密 封環3 1 b構成一第一密封部分31。 在小直徑部分14上,形成有—第二安裝槽32a,其具有 一凹入於外表面上且沿外表面周向延伸之正方形截面形 狀。在第二安裝槽32a中,裝配有一密封環32b,其係一在 耐熱性方面極佳之氟系列像膠〇形環。第二安裝槽32a與密 封環32b構成一第二密封部分32。構成密封環3lb及32b之 材料不僅限於氟系列像膠,而是較佳使用具有達到允許安 裝於一引擎上之程度之材料特性(例如耐熱性、耐汽油性 及耐水性)的材料。 中間部分13以一多階梯式錐形方式在外徑及内徑上縮減 並連接大直徑部分12與小直徑部分14。 如圖4中所示,當燃料噴射器本體172安裝於筒狀壁部分 11中時,大直徑部分12之内周邊表面及中間部分13之内周 邊表面與燃料喷射器本體172之外周邊表面裝配。進一步 地,燃料噴射器本體172之尖端與該中間部分之尖端侧階 梯式部分接觸從而將燃料口丨7丨定位至中間部分〗3之尖端 側。此時,一形成於燃料噴射器本體172上之凸出部(未顯 140301.doc •14· 201005175 不)裝配於定位部分19b中以將燃料喷射器本體172相對於 轉接器10定位於軸線S1周圍。 在燃料喷射器本體172之外周邊表面與大直徑部分12之 内周邊表面之間,具有一密封環172b,其係一在耐熱性方 • 面極佳之氟系列像膠〇型環。密封環172b構成為密封燃料 . 喷射本體172與筒狀壁部分11之間的間隙從而防止空氣向 汽缸環172b的外部洩漏。構成密封環17215之材料不僅限於 氟系列像膠,而是較佳使用具有達到允許安裝於一引擎上 ® t材料特性(例如财熱性、耐汽油性及耐水性)之材料。 如圖4至7中所示,在中間部分13之尖端側處,形成有四 個連通孔15。連通孔15係以9〇度間隔沿筒狀壁部分之圓 周方向配置成一排。每一連通孔15之形狀及尺寸皆設定為 相同。如圖7及9中最佳顯*,每一連通孔15皆形成為一 Z 筒狀壁部分1 1之圓周方向拉長之長孔,更特定而言,—沿 該周向方式拉長之矩形孔。在毗鄰連通孔15之間,形成^ 一柱部分16,其係一用於分隔連通孔15之部分。 如圖7中所示,每一連通孔15皆相對於定位於中間部分 13之尖端側處之喷射口 171沿筒狀壁部分u之轴線si方向 .肖前定位。在開口於筒狀壁部分此内表面側處之每—連 • 通孔15之開口邊緣之中,沿一與燃料噴射器17〇之噴射方 向相交之方向延伸且位於靠近噴射口 m之側處的邊緣部 刀15a位於一個在除末端拐角R部分以外之範圍内垂直於軸 線S1方向之平面p(僅顯示於圖7中)上。較佳地,平面p與 喷射口 171之間的距離設定為盡可能短以增強燃料霧化。 140301.doc -15- 201005175 如圖7及9中所示,在其中形成每—連通孔15之筒狀壁部 刀11之#为中,外表面側形成為一沿轴線si方向之錐形形 狀(更特定而言,當轴線81自該側看去時,筒狀壁部分二 之外表面向前漸縮至每-連通口 15之約二分之一,且隨後 沿軸線si方向向前延伸),且内表面側沿轴線si方向形 成。每一連通孔15皆沿一垂直於轴線S1方向之方向穿透。 藉由形成如丨文所提及之形狀,每一連通孔15中之筒狀壁 部分11之外表面侧之開口平面之面積15p(由圖9中之虛雙 點線環繞之範圍之面積,實際上,彎曲表面之面積)小於 外表面側之開口平面之面積15q(由圖9中之虛點線環繞之 範圍之面積,實際上彎曲表面之面積)。換言之,每一連 通孔15皆形成呈一在截面面積上自筒狀壁部分^之外表面 側朝其内表面側減少之孔口形狀。 較佳地,形成實施例1之轉接器10之樹脂在耐熱性、熱 絕緣、耐汽油性、耐水性及強度方面為高。特定而言,較 佳使用酚樹脂(一般溫度上限:約180。)或PPS(聚苯硫醚)樹 脂(一般溫度上限:約260。)作為該樹脂。此使得汽缸蓋121 之南溫難以傳導至燃料噴射器1 7 0同時保證轉接器丨〇對燃 料喷射器170之確保固持。 如圖8中所示,由樹脂形成之轉接器1〇可藉由下述方式 一趙模製而成:使用兩個對開模91 a及91 b及一滑動芯92來 實施噴射模製或轉移模製。 特定而言,對開模91a及91b具有沿著沿線VIII-VIII(顯 示於圖6中)剖切之截面延伸且包括筒狀壁部分^之轴線S1 I40301.doc -16· 201005175 之裝配面’且構成為形成轉接器10之外表面及四個連通孔 15。滑動芯92可沿筒狀壁部分11之轴線si方向滑動且構成 為形成筒狀壁部分11之内表面。 如圖6中所示’在自軸線S1方向看去呈一扇形形式之形 狀之每一連通孔1 5中,由該扇形形式之兩個線性側形成之 角度設定至90度。該兩側中之一者與νίπ-νΐΐΐ截面平行, 且另一者垂直於VIII-VIII截面。因此,根據具有沿VIII_ VIII截面延伸之裝配面之拼合式模91&及91|3,可自拼合式 模91a及91b移除模製轉接器10而不對每一模製連通孔15造 成任何損壞。 滑動怒92形成具有一能夠同時形成鎖緊孔19a及定位部 分19b之形狀。進一步地,在圖6中,凸緣19本身相對於 VIII-VIII截面不對稱。因此’當¥111-乂111截面用作一裝配 面時’無法自該模移除其位置毗鄰於鎖緊孔l9a之部分。 為瞭解決此問題’藉由使對應於凸緣j 9之鎖緊孔19a附近 之對開模91a之一部分朝對開模911)凸出以使對開模9U及 9lb之裝配面部分地變形,可自該模移除凸緣19之鎖緊孔 19a之附近。 如圖4中所示,當轉接器10之筒狀壁部分u插入至含納 部分137中而燃料喷射器170由該轉接器固持時,凸緣19與 >飞缸蓋121之外面接觸。然後,螺栓(未圖解闡釋)插入至形 成於燃料喷射本體172中之安裝孔(未圖解闡釋)及鎖緊孔 19a中並與形成於汽缸蓋pi之外面中之内螺紋(未圖解闡 釋)螺紋卡合。因此,燃料喷射器17〇經由轉接器1〇緊固至 140301.doc 201005175 含納部分13 7。 大直徑部分12定位於汽缸蓋121之外表面側處而轉接器 1〇定位於含納部分137中。大直徑部分以外周邊表面以 裝配方式固定至靠近汽缸蓋121之外面之含納部分ip之壁 表面°此時’第-密封部分31密封於大直徑部分12之外周 邊表面與含納部分137之壁表面之間。 在其中轉接器10配置於含納部分137中之狀態下,小 直接部分14定位於靠近進氣閥開口⑵之側處並沿喷射口 171之轴線si方向(沿燃料噴射器17〇之喷射方向)向前凸 出”i、直徑部分14之外周邊表面以裝配方式固定至靠近進 氣口 131之含納部分137之壁表面。此時,第二密封部㈣ 密封於小直徑部分14之外周邊表面與含納部分137之壁表 面之間。 因此,筒狀壁部分11之外表面與含納部分137之壁表面 形成第至174a。第一室174a係一以軸線S1為中心之環 形空間。此外,在㈣部分u之内表面側處,形成有一第 至174b第一至174b沿軸線S1方向向前延伸且與進氣口 131連通同時由小直徑部分14之内周邊表面及含納部分η? 之壁表面環繞。第一室17乜與第二室i74b由連通孔15連 通。第一室174a與第二室174b構成一室174。 自節流本體160分叉之旁路通道18〇之一下游側開口 18扑 與室174之第一室174a連通。旁路通道18〇經由(例如)一連 接管180c及一軟管180(1(參見圖2)與上游側開口 18〇&連通。 如圖4中所示’位於筒狀壁部分丨丨之外表面側處之每一 140301.doc • 18- 201005175 連通孔15之開口皆相對於室174中之旁路通道i8〇之下游側 開口 180b沿轴線S1方向向後偏移。此將達成藉由使自室 174之第-室174a朝每—連通孔15流動之輔助空氣之流動 通道彎曲來使欲引人至第二室17财之輔助空氣在以輛線 S1為中心的各個方向(360。)上更均勻化。The flange is elongated in the shape of an elongated plate in which the axis 81 protrudes in a radially outward direction only in a radial direction outward (four) P. In the convex elongated portion of the convex (four), a vertical; 〇_τ... the locking hole 19a penetrates parallel to the axis S1. In the flange 19, a portion on the opposite side of the locking hole ... on the center of the shaft (four) forms a concave portion 19b toward the front side in the direction of the axis 81 from the rear side. The cylindrical wall portion 11 includes: a tube-shaped siemens-shaped large straight portion 12' which is adjacent to the flange 19; a cylindrical small-diameter portion 14 which is smaller than the large-diameter portion on the squash 140301.doc -13 · 201005175 12; and a multi-stepped tapered cylindrical intermediate portion 13 between the large diameter portion 12 and the small diameter portion 14. The large diameter portion 12, the intermediate portion 13 and the small diameter portion 14 are formed coaxially. On the large diameter portion 12, there is formed a first mounting groove having a square cross-sectional shape recessed on the outer surface and extending circumferentially along the outer surface. In the first mounting groove 31 & a seal ring 31b is assembled, which is a fluorine series like a plastic ring type which is excellent in heat resistance. The first mounting groove 3u and the sealing ring 3 1 b constitute a first sealing portion 31. On the small-diameter portion 14, there is formed a second mounting groove 32a having a square cross-sectional shape recessed on the outer surface and extending circumferentially along the outer surface. In the second mounting groove 32a, a seal ring 32b is assembled which is a fluorine series like a plastic ring which is excellent in heat resistance. The second mounting groove 32a and the sealing ring 32b constitute a second sealing portion 32. The material constituting the seal rings 31b and 32b is not limited to the fluorine-based adhesive, but a material having a material property (e.g., heat resistance, gasoline resistance, and water resistance) to the extent that it is allowed to be mounted on an engine is preferably used. The intermediate portion 13 is reduced in the outer diameter and the inner diameter in a multi-stepped tapered manner and connects the large diameter portion 12 and the small diameter portion 14. As shown in FIG. 4, when the fuel injector body 172 is mounted in the cylindrical wall portion 11, the inner peripheral surface of the large diameter portion 12 and the inner peripheral surface of the intermediate portion 13 are assembled with the outer peripheral surface of the fuel injector body 172. . Further, the tip end of the fuel injector body 172 is in contact with the tip end stepped portion of the intermediate portion to position the fuel port 7' to the tip end side of the intermediate portion 〖3. At this time, a projection formed on the fuel injector body 172 (not shown 140301.doc • 14·201005175) is fitted in the positioning portion 19b to position the fuel injector body 172 relative to the adapter 10 at the axis. Around S1. Between the outer peripheral surface of the fuel injector body 172 and the inner peripheral surface of the large-diameter portion 12, there is a seal ring 172b which is a fluorine-like adhesive-like ring which is excellent in heat resistance. The seal ring 172b is configured to seal the fuel. The gap between the injection body 172 and the cylindrical wall portion 11 prevents air from leaking to the outside of the cylinder ring 172b. The material constituting the seal ring 17215 is not limited to the fluorine-based adhesive, but is preferably a material having a material property (e.g., heat resistance, gasoline resistance, and water resistance) that allows mounting on an engine. As shown in Figs. 4 to 7, at the tip end side of the intermediate portion 13, four communication holes 15 are formed. The communication holes 15 are arranged in a row along the circumferential direction of the cylindrical wall portion at intervals of 9 turns. The shape and size of each of the communication holes 15 are set to be the same. As best seen in Figures 7 and 9, each of the communication holes 15 is formed as a long hole elongated in the circumferential direction of a Z-cylindrical wall portion 11 and, more specifically, elongated in the circumferential direction. Rectangular hole. Between the adjacent communication holes 15, a column portion 16 is formed which is a portion for separating the communication holes 15. As shown in Fig. 7, each of the communication holes 15 is positioned with respect to the ejection opening 171 positioned at the tip end side of the intermediate portion 13 in the direction of the axis si of the cylindrical wall portion u. Among the opening edges of each of the through holes 15 opening at the inner surface side of the cylindrical wall portion, extending in a direction intersecting the ejection direction of the fuel injector 17A and located at the side close to the ejection opening m The edge portion knife 15a is located on a plane p (shown only in Fig. 7) perpendicular to the direction of the axis S1 in a range other than the end corner portion R. Preferably, the distance between the plane p and the injection port 171 is set to be as short as possible to enhance fuel atomization. 140301.doc -15- 201005175 As shown in FIGS. 7 and 9, in the middle of the cylindrical wall portion knife 11 in which each of the communication holes 15 is formed, the outer surface side is formed into a tapered shape along the axis si direction. The shape (more specifically, when the axis 81 is viewed from the side, the outer surface of the cylindrical wall portion 2 is tapered forward to about one-half of each of the communication ports 15, and then forwards along the axis si Extending), and the inner surface side is formed along the axis si direction. Each of the communication holes 15 penetrates in a direction perpendicular to the direction of the axis S1. By forming the shape as mentioned in the text, the area of the opening plane 15p on the outer surface side of the cylindrical wall portion 11 in each of the communication holes 15 (the area surrounded by the virtual double dotted line in Fig. 9, Actually, the area of the curved surface is smaller than the area 15q of the opening plane on the outer surface side (the area of the range surrounded by the dotted line in Fig. 9, actually the area of the curved surface). In other words, each of the through holes 15 is formed in an aperture shape which is reduced in cross-sectional area from the outer surface side of the cylindrical wall portion toward the inner surface side thereof. Preferably, the resin forming the adapter 10 of the first embodiment is high in heat resistance, thermal insulation, gasoline resistance, water resistance and strength. Specifically, it is preferred to use a phenol resin (generally upper temperature limit: about 180.) or PPS (polyphenylene sulfide) resin (general temperature upper limit: about 260.) as the resin. This makes it difficult to conduct the south temperature of the cylinder head 121 to the fuel injector 170 while ensuring that the adapter 丨〇 secures the fuel injector 170. As shown in FIG. 8, the adapter 1 formed of a resin can be molded by using a pair of split molds 91a and 91b and a slide core 92 for injection molding or Transfer molding. Specifically, the split molds 91a and 91b have an assembly surface extending along a section cut along line VIII-VIII (shown in FIG. 6) and including the axis S1 I40301.doc -16· 201005175 of the cylindrical wall portion ^ And configured to form the outer surface of the adapter 10 and the four communication holes 15. The slide core 92 is slidable in the direction of the axis si of the cylindrical wall portion 11 and is formed to form the inner surface of the cylindrical wall portion 11. As shown in Fig. 6, in each of the communication holes 15 which is in the shape of a sector as seen from the direction of the axis S1, the angle formed by the two linear sides of the sector form is set to 90 degrees. One of the two sides is parallel to the νίπ-νΐΐΐ section, and the other is perpendicular to the VIII-VIII section. Therefore, according to the split molds 91 & and 91|3 having the fitting faces extending along the VIII_VIII section, the molded adapters 10 can be removed from the split molds 91a and 91b without causing any of the molded communication holes 15 damage. The sliding anger 92 is formed to have a shape capable of simultaneously forming the locking hole 19a and the positioning portion 19b. Further, in Fig. 6, the flange 19 itself is asymmetrical with respect to the section VIII-VIII. Therefore, when the section of the ¥111-乂111 is used as a fitting surface, it is impossible to remove the portion of the mold which is adjacent to the locking hole 19a from the mold. In order to solve this problem, 'the portion of the split mold 91a corresponding to the vicinity of the locking hole 19a corresponding to the flange j9 is convex toward the split mold 911) to partially deform the assembly faces of the split molds 9U and 9lb. The mold removes the vicinity of the locking hole 19a of the flange 19. As shown in FIG. 4, when the cylindrical wall portion u of the adapter 10 is inserted into the containing portion 137 and the fuel injector 170 is held by the adapter, the flange 19 and the outer surface of the fly cylinder cover 121 are contact. Then, a bolt (not illustrated) is inserted into a mounting hole (not illustrated) formed in the fuel injection body 172 and the locking hole 19a and internally threaded (not illustrated) formed in the outer surface of the cylinder head pi Engage. Therefore, the fuel injector 17 is fastened via the adapter 1 to the 140301.doc 201005175 containing portion 13 7 . The large diameter portion 12 is positioned at the outer surface side of the cylinder head 121 and the adapter 1 is positioned in the containing portion 137. The outer peripheral surface of the large diameter portion is fixed in an assembled manner to the wall surface of the containing portion ip near the outer surface of the cylinder head 121. At this time, the 'first sealing portion 31 is sealed to the outer peripheral surface of the large diameter portion 12 and the containing portion 137. Between the wall surfaces. In a state in which the adapter 10 is disposed in the containing portion 137, the small direct portion 14 is positioned near the side of the intake valve opening (2) and in the direction of the axis si of the injection port 171 (along the fuel injector 17) The ejection direction) protrudes forward i. The outer peripheral surface of the diameter portion 14 is fixed in an assembled manner to the wall surface of the containing portion 137 adjacent to the air inlet 131. At this time, the second sealing portion (4) is sealed to the small diameter portion 14 The outer peripheral surface is between the wall surface of the containing portion 137. Therefore, the outer surface of the cylindrical wall portion 11 forms a first to 174a with the wall surface of the containing portion 137. The first chamber 174a is centered on the axis S1. Further, at the inner surface side of the (four) portion u, a first to 174b first to 174b are formed to extend forward in the direction of the axis S1 and communicate with the air inlet 131 while being surrounded by the inner peripheral surface of the small diameter portion 14 and The wall portion of the nano portion η? is surrounded. The first chamber 17A and the second chamber i74b are communicated by the communication hole 15. The first chamber 174a and the second chamber 174b constitute a chamber 174. The bypass passage from the throttle body 160 One of the 18 下游 downstream side openings 18 flutters with the first chamber 17 of the chamber 174 4a is connected. The bypass passage 18 is connected to the upstream side opening 18〇& via, for example, a connecting pipe 180c and a hose 180 (1 (see Fig. 2). As shown in Fig. 4, 'located in the cylindrical wall portion丨Each of the outer surface sides of the crucible is 140301.doc • 18- 201005175 The opening of the communication hole 15 is offset rearward in the direction of the axis S1 with respect to the downstream side opening 180b of the bypass passage i8 in the chamber 174. This will be achieved. By bending the flow passage of the auxiliary air flowing from the first chamber 174a of the chamber 174 toward each of the communication holes 15, the auxiliary air to be introduced to the second chamber is in all directions centered on the line S1 (360). .) is more uniform.
如圖4及5中所示,作為用於劃分毗鄰連通孔15之部分之 柱部分16中之―者配置於藉由下述方式所獲得之投影範圍 E(僅顯示於圖4及5中)内··使位於室m之側處之旁路通道 1 80之下游側開口 1 80b之開口表面沿旁路通道丨8〇之中心轴 線S2(僅顯示於圖5中)投影至筒狀壁部分u之側。此將達 成藉由使欲引入至室174之第一室17乜中之輔助空氣與柱 部分16中之一者接觸來使其攪動。 從達成輔助空氣在以中心軸線81為中心的各個方向上均 勻化之觀點出發,位於旁路通道18〇之下游側端開口18肋 附近之中心軸線S2經過室174之中心軸線S1可認為更佳。 然而,在此一情況下,使用五軸機對汽缸蓋121之處理步 驟變得複雜’從而在一些情況下難以達成製造成本之降 低。由於這種原因,在實施例!中,位於下游側開口 18讣 附近之旁路通道18〇之中心轴線S2偏離室174之中心軸線si 以達成使用五軸機對汽缸蓋12ι之處理步驟之簡化。 在如上文所述構造之燃料噴射器170中,一燃料箱(未圖 解闡釋)中之燃料經由一燃料供應軟管(未圖解闡釋)及一燃 料供應軟管連接部分172a引入至燃料喷射器本體172中。 安裝於燃料噴射器本體172中之電磁操作閥與進氣閥132之 140301.doc •19- 201005175 打開及閉合操作同步以預定時序實施打開及閉合 將燃料自喷射口171沿軸線S1方向(沿燃料噴❹⑽之喷 射方向)向前喷射。因此,燃料與進氣之燃料-空氣混合物 引入至燃燒室c中。此燃料喷射時序由—例如—ecu^擎 控制單元)之控制器控制。 此時’第-及第二節流閥161及162由騎乘者之節流操作 控制以在相應搖臂軸1613及162&周圍擺動從而控制自節流 本體160流至進氣口〗31中之進氣之流動速率及引入至= 174之第一室174&中之輔助空氣之流動速率。 第二節流閥162連接至耦接至圖丨中所示之把手1〇3之節 流手柄之節流操作纜索(未圖解闡釋)。第一節流閥i6i連接 至一藉由其以一延遲方式傳輸對節流纜索(未圖解闡釋)之 操作的鏈接式延遲機構(未圖解闡釋)。因此,當騎乘者增 大對節流手柄之操作量時,第二節流閥162之開度與該操 作篁對應増大。另一方面,第一節流閥161之開度保持完 全閉合狀態直至節流手柄被操作達一預定操作量為止。當 其超過預疋操作量時,開度以相同之比率增大同時相對於 第二節流閥162延遲。 舉例而言’如圖3中所示’當引擎處於一空載狀態(閒置 狀態)下或處於一低負載狀態下(處於一其中對節流手柄之 操作量為小之狀態下)時,第一節流閥161處於一完全閉合 狀態下。因此’欲使其自構成主通道之節流本體16〇流至 進氣口 131之進氣之流動速率變為零。另一方面,第二節 流閥162不處於一完全閉合狀態下,且因此輔助空氣自上 140301.doc • 20- 201005175 游側開口 180a經由旁路通道18〇引入至室174之第—室丨74a 中。然後,此辅助空氣經由每一連通孔15引入至第二室 17仆中之噴射口 171附近中。因此,欲自噴射口 171噴射之 燃料之霧化得到增強。辅助空氣同時對燃料噴射器本體 171之尖端側實施冷卻。 接下來,當引擎變成一高負載狀態(其中對節流手柄之 操作量為大之狀態)時,第一節流閥161不再處於一完全閉 合狀態下且在開度方面增大,此又會增大欲使其自節流本 ^ 體160流至進氣口 131中之進氣之流動速率。因此,欲引入 至燃燒室c中之進氣增大,且因此引擎120之輸出增大。此 外,第一節流閥162之開度進一步增大,從而促成更多辅 助空氣自上游側開口 l80a經由旁路通道18〇、第一室174a 及每一連通孔15引入至第二室174b中之噴射口 171附近。 因此,自喷射口 171喷射之燃料之霧化得到進一步增強。 輔助空氣對燃料喷射器本體171之尖端側之冷卻作用得以 保持。 在一高負載狀態下’當對節流手柄之操作量進一步增大 時,第一節流閥1 61之開度對應於其進一步增大。因此, 欲使其自節流本體160流至進氣口 131中之進氣之流動速率 - 進一步增大’從而促成引擎120之輸出進—步增大。在此 種情況下,儘管第二節流閥162之開度進—步增大,但進 氣口 131中之壓力與旁路通道18〇中之壓力之間的差亦增 大,從而達到欲引入至旁路通道180中之輔助空氣之流動 速率之一峰值。 140301.(j〇c -21 · 201005175 4_對實施例1之功能及作用之說明 除凸緣19以外之轉接器1〇之部 < °丨刀(亦即’沿軸線S i方向As shown in FIGS. 4 and 5, the column portion 16 for dividing the portion adjacent to the communication hole 15 is disposed in the projection range E obtained by the following means (only shown in FIGS. 4 and 5). The opening surface of the downstream side opening 1 80b of the bypass passage 180 at the side of the chamber m is projected to the cylindrical wall along the central axis S2 of the bypass passage 丨8 (shown only in FIG. 5) Part u side. This will be achieved by causing the auxiliary air to be introduced into the first chamber 17 of the chamber 174 to contact one of the column portions 16 to agitate it. From the viewpoint of achieving uniformization of the auxiliary air in all directions centered on the central axis 81, the central axis S2 located near the rib of the downstream side end opening 18 of the bypass passage 18〇 passes through the central axis S1 of the chamber 174, which is considered to be better. . However, in this case, the processing steps of the cylinder head 121 using the five-axis machine become complicated', and thus it is difficult to achieve a reduction in manufacturing cost in some cases. For this reason, in the embodiment! The central axis S2 of the bypass passage 18〇 located near the downstream side opening 18讣 deviates from the central axis si of the chamber 174 to achieve a simplification of the processing steps of the cylinder head 121 using the five-axis machine. In the fuel injector 170 constructed as described above, fuel in a fuel tank (not illustrated) is introduced to the fuel injector body via a fuel supply hose (not illustrated) and a fuel supply hose connection portion 172a. 172. The solenoid-operated valve installed in the fuel injector body 172 is synchronized with the opening and closing operation of the intake valve 132 in the fuel injector body 172. The opening and closing are performed at predetermined timings to direct the fuel from the injection port 171 in the direction of the axis S1 (along the fuel) The spray direction of the sneeze (10) is sprayed forward. Therefore, the fuel-air mixture of fuel and intake air is introduced into the combustion chamber c. This fuel injection timing is controlled by a controller, for example, an ecu engine control unit. At this time, the 'first and second throttle valves 161 and 162 are controlled by the rider's throttle operation to swing around the respective rocker shafts 1613 and 162& to control the flow from the throttle body 160 to the intake port 31. The flow rate of the intake air and the flow rate of the auxiliary air introduced into the first chamber 174 & The second throttle valve 162 is coupled to a throttle operating cable (not illustrated) coupled to the throttle handle of the handle 1〇3 shown in FIG. The first throttle valve i6i is coupled to a linked delay mechanism (not illustrated) for transmitting the operation of the throttle cable (not illustrated) in a delayed manner. Therefore, when the rider increases the amount of operation of the throttle handle, the opening degree of the second throttle valve 162 corresponds to the operation 篁. On the other hand, the opening degree of the first throttle valve 161 is kept in a completely closed state until the throttle handle is operated for a predetermined operation amount. When it exceeds the pre-turn operation amount, the opening degree is increased by the same ratio while being delayed with respect to the second throttle valve 162. For example, as shown in FIG. 3, when the engine is in an idle state (idle state) or in a low load state (in a state in which the operation amount of the throttle handle is small), The throttle valve 161 is in a fully closed state. Therefore, the flow rate of the intake air flowing from the throttle body 16 constituting the main passage to the intake port 131 becomes zero. On the other hand, the second throttle valve 162 is not in a fully closed state, and thus the auxiliary air is introduced from the upper 140301.doc • 20- 201005175 the side opening 180a via the bypass passage 18 to the first chamber of the chamber 174. 74a. Then, this auxiliary air is introduced into the vicinity of the ejection port 171 in the servant of the second chamber 17 via each of the communication holes 15. Therefore, the atomization of the fuel to be injected from the ejection port 171 is enhanced. The auxiliary air simultaneously cools the tip end side of the fuel injector body 171. Next, when the engine becomes a high load state (in which the operation amount of the throttle handle is large), the first throttle valve 161 is no longer in a fully closed state and increases in opening degree, which in turn The flow rate of the intake air to flow from the throttle body 160 to the intake port 131 is increased. Therefore, the intake air to be introduced into the combustion chamber c is increased, and thus the output of the engine 120 is increased. In addition, the opening degree of the first throttle valve 162 is further increased, thereby causing more auxiliary air to be introduced into the second chamber 174b from the upstream side opening 110a via the bypass passage 18, the first chamber 174a, and each of the communication holes 15. Near the injection port 171. Therefore, the atomization of the fuel injected from the injection port 171 is further enhanced. The cooling effect of the auxiliary air on the tip end side of the fuel injector body 171 is maintained. In a high load state, when the amount of operation of the throttle handle is further increased, the opening degree of the first throttle valve 1 61 corresponds to its further increase. Therefore, the flow rate of the intake air flowing from the throttle body 160 to the intake port 131 - further increased - causes the output of the engine 120 to increase step by step. In this case, although the opening degree of the second throttle valve 162 is further increased, the difference between the pressure in the intake port 131 and the pressure in the bypass passage 18〇 is increased, thereby achieving the desired One of the peaks of the flow rate of the auxiliary air introduced into the bypass passage 180. 140301. (j〇c - 21 · 201005175 4_ Description of the function and effect of the embodiment 1 except for the flange 19, the portion of the adapter 1 & 丨 ( (that is, ' along the axis S i direction
(沿燃料噴射器17〇之噴射方向、W )向别延伸同時環繞嗜射口 171、沿徑向分隔室174且具有 丹有形成於噴射口 171附近之筒 狀壁部分11中之每一連通孔15夕销 遇扎15之琦狀壁部分11)起一構成 實施例1之引擎120之分隔構件之作用。 在實施例1之引擎120中,第一月笙一— 乐及第一密封部分31及32在 介入沿軸線S1方向向前及向後之每一連通孔15之位置處密 封於形成室174之含納部分137之壁表面與筒狀壁部分^之 外周邊表面之間。換言之,不僅第一密封部分川方止自室 174之第-室174a至汽缸蓋121之—外部之空錢漏,而且 第二密封部分32防止自第一室174&朝構成主通道之進氣口 131之直接空氣洩漏。因此,在此引擎12〇中經由旁路通 道180引入至第一室174a中之輔助空氣可均經由每一連通 孔1 5吹至第二室174b中之喷射口 17 1附近中,從而增強燃 料之霧化。 因此,實施例1之引擎120可改良燃料之霧化效率。 此外,在此引擎120中,具有一形成室174之壁表面137& 之含納部分137形成於汽缸蓋121中而開口打開於該汽缸蓋 之外表面處。轉接器10係一與汽缸蓋121分開形成之構 件。燃料噴射器170經由轉接器10安裝於含納部分137中。 因此’在此引擎120中,一用於將燃料噴射器17〇安裝於汽 缸蓋121中之構件及一用於分隔室174之構件可由—單個構 件構成,從而可防止部件數量之增加。 140301.doc -22- 201005175 此外,在此引擎丨20中,第一及第二密封部分31及32係 由沿喷射口 171之軸線S1方向形成於每一連通孔15之兩侧 處之第一及第二安裴槽31a及31b與分別裝配於安裝槽31a 及32a中之密封環31bA32b構成。轉接器1〇構成為使密封 環3 lb及32b可安裝於其上,從而實現一僅在燃料喷射器 I70之側處之密封結構。因此,燃料喷射器171與引擎12〇 之組裝作業可容易實施。 此外,在此引擎120中,每一連通孔15皆形成呈一周向 Φ 放大形狀。由於這種原因,在與一圓孔或一沿軸線81方向 拉長之長孔相比開口面積相同之先決條件下,使欲自每一 連通孔15朝喷射口 171引入之辅助空氣集中靠近噴射口 171 成為可能。因此,在此引擎12〇中,輔助空氣可有效地引 入至噴射口 171,從而產生改良之霧化效率。另一方面, 在一圓孔之情況下,為了滿足上述先決條件,需要將該等 孔配置成一鋸齒形配置或增大孔徑,從而致使將輔助空氣 Φ 集中靠近喷射口 171之作用劣化。進一步地,在採用此結 構之情況下,難以沿軸向方向縮短轉接器10之尺寸。 此外,在此引擎120中,四個連通孔15沿筒狀壁部分u 之圓周方向配置。因此,辅助空氣之引入可不經由單個連 通孔而經由沿該圓周方向配置成一分散狀態之複數個部分 來實施,從而使更有效地實施燃料之霧化成為可能。特別 地,在此實施例中,由於與該鋸齒形配置相比連通孔15沿 該圓周方向配置成一排,因此沿轴向方向縮短轉接器丨❹可 谷易實施。 140301.doc •23- 201005175 此外,在此引擎120中,在開口於筒狀壁部分丨丨之内表 面側處之每一連通孔15冬開口邊緣之中,沿一與燃料喷射 器170之喷射方向相交之方向延伸且位於靠近噴射口 i7i之 侧處之邊緣部分15 a位於一個在除末端拐角R部分以外的範 圍内垂直於軸線S1方向(燃料噴射器ι7〇之噴射方向)之平 面p上。因此,在此引擎m中,欲自每—連通孔15朝喷射 口 171引入之辅助空氣可更有效地集中於噴射口 i7i附近。 因此,可進一步改良霧化效率。 此外,在此引擎120中,位於筒狀壁部分u之内周邊表 面侧處之每一連通孔15之開口之面積15p設定為小於位於 外周邊表面側處之每一連通孔丨5之開口之面積Bq。由於 這種原因,每一連通孔15皆可發揮孔口效應,從而可提高 欲自第一室174a經由每一連通孔15引入至第二室口仆之輔 助空氣之流動速度。因此,在此引擎12〇中,進一步改良 霧化效率。 此外,在此引擎丨2〇中,其中形成每一連通孔15之筒狀 壁部分11之部分經形成以使其外表面側沿轴線81方向(沿 燃料喷射器丨7〇之喷射方向)漸縮且其内表面侧沿軸線“方 向(沿燃料喷射器170之喷射方向)形成。每一連通孔15皆沿 一垂直於軸線S1方向(沿燃料噴射器17〇之喷射方向)穿 透。因此,在此引擎120中,每一連通孔15可容易形成呈 上述孔口形狀以避免製造成本增加。 此外,在此引擎120中,若假定每一連通孔15皆相對於 噴射口 17丨沿筒狀壁部分U之轴線S1方向(與燃料喷射器 14030l.doc • 24 - 201005175(in the direction in which the fuel injector 17 is sprayed, W) extends to surround the pericardium 171, along the radial partition 174, and has each of the tubular wall portions 11 formed in the vicinity of the ejection opening 171. The hole-shaped wall portion 11) of the hole 15 is formed to function as a partition member of the engine 120 of the first embodiment. In the engine 120 of the first embodiment, the first month - the first sealing portions 31 and 32 are sealed in the forming chamber 174 at positions where each of the communicating holes 15 forward and backward in the direction of the axis S1 is interposed. The wall surface of the nano portion 137 is between the outer peripheral surface of the cylindrical wall portion. In other words, not only the first sealing portion stops from the first chamber 174a of the chamber 174 to the outside of the cylinder head 121, but also the second sealing portion 32 prevents the air from the first chamber 174 & toward the air passage constituting the main passage Direct air leakage of 131. Therefore, the auxiliary air introduced into the first chamber 174a via the bypass passage 180 in this engine 12A can be blown into the vicinity of the injection port 17 1 in the second chamber 174b via each of the communication holes 15 to enhance the fuel. Atomization. Therefore, the engine 120 of Embodiment 1 can improve the atomization efficiency of the fuel. Further, in this engine 120, the containing portion 137 having a wall surface 137 & forming a chamber 174 is formed in the cylinder head 121 and the opening is opened at the outer surface of the cylinder head. The adapter 10 is a member formed separately from the cylinder head 121. The fuel injector 170 is mounted in the containing portion 137 via the adapter 10. Therefore, in this engine 120, a member for mounting the fuel injector 17A in the cylinder head 121 and a member for the compartment 174 can be constituted by a single member, so that an increase in the number of components can be prevented. 140301.doc -22- 201005175 Further, in the engine casing 20, the first and second sealing portions 31 and 32 are first formed at both sides of each of the communication holes 15 in the direction of the axis S1 of the injection port 171. The second ampoules 31a and 31b are formed by the seal rings 31bA32b which are respectively fitted in the mounting grooves 31a and 32a. The adapter 1 is configured such that the seal rings 3 lb and 32b can be mounted thereon to achieve a sealing structure only at the side of the fuel injector I70. Therefore, the assembly work of the fuel injector 171 and the engine 12A can be easily performed. Further, in this engine 120, each of the communication holes 15 is formed in a magnified shape in a circumferential direction Φ. For this reason, the auxiliary air to be introduced from each of the communication holes 15 toward the injection port 171 is concentrated near the ejection port under the premise that the opening area is the same as that of a circular hole or an elongated hole elongated in the direction of the axis 81. 171 is possible. Therefore, in this engine 12, the auxiliary air can be efficiently introduced to the injection port 171, resulting in improved atomization efficiency. On the other hand, in the case of a circular hole, in order to satisfy the above-mentioned preconditions, it is necessary to arrange the holes in a zigzag configuration or to increase the aperture, thereby causing the effect of concentrating the auxiliary air Φ near the ejection port 171 to deteriorate. Further, with this configuration, it is difficult to shorten the size of the adapter 10 in the axial direction. Further, in this engine 120, four communication holes 15 are arranged along the circumferential direction of the cylindrical wall portion u. Therefore, the introduction of the auxiliary air can be carried out via a plurality of portions arranged in a dispersed state in the circumferential direction without passing through a single through hole, thereby making it possible to perform atomization of the fuel more efficiently. In particular, in this embodiment, since the communication holes 15 are arranged in a row in the circumferential direction as compared with the zigzag configuration, shortening the adapter in the axial direction can be easily performed. 140301.doc • 23- 201005175 Further, in this engine 120, among the winter opening edges of each of the communication holes 15 opening at the inner surface side of the cylindrical wall portion ,, along a jet with the fuel injector 170 The edge portion 15a extending in the direction intersecting the direction and located at the side close to the ejection opening i7i is located on a plane p perpendicular to the direction of the axis S1 (the ejection direction of the fuel injector ι7) in a range other than the end corner portion R . Therefore, in this engine m, the auxiliary air to be introduced from the per-communication hole 15 toward the ejection port 171 can be more effectively concentrated in the vicinity of the ejection port i7i. Therefore, the atomization efficiency can be further improved. Further, in this engine 120, the area 15p of the opening of each of the communication holes 15 at the inner peripheral surface side of the cylindrical wall portion u is set smaller than the opening of each of the communication holes 5 at the outer peripheral surface side. Area Bq. For this reason, each of the communication holes 15 can exert an orifice effect, thereby increasing the flow velocity of the auxiliary air to be introduced from the first chamber 174a to the second chamber via each of the communication holes 15. Therefore, in this engine 12, the atomization efficiency is further improved. Further, in this engine unit, a portion in which the cylindrical wall portion 11 of each of the communication holes 15 is formed is formed such that the outer surface side thereof is in the direction of the axis 81 (in the ejection direction of the fuel injector 7). The inner surface side is tapered and formed along the axis "direction (in the ejection direction of the fuel injector 170). Each of the communication holes 15 penetrates in a direction perpendicular to the axis S1 (in the ejection direction of the fuel injector 17). Therefore, in this engine 120, each of the communication holes 15 can be easily formed in the above-described shape of the orifice to avoid an increase in manufacturing cost. Further, in this engine 120, it is assumed that each of the communication holes 15 is adjacent to the ejection port 17 The direction of the axis S1 of the cylindrical wall portion U (with the fuel injector 14030l.doc • 24 - 201005175
之喷射方向相反之方向)向後定位,則自fa經 由母-連通孔15引入至第二室⑽中之輔助空氣不得不繞 過具有喷射口 171之燃料噴射器本體m之尖端部分。然 而,在此引擎120中,每-連通孔15皆相對於喷射口 μ沿 筒狀壁部分11之軸線si方向(燃料喷射器17〇之喷射方向) 向前定位。由於這種原因,I自第一室心經由每一連通 孔15引入至第二室174b之輔助空氣抵達喷射口 ΐ7ι而不在 第二室174b中迁回。因此,進一步改良霧化效率。 此外’在此引擎12G中,位於筒狀壁部分u之外表面側 處之每一連通孔15之開口相對於旁路通道18〇之下游侧開 口 180b沿軸線S1方向(與燃料噴射器17〇之喷射方向相反之 方向)向後偏移。因此,自旁路通道18〇引入至第一室17乜 中之輔助空氣撞擊筒狀壁部分丨丨之外周邊表面並經由每一 連通孔15流入第二室i74b同時改變沿轴線“方向向後之流 動方向。因此,在此引擎120中,欲引入至第二室17朴中 之輔助空氣可沿以軸線s 1為中心之各個方向進一步均勻 化’從而促成較佳霧化。 此外’在此引擎120中,用於分隔毗鄰連通孔15之複數 個柱16之中的柱部分16中之一者配置於旁路通道之下 游側開口 1 80b之投影範圍e内。因此’欲自旁路通道丨8〇引 入至第一室174a中之輔助空氣由柱16攪動。因此,前進至 第二室174b中之辅助空氣可相對於以軸線§1為中心之各個 方向更均勻化,從而促成較佳霧化。在實施例1中’旁路 通道180之中心軸線S2偏離自轴線S1方向看去之室174之中 140301.doc -25- 201005175 心軸線si。然而,亦在此種情況下,藉由柱部分16之攪動 效應,朝該筒狀壁部分之内部前進之辅助空氣可容易沿以 轴線S1為中心之各個方向均勻化。 此外,在此引擎120中,轉接器10係由相對於金屬在可 工作性及可成形性方面極佳之樹脂製成,且因此可達成製 造成本降低。特別地,在實施例丨中,作為形成轉接器1〇 · 之樹脂,採用在熱絕緣、耐熱性、耐汽油性、耐水性及強 度方面高的盼樹脂或PPS樹脂。因此,甚至在嚴格的使用 環境下,轉接器10亦可確保緊固至汽缸蓋121。 g 特別地,轉接器1 0係由一在耐熱性方面高的樹脂形成。 因此,即使引擎120之冷卻類型係一水冷類型或一氣冷類 型,亦可達成汽缸蓋m之高溫至燃料喷射器17〇之硬傳導 同時保持轉接器ίο本身之強度。因此,在實施例1中不需 要一熱絕緣材料,該熱絕緣材料增加當轉接器1〇由金屬製 成時介入於該轉接器與汽缸蓋12ι之間的必要性。因此, 在此引擎120中,可達成藉由減少部件數量之製造成本降 低。 ❹ 此外’在此引擎120中,在由位於軸線s 1方向後方側(燃 料噴射器170之喷射方向之對置側)處之樹脂所形成之轉接 器10之筒狀壁部分11之端部分處,欲緊固至汽缸蓋121之 凸緣19與燃料喷射器no—起一體模製而成。因此,在此 引擎120中,可達成裝置結構之簡化及組裝工時之縮短。 進一步地,凸緣19之一體模製可降低製造成本。 此外,在此引擎120中,凸緣19具有一個用於將該凸緣 140301.doc -26- 201005175 與燃料喷射器m鎖緊在一起之鎖緊孔19a。因此,提供僅 -個鎖緊部分就足矣,從而促成容易的組裝作業。 此外’在此引擎m中,凸緣19具有一凹入定位部分 19a,該凹人定位部分用於藉由與燃料噴射器17时合來將 筒狀壁部分n之周向部分相對於燃料噴射器170定位於轴 線81周圍。因此,在此引擎12G中’可減少用於將燃料喷 射器170裝配於該轉接器中之作業時間。 、此外,實施例1本身之轉接器1〇具有第一及第二密封部 分31及32,從而能夠實現部件數量之減少及組裝作業時間 之減少。 實施m之轉接器10之製造方法如下:使用上述對開模 91a及91bu及滑動芯92來一體模製樹脂轉接器職同時形 成每-連通孔15。因此’與其中藉由一後處理在轉接器中 形成每—連通孔15之情況相比較,可達成製造成本之顯著 降低。 ❷ <實施例2> 如在圖10中所示,實施例2之引擎與實施例1之引擎的不 同點在於:—熱絕緣構件299提供於上面附裝有轉接器10 之含納部分U7之壁表面處;位於筒狀壁部分"之外周邊 表面侧處之每-連通孔15之開口相對於室174中之旁路通 道180之下游側開口議沿轴線S1方向(燃料噴射器170之 喷射方向)向前偏移。實施' ^ J々力、名構與實施例1相 =因此將藉由除不同部分以外分配相同參考編號來省 略說明。 140301.doc -27- 201005175 熱絕緣構件299形Μ-其中上述多階梯式錐形孔狀含 納部分137形成於内表面侧處且外表面侧與汽虹蓋ΐ2ι接觸 並緊固至其之多階梯式錐形孔形狀。緊固熱絕緣構件299 之方法可係任-方法,但較佳密封該熱絕緣構件與該汽缸 蓋之間的一間隙以防止空氣向汽缸蓋121外部洩漏。 較佳地,形成熱絕緣構件299之材料在熱絕緣、耐熱 . 性、耐汽油性、耐水性及強度方面為高。特別地,較佳採 - 用陶瓷、酚樹脂或PPS樹脂。 如上文所述構造之實施例2之引擎亦發揮與實施例i之引 瘳 擎相同之功能及作用。 此外,在此引擎中,甚至在其中無法充分確保轉接器1〇 之熱絕緣之情況下,更特定而言在其中採用一由具有不足 财熱性之材料(例如樹脂或金屬)形成之轉接器1〇之情況 下,熱絕緣構件299確保能夠實現汽缸蓋m之高溫至燃料 喷射器170之硬傳導。因此’在此引擎中,不管引擎冷卻The direction in which the ejection direction is opposite is rearwardly positioned, and the auxiliary air introduced from the fa through the mother-communication hole 15 into the second chamber (10) has to bypass the tip end portion of the fuel injector body m having the ejection port 171. However, in this engine 120, each of the communication holes 15 is positioned forward relative to the injection port μ in the direction of the axis si of the cylindrical wall portion 11 (the ejection direction of the fuel injector 17). For this reason, the auxiliary air introduced from the first chamber center to the second chamber 174b via each of the communication holes 15 reaches the ejection port ΐ7ι and does not move back in the second chamber 174b. Therefore, the atomization efficiency is further improved. Further, in this engine 12G, the opening of each of the communication holes 15 at the outer surface side of the cylindrical wall portion u is in the direction of the axis S1 with respect to the downstream side opening 180b of the bypass passage 18 (with the fuel injector 17) The direction of the opposite direction of the spray is shifted backward. Therefore, the auxiliary air introduced into the first chamber 17A from the bypass passage 18A strikes the outer peripheral surface of the cylindrical wall portion 并 and flows into the second chamber i74b via each of the communication holes 15 while changing the direction "backward" along the axis The direction of flow. Therefore, in this engine 120, the auxiliary air to be introduced into the second chamber 17 can be further homogenized in all directions centered on the axis s 1 to promote better atomization. In the engine 120, one of the column portions 16 for separating the plurality of columns 16 adjacent to the communication hole 15 is disposed within the projection range e of the downstream side opening 1 80b of the bypass passage. The auxiliary air introduced into the first chamber 174a is agitated by the column 16. Therefore, the auxiliary air advanced into the second chamber 174b can be more uniform with respect to the respective directions centered on the axis §1, thereby contributing to better In the first embodiment, the central axis S2 of the bypass passage 180 deviates from the center axis si of the chamber 174 seen from the direction of the axis S1. However, also in this case, By the agitation effect of the column portion 16, The auxiliary air advancing toward the inside of the cylindrical wall portion can be easily homogenized in various directions centered on the axis S1. Further, in the engine 120, the adapter 10 is operable and operable with respect to the metal. It is made of a resin excellent in formability, and thus it is possible to achieve a reduction in manufacturing cost. In particular, in the embodiment, as the resin forming the adapter, thermal insulation, heat resistance, gasoline resistance, The resin and PPS resin are high in water resistance and strength. Therefore, even under strict use environment, the adapter 10 can be secured to the cylinder head 121. g In particular, the adapter 10 is composed of one Therefore, a resin having a high heat resistance is formed. Therefore, even if the cooling type of the engine 120 is a water-cooling type or an air-cooling type, the high temperature of the cylinder head m can be achieved to the hard conduction of the fuel injector 17 while maintaining the adapter ίο itself Therefore, there is no need in the embodiment 1 for a heat insulating material which increases the necessity of intervening between the adapter and the cylinder head 12 when the adapter 1 is made of metal. here In the engine 120, the manufacturing cost reduction by reducing the number of components can be achieved. ❹ In addition, in this engine 120, the resin is located at the rear side in the direction of the axis s1 (the opposite side to the injection direction of the fuel injector 170). At the end portion of the cylindrical wall portion 11 of the formed adapter 10, the flange 19 to be fastened to the cylinder head 121 is integrally molded with the fuel injector no. Therefore, in this engine 120, The simplification of the structure of the device and the shortening of the assembly man-hour can be achieved. Further, one body molding of the flange 19 can reduce the manufacturing cost. Further, in this engine 120, the flange 19 has a flange 140301.doc for the flange 140301. -26- 201005175 A locking hole 19a that is locked with the fuel injector m. Therefore, it is sufficient to provide only one locking portion, thereby facilitating an easy assembly work. Further, in this engine m, the flange 19 has a concave positioning portion 19a for urging the circumferential portion of the cylindrical wall portion n with respect to the fuel injection by cooperating with the fuel injector 17. The device 170 is positioned around the axis 81. Therefore, the operating time for assembling the fuel injector 170 in the adapter can be reduced in this engine 12G. Further, the adapter 1 of the first embodiment itself has the first and second sealing portions 31 and 32, so that the number of parts can be reduced and the assembly work time can be reduced. The manufacturing method of the adapter 10 for performing m is as follows: the above-mentioned split molds 91a and 91bu and the slide core 92 are used to integrally mold the resin adapter to form the per-communication hole 15 at the same time. Therefore, a significant reduction in manufacturing cost can be achieved as compared with the case where each of the communication holes 15 is formed in the adapter by a post-processing. ❷ <Embodiment 2> As shown in Fig. 10, the engine of Embodiment 2 is different from the engine of Embodiment 1 in that: - the heat insulating member 299 is provided on the containing portion on which the adapter 10 is attached The wall surface of the U7; the opening of each of the communication holes 15 at the outer peripheral surface side of the cylindrical wall portion " with respect to the downstream side opening of the bypass passage 180 in the chamber 174 is oriented in the direction of the axis S1 (fuel injection) The ejection direction of the device 170 is shifted forward. The implementation of '^ 々 , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , 140301.doc -27- 201005175 Thermal insulation member 299-shaped Μ- wherein the multi-stepped tapered hole-shaped containing portion 137 is formed at the inner surface side and the outer surface side is in contact with the steam cover ΐ2ι and fastened thereto Stepped tapered hole shape. The method of fastening the heat insulating member 299 may be a method, but it is preferable to seal a gap between the heat insulating member and the cylinder head to prevent air from leaking to the outside of the cylinder head 121. Preferably, the material forming the heat insulating member 299 is high in thermal insulation, heat resistance, gasoline resistance, water resistance and strength. In particular, it is preferred to use ceramic, phenol resin or PPS resin. The engine of the embodiment 2 constructed as described above also exerts the same functions and functions as those of the engine of the embodiment i. Further, in this engine, even in the case where the thermal insulation of the adapter 1 is not sufficiently ensured, more specifically, a transfer formed of a material having insufficient heat (for example, resin or metal) is employed therein. In the case of the device 1, the thermal insulation member 299 ensures that the high temperature of the cylinder head m can be achieved to the hard conduction of the fuel injector 170. So in this engine, regardless of engine cooling
類型,一水冷類型或一氣冷類型,燃料喷射器17〇皆可確 保受到保護。 G 此外’在此引擎中’每一連通孔15皆相對於旁路通道 180之下游侧開口 1 80b沿轴線S1方向(燃料喷射器i 70之喷 射方向)向前偏移。因此,自旁路通道180引入至第一室 174a中之輔助空氣撞擊筒狀壁部分丨丨之外周邊表面且經由 每一連通孔1 5流入第二室174b同時改變沿轴線s 1方向向前 之流動方向。因此,在此引擎120中,欲引入至第二室 174b中之輔助空氣可沿以轴線S1為中心之各個方向進一步 140301.doc -28- 201005175 均勻化,從而促成較佳霧化。 <實施例3> 圖11顯示實施例3之一引擎結構。在上述實施例1及2 中’旁路通道180之另一端(下游側端)直接連接至金屬筒狀 頭121。在實施例3中,旁路通道300之下游端經由一由合 成樹脂製成之連接構件310連接至汽缸蓋3〇1。汽缸蓋301 具有一圓形安裝部分303 ’該圓形安裝部分相對於含納部 分302(室174)同心凹入於該汽缸蓋之上表面上且具有一大 於含納部分302之上端部分之直徑之直徑。 連接室310具有一整個地與轉接器1〇同心形成之筒狀主 體311。在主體311之下端部分處,一體地形成一小直徑筒 狀部分3 12 ’該小直徑筒狀部分具有一與主體3丨丨同心配置 且在外徑上以階梯方式減小之外徑。一密封槽313a形成於 筒狀部分312之外周邊上且由一密封環313b裝配,且此密 封槽313a與密封環313b形成第三密封部分313。 主體311具有一自外周邊表面沿轴向方向穿透至内周邊 表面之圓連接孔314。進一步地,在主體3Π之外周邊上, 與連接孔314同心形成之筒狀狀之連接部分315以一凸出方 式形成。至此連接口 315,旁路通道300之下游側端部分氣 密地裝配並緊固。 在—其中筒狀部分312裝配於安裝部分303中而主體311 之下端表面與汽缸蓋301之上表面接觸之狀態下,連接構 件310附裝至&虹蓋。在連接構件之安裝狀態下, 主體311之内周邊壁構成含納部分3〇2(室174之第—室174約 140301.doc •29· 201005175 之内周邊壁部分之中的一沿燃料喷射器170之喷射方向之 後端侧大致半區(圖11中之上側區)。進一步地,第三密封 部分313氣密地密封筒狀部分312之外周邊表面與安裝部分 303之内周邊表面之間的間隙。 上面先前附裝有燃料喷射器170之轉接器1〇插入於連接 構件310之主體311中。因此,燃料喷射器17〇經由連接構 件310及轉接器ίο附裝至汽缸蓋300(譯者注:正確地3〇1)。 在燃料喷射器170之附裝狀態下,室174之内部由筒狀壁部 分11分隔成外周邊側第一室174a及内周邊侧第二室174b。 主體311之内周邊表面面向第一室i74a。連接至連接部分 315之旁路通道300之下游側經由連接孔314與第一室174a 之内部連通。連接孔3 14相對於連通孔15沿燃料噴射器i 7〇 之喷射方向向後偏移。 在此實施例3中’由合成樹脂製成之連接構件31〇介入於 旁路通道300與汽缸蓋301之間以使旁路通道3〇〇不與由金 屬製成之汽缸蓋301直接接觸。因此,汽缸蓋3〇1之熱量幾 乎不傳輸至旁路通道300。此抑制因流過旁路通道3〇〇之輔 助空氣之熱膨脹而引起之氧濃縮,此又可避免因劣化之氧 濃縮而引起之燃燒效率劣化。 <其他實施例> 本發明不僅限於參照說明及圖示所解釋之實施例。舉例 而言,下述實施例仍屬於本發明之技術範疇内。此外,除 下述以外’可在不背離本發明之要旨之範疇内實施各種修 改。 J4030l.doc •30· 201005175 (i)舉例而言,在實施例丨中,說明係如此簡化以致引 擎120由單個進氣閥開口 128、單個排氣閥開口 m及單個 燃料噴射器17〇構成,但根據本發明之引擎不僅限於此結 構。舉例而言,引擎12〇可包括任意數量之排氣閥開口、 - 進氣閥開口及燃料噴射器。 (2)轉接器(分隔構件)可由常見之材料(如(例如)樹脂、 纖維增強型樹脂或金屬)形成。纖維增強型樹脂可係常見 之增強纖維,如(例如)玻璃纖維或碳纖維。轉接器(分隔構 罾 可使用像膠及樹脂藉由雙模製來製造,且其可構成為 使應保持形狀而不變形之連通口及其附近由樹脂形成,而 剩餘部分由像膠形成。轉接器(分隔構件)可由一單個構件 或複數個構件之一組合構成。在由樹脂形成轉接器(分隔 構件)之情況下,較佳地,該樹脂在熱絕緣、耐熱性、耐 >飞油性、耐水性及強度方面為高。 (3)琦狀壁部分不需要為完全筒狀的,只要其形成呈一 φ 筒狀狀。舉例而言,作為第一及第二密封部分,可採用— 墊圈、一密封劑、像膠烘烤。作為密封環,可使用任一由 (例如)金屬、像膠或彈性體製成之市售構件 ' (4)連通孔可具有任一形狀,如(例如)一垂直拉長孔、 • —水平拉長孔、一圓孔、一方孔、一矩形孔、—本日π f 卞月形 札°連通孔之數量及尺寸不僅限於上述實施例。 (5) 轉接器(分隔構件)之處理方法可係製造方法如 (例如)切削、喷射模製、轉移模製或壓縮模製。 (6) 在上述實施例3中,其構成為使連接構件與轉接器 ]4〇3〇丨如 -3,- 201005175 (分隔構件)處於直接接觸狀態下,但連接構件與轉接器(分 隔構件)可處於非接觸狀態下。 (7)在上述實施例3中,連接構件直接面向第一室,但 其可構成為使連接構件不直接面向第一室。在此種情況 下,其可構成為使一敖使連接構件與第一室之間的連通之 孔部分形成於汽缸蓋中。 (8)在上述實施例3中,形成第一室之壁表面由汽缸蓋Types, one water-cooled or one air-cooled, fuel injectors 17 are guaranteed to be protected. Further, each of the communication holes 15 in the engine is shifted forward in the direction of the axis S1 (the ejection direction of the fuel injector i 70) with respect to the downstream side opening 1 80b of the bypass passage 180. Therefore, the auxiliary air introduced into the first chamber 174a from the bypass passage 180 strikes the outer peripheral surface of the cylindrical wall portion 且 and flows into the second chamber 174b via each of the communication holes 15 while changing the direction along the axis s 1 The direction of the flow before. Thus, in this engine 120, the auxiliary air to be introduced into the second chamber 174b can be further homogenized in various directions centered on the axis S1 by 140301.doc -28- 201005175, thereby facilitating better atomization. <Embodiment 3> Fig. 11 shows an engine structure of Embodiment 3. In the above-described Embodiments 1 and 2, the other end (downstream side end) of the bypass passage 180 is directly connected to the metal cylindrical head 121. In Embodiment 3, the downstream end of the bypass passage 300 is connected to the cylinder head 3〇1 via a connecting member 310 made of a synthetic resin. The cylinder head 301 has a circular mounting portion 303' which is concentrically recessed relative to the containing portion 302 (chamber 174) on the upper surface of the cylinder head and has a larger diameter than the upper end portion of the containing portion 302. The diameter. The connection chamber 310 has a cylindrical body 311 which is formed integrally with the adapter 1A. At a lower end portion of the main body 311, a small-diameter cylindrical portion 3 12 ' is integrally formed. The small-diameter cylindrical portion has an outer diameter concentrically arranged with the main body 3 且 and which is reduced in a stepwise manner on the outer diameter. A seal groove 313a is formed on the outer periphery of the cylindrical portion 312 and is fitted by a seal ring 313b, and this seal groove 313a forms a third seal portion 313 with the seal ring 313b. The main body 311 has a circular connecting hole 314 which penetrates from the outer peripheral surface in the axial direction to the inner peripheral surface. Further, on the outer periphery of the main body 3, a cylindrical connecting portion 315 which is formed concentrically with the connecting hole 314 is formed in a convex manner. At this point, the connection port 315, the downstream side end portion of the bypass passage 300 is airtightly assembled and fastened. In a state in which the cylindrical portion 312 is fitted in the mounting portion 303 and the lower end surface of the main body 311 is in contact with the upper surface of the cylinder head 301, the connecting member 310 is attached to the & rainbow cover. In the mounted state of the connecting member, the inner peripheral wall of the main body 311 constitutes a fuel injector in the inner peripheral portion of the inner portion 3〇2 (the first chamber 174 of the chamber 174 is approximately 140301.doc •29·201005175). Further, the end side is substantially a half area (the upper side area in Fig. 11). Further, the third sealing portion 313 hermetically seals between the outer peripheral surface of the cylindrical portion 312 and the inner peripheral surface of the mounting portion 303. The adapter 1 previously attached to the fuel injector 170 is inserted into the body 311 of the connecting member 310. Therefore, the fuel injector 17 is attached to the cylinder head 300 via the connecting member 310 and the adapter ( Translator's Note: Correctly 3〇1) In the attached state of the fuel injector 170, the inside of the chamber 174 is partitioned by the cylindrical wall portion 11 into an outer peripheral side first chamber 174a and an inner peripheral side second chamber 174b. The inner peripheral surface of the main body 311 faces the first chamber i74a. The downstream side of the bypass passage 300 connected to the connecting portion 315 communicates with the inside of the first chamber 174a via the connecting hole 314. The connecting hole 3 14 is fueled with respect to the communicating hole 15 Direction of spray In this embodiment 3, the connecting member 31 made of synthetic resin is interposed between the bypass passage 300 and the cylinder head 301 so that the bypass passage 3 does not engage with the cylinder head 301 made of metal. Direct contact. Therefore, the heat of the cylinder head 3〇1 is hardly transmitted to the bypass passage 300. This suppresses the concentration of oxygen caused by the thermal expansion of the auxiliary air flowing through the bypass passage 3, which avoids deterioration. The combustion efficiency is deteriorated by the concentration of oxygen. <Other Embodiments> The present invention is not limited to the embodiments explained with reference to the description and the drawings. For example, the following embodiments are still within the technical scope of the present invention. Various modifications may be made without departing from the gist of the present invention. J4030l.doc • 30· 201005175 (i) By way of example, in the embodiment, the description is so simplified that the engine 120 is singled out. The valve opening 128, the single exhaust valve opening m, and the single fuel injector 17 are constructed, but the engine according to the present invention is not limited to this configuration. For example, the engine 12A may include any number of exhaust valve openings, - Intake valve opening and fuel injector. (2) Adapter (separator) can be formed from common materials such as, for example, resin, fiber reinforced resin or metal. Fiber reinforced resin can be a common reinforcing fiber. Such as, for example, glass fiber or carbon fiber. The adapter (the partition structure can be manufactured by double molding using glue and resin, and it can be configured such that the communication port should be maintained without deformation and its vicinity) The resin is formed while the remainder is formed of a gel. The adapter (separating member) may be composed of a single member or a combination of a plurality of members. In the case where the adapter (separator member) is formed of a resin, the resin is preferably high in thermal insulation, heat resistance, oil repellency, water resistance, and strength. (3) The Qi-shaped wall portion does not need to be completely cylindrical as long as it is formed in a φ cylindrical shape. For example, as the first and second sealing portions, a gasket, a sealant, and a gel can be used for baking. As the seal ring, any commercially available member made of, for example, metal, glue or elastomer can be used. (4) The communication hole can have any shape such as, for example, a vertical elongated hole, • horizontal The elongated hole, a circular hole, a single hole, and a rectangular hole, the number and size of the π f 卞 形 ° 、 、 、 、 、 、 、 、 、 、 、 、 、 、 (5) The processing method of the adapter (separating member) may be a manufacturing method such as, for example, cutting, injection molding, transfer molding, or compression molding. (6) In the above-described Embodiment 3, it is configured such that the connecting member is in direct contact with the adapter, such as -3, - 201005175 (separating member), but the connecting member and the adapter ( The partition member) can be in a non-contact state. (7) In the above-described Embodiment 3, the connecting member directly faces the first chamber, but it may be configured such that the connecting member does not directly face the first chamber. In this case, it may be configured such that a hole portion for communicating between the connecting member and the first chamber is formed in the cylinder head. (8) In the above embodiment 3, the wall surface forming the first chamber is covered by the cylinder head
及連接構件構成,但其可構成為使形成第一室之整個壁表 面僅由連接構件構成。 (9) 在上述實施例3中,連接構件具有一筒狀狀,但^ 呈任一不同於一筒狀狀態之形狀(例如,方塊形狀)。 (10) 在上述實施例3中,連接構件係一與轉接器(分隔掮 件)分開形成之構件,但可係一可發揮兩種功能(一將燃剩 噴射器安襞於汽缸蓋上之功能及—作為1於沿軸向分隔 室之分隔構件之功能)中之一者或兩者。 〇1)在上述實施例1至3中,用於將燃料喷射器安裝於汽 ❹ =^之轉接器亦起—分隔構件之翻,但另—專用分隔 構件亦可用來補充該轉接器。 (12) 在上述實施例1至3中, 射器藉由鎖緊一螺栓緊固至汽:蓋接器(分隔構件)及燃料喷 器亦可分開緊固至汽虹蓋。L但轉接器及燃料喷射 (13) 在上述實施例3中,裒开摄丄、 接器與連接構件整合且第一室與第一:藉由使用-其中轉 部分密封之構件來省略第一密封部::、封部分及第三密封 M0301.doc -32- 201005175 【圖式簡單說明】 [圖1 ]圖1係一其中施加實施例1之一引擎之摩托車之一 側視圖; [圖2]圖2係實施例1之引擎之一截面圖; [圖3]圖3係圖1中所示之引擎之主要部分之一放大截面 團, [圖4]圖4係圖3中所示之主要部分之一放大截面圖; [圖5]圖5係一顯示圖4之V-V裁面之截面圖; [圖6]圖6係一沿圖4中之箭頭VI方向看去之轉接器(分 隔構件)之俯視圖; [圖7]圖7係一顯示圖6之VII-VII截面之截面圖; [圖8]圖8係一顯示圖6之VIII-VIII截面之截面圖; [圖9]圖9係一顯示圖8中所示之連通孔之附近之侧視 rgl · 園,And the connecting member, but it may be configured such that the entire wall surface forming the first chamber is constituted only by the connecting member. (9) In the above-described Embodiment 3, the connecting member has a cylindrical shape, but is in any shape different from a cylindrical state (for example, a square shape). (10) In the above-mentioned Embodiment 3, the connecting member is a member formed separately from the adapter (separating member), but it can be used to perform two functions (one is to mount the remaining injector on the cylinder head) One or both of the functions and functions of 1 as a partitioning member separating the chambers in the axial direction. 〇1) In the above embodiments 1 to 3, the adapter for mounting the fuel injector to the steam cylinder also functions as a partition member, but another dedicated partition member may be used to supplement the adapter. . (12) In the above embodiments 1 to 3, the ejector is fastened to the steam by locking a bolt: the cover (separator member) and the fuel injector may be separately fastened to the steam cap. L, but the adapter and the fuel injection (13) In the above-mentioned Embodiment 3, the opening of the camera, the connector and the connecting member are integrated and the first chamber and the first portion are omitted by using the member in which the rotating portion is sealed. A sealing portion::, sealing portion and third sealing M0301.doc -32- 201005175 [Simplified illustration of the drawing] [Fig. 1] Fig. 1 is a side view of a motorcycle in which an engine of Embodiment 1 is applied; Figure 2] Figure 2 is a cross-sectional view of the engine of Embodiment 1; [Figure 3] Figure 3 is an enlarged cross-sectional group of one of the main parts of the engine shown in Figure 1, [Figure 4] Figure 4 is Figure 3 1 is an enlarged cross-sectional view of the main part; [Fig. 5] Fig. 5 is a cross-sectional view showing the VV cut surface of Fig. 4; [Fig. 6] Fig. 6 is a transfer seen in the direction of the arrow VI in Fig. 4. [FIG. 7] FIG. 7 is a cross-sectional view showing a section VII-VII of FIG. 6; [FIG. 8] FIG. 8 is a cross-sectional view showing a section VIII-VIII of FIG. 6; 9] Fig. 9 is a side view rgl · garden showing the vicinity of the communication hole shown in Fig. 8,
[圖10]圖10係一顯示一根據實施例2之引擎之主要部分 之放大截面圖;及 [圖11 ]圖11係一顯示一根據實施例3之引擎之主要部分 之一放大截面圖。 【主要元件符號說明】 轉接器(分隔構件) 筒狀壁部分 連通孔 沿一與燃料噴射器之噴射方向相交之方 向延伸且位於靠近噴射口之側處之連通 10 11 15 15a 140301.doc •33- 201005175 孔之開口邊緣之中的邊緣部分 15p 位於筒狀壁部分之内侧處之連通孔之開 口之面積 15q 位於筒狀壁部分之外側處之連通孔之開 口之面積 16 柱部分 19 凸緣 19a 鎖緊孔 19b 定位部分 31 第一密封部分 31a 第一安裝槽 31b 密封環 32 第二密封部分 32a 第二安裝槽 32b 密封環 120 引擎 121 汽缸蓋 122 汽缸體 124 活塞 128 進氣閥開口 131、160、141 主通道(131.·.進氣口、16〇…節流本 體、141…進氣管) 137 含納部分 137a 形成一室之壁表面 140301.doc -34- 201005175 170 燃料噴射器 171 喷射口 174 室 180 旁路通道 180a 旁路通道之一端(上游端開口) 180b 旁路通道之另一端(下游端開口) 299 熱絕緣構件 C 燃燒室 E 投影範圍 P 一個垂直於噴射器之噴射方向之平面 SI 顯示喷射器之喷射方向之軸線、顯示筒 狀壁部分之軸線 S2 旁路通道之中心軸線[ Fig. 10] Fig. 10 is an enlarged cross-sectional view showing a main portion of an engine according to Embodiment 2; and Fig. 11 is an enlarged cross-sectional view showing an essential part of an engine according to Embodiment 3. [Description of main component symbols] Adapter (separator member) The tubular wall portion communication hole extends in a direction intersecting the injection direction of the fuel injector and is located at a side close to the injection port 10 11 15 15a 140301.doc • 33- 201005175 The edge portion 15p of the opening edge of the hole is located at the inner side of the cylindrical wall portion, and the area 15q of the opening of the communicating hole at the outer side of the cylindrical wall portion is the area of the opening of the communicating hole at the outer side of the cylindrical wall portion. 19a locking hole 19b positioning portion 31 first sealing portion 31a first mounting groove 31b sealing ring 32 second sealing portion 32a second mounting groove 32b sealing ring 120 engine 121 cylinder head 122 cylinder block 124 piston 128 intake valve opening 131, 160, 141 Main channel (131.·. Inlet, 16〇...throttle body, 141...intake pipe) 137 Inclusive part 137a Forms a wall surface of a chamber 140301.doc -34- 201005175 170 Fuel injector 171 Injection port 174 chamber 180 bypass passage 180a one end of the bypass passage (upstream end opening) 180b the other end of the bypass passage (opening end opening) 299 An insulating member projection range P E C combustor a plane perpendicular to the direction of injection of the injector SI the display of the axial direction of the injection of the injector, the central axis of the display S2 of the cylindrical wall portion of the bypass passage axis
140301.doc •35-140301.doc •35-
Claims (1)
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| JP2008188988 | 2008-07-22 | ||
| JP2009043001A JP2010048249A (en) | 2008-07-22 | 2009-02-25 | Engine, partition member and method of manufacturing partition member |
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| TW201005175A true TW201005175A (en) | 2010-02-01 |
| TWI392797B TWI392797B (en) | 2013-04-11 |
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| JP5195893B2 (en) * | 2010-12-24 | 2013-05-15 | トヨタ自動車株式会社 | High pressure pump |
| JP2013108457A (en) * | 2011-11-22 | 2013-06-06 | Suzuki Motor Corp | Arrangement structure for fuel injection device of motorcycle |
| JP5984725B2 (en) * | 2013-03-26 | 2016-09-06 | 三菱重工工作機械株式会社 | Engine fuel injector |
| WO2020145153A1 (en) * | 2019-01-07 | 2020-07-16 | 三菱自動車工業株式会社 | Cylinder head |
| DE102019201507A1 (en) * | 2019-02-06 | 2020-08-06 | Robert Bosch Gmbh | Injector with improved corrosion protection |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4446242A1 (en) * | 1994-12-23 | 1996-06-27 | Bosch Gmbh Robert | Fuel injection device for an internal combustion engine |
| JP4358367B2 (en) * | 1998-10-16 | 2009-11-04 | 本田技研工業株式会社 | Structure and manufacturing method of vehicle body frame |
| US6561167B2 (en) * | 2001-02-16 | 2003-05-13 | Synerject, Llc | Air assist fuel injectors |
| JP2002327665A (en) * | 2001-04-27 | 2002-11-15 | Yamaha Motor Co Ltd | Fuel supply system for 4-cycle engine |
| KR100604300B1 (en) * | 2003-04-03 | 2006-07-31 | 닛산 지도우샤 가부시키가이샤 | Intake system of internal combustion engine |
| EP2138710B1 (en) * | 2004-03-30 | 2012-02-22 | Yamaha Hatsudoki Kabushiki Kaisha | Saddle-straddling type motor vehicle |
-
2009
- 2009-02-25 JP JP2009043001A patent/JP2010048249A/en active Pending
- 2009-05-12 TW TW98115746A patent/TWI392797B/en not_active IP Right Cessation
- 2009-07-22 CN CN2009101647427A patent/CN101634269B/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN101634269B (en) | 2012-07-04 |
| TWI392797B (en) | 2013-04-11 |
| CN101634269A (en) | 2010-01-27 |
| JP2010048249A (en) | 2010-03-04 |
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| Date | Code | Title | Description |
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| MM4A | Annulment or lapse of patent due to non-payment of fees |