JPH02146271A - Hydraulic pressure generating device - Google Patents
Hydraulic pressure generating deviceInfo
- Publication number
- JPH02146271A JPH02146271A JP63298618A JP29861888A JPH02146271A JP H02146271 A JPH02146271 A JP H02146271A JP 63298618 A JP63298618 A JP 63298618A JP 29861888 A JP29861888 A JP 29861888A JP H02146271 A JPH02146271 A JP H02146271A
- Authority
- JP
- Japan
- Prior art keywords
- chamber
- hydraulic pressure
- combustion chamber
- combustion
- pressure
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000002485 combustion reaction Methods 0.000 claims abstract description 61
- 239000000203 mixture Substances 0.000 claims abstract description 29
- 239000007788 liquid Substances 0.000 claims abstract description 28
- 239000002912 waste gas Substances 0.000 claims abstract description 14
- 239000000446 fuel Substances 0.000 claims description 43
- 238000009413 insulation Methods 0.000 claims description 14
- 230000036316 preload Effects 0.000 claims description 11
- 230000002000 scavenging effect Effects 0.000 claims description 8
- 238000010438 heat treatment Methods 0.000 abstract description 2
- 230000005540 biological transmission Effects 0.000 abstract 1
- 230000000903 blocking effect Effects 0.000 abstract 1
- 238000011109 contamination Methods 0.000 abstract 1
- 238000002309 gasification Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 description 6
- 238000006243 chemical reaction Methods 0.000 description 5
- 230000007423 decrease Effects 0.000 description 4
- 239000003502 gasoline Substances 0.000 description 3
- 238000007906 compression Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 230000000630 rising effect Effects 0.000 description 2
- 230000008016 vaporization Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
Landscapes
- Reciprocating Pumps (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明は油や水などの液体に液圧を発生させる装置に関
するものである。DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to an apparatus for generating hydraulic pressure in a liquid such as oil or water.
(従来の技術)
従来の技術では例えば油圧ポンプにみられるように、電
動機の回転力によりベーンポンプや歯車ポンプやプラン
ジャーポンプを駆動して液圧を発生させるのが普通であ
った。しかしながら電動機を駆動する電力を得る過程は
効率が悪い上、電力から液圧を得る過程でも多くの損失
をともなった。(Prior Art) In conventional technology, for example, as seen in hydraulic pumps, hydraulic pressure is usually generated by driving a vane pump, gear pump, or plunger pump using the rotational force of an electric motor. However, the process of obtaining electric power to drive the motor was inefficient, and the process of obtaining hydraulic pressure from electric power also involved a lot of loss.
電動機用の電源が得られない場合には、ガソリンエンジ
ンやディーゼルエンジンによって発電して。If power for an electric motor is not available, generate electricity using a gasoline or diesel engine.
この電力により電動機を回転し液圧を発生させるが、こ
れらのエンジンの効率は低く、燃料の20〜30%のエ
ネルギが出力として取り出せるに過ぎず。This electric power rotates an electric motor and generates hydraulic pressure, but the efficiency of these engines is low and only 20 to 30% of the energy of the fuel can be extracted as output.
これにポンプの効率を乗ずればこの値はさらに低下した
。Multiplying this by the efficiency of the pump further reduced this value.
従来のエンジンの出力の効率が低い原因は、エンジンの
回転数が2000〜8000rpmと極めて高いために
、高温高圧のエネルギを十分に利用できずに廃ガスとし
て大気中に放出したことや、ピストンの往復運動をコン
ロッドとクランクシャフトによって回転運動に変換する
過程でのエネルギ損失が大きいことにあった。The reason for the low output efficiency of conventional engines is that the engine speed is extremely high (2000 to 8000 rpm), so the high temperature and high pressure energy cannot be fully utilized and is released into the atmosphere as waste gas, and the piston The problem was that there was a large amount of energy loss in the process of converting reciprocating motion into rotational motion using the connecting rod and crankshaft.
(発明が解決しようとするK[)
本発明は以上のような従来技術の問題点を克服するため
に、内燃機関での燃焼エネルギを直接的に液圧に変換す
る装置を提供することを第1の目的とする。また本発明
装置において液圧媒体中に燃焼廃ガスの混入を防ぐ液圧
発生装置を提供することを第2の目的とする。さらに燃
焼熱の伝熱により液圧媒体が昇温し気化するのを防ぐ液
圧発生装置を提供することを第3の目的とする。(K to be solved by the invention) In order to overcome the problems of the prior art as described above, the present invention aims to provide a device that directly converts combustion energy in an internal combustion engine into hydraulic pressure. 1 purpose. A second object of the present invention is to provide a hydraulic pressure generating device that prevents combustion waste gas from being mixed into the hydraulic medium in the device of the present invention. A third object of the present invention is to provide a hydraulic pressure generating device that prevents a hydraulic medium from increasing in temperature and vaporizing due to transfer of combustion heat.
(問題点を解決するための手段・作用)本発明は次のよ
うに構成する。すかはち第1図ないし第4図に示すよう
に、一体的に往復運動する一対のピストンl、 2に
よりシリンダ3内を3分割し、端から順に燃料を燃焼す
る燃焼室4と。(Means and effects for solving the problems) The present invention is constructed as follows. As shown in Figures 1 to 4, the inside of the cylinder 3 is divided into three by a pair of pistons 1 and 2 that reciprocate integrally, and a combustion chamber 4 is formed in which fuel is burned sequentially from the end.
燃焼室4からの伝熱を遮る断熱室5と、液体を高圧にす
る液圧室6とにより構成することを特徴とする液圧発生
装置である。第1図の例は吸気弁と排気弁を装備する2
サイクルエンジン(2ストロークサイクルエンジン)の
例であり、ガソリンやLPGやLNGを燃料とするが2
点火プラグ7の代わりに燃料噴射ノズルを用いて灯油や
前記の燃料を噴射しても良い、第1図の装置の燃焼室4
ではピストン1が同図の様に下限にある時に、排気弁9
を問いて燃焼廃ガスを排気し、これより僅かに遅れて吸
気弁8を問いて加圧した燃料混合気を圧力して燃焼廃ガ
スを掃気すると共に、燃焼室4内に燃料混合気を充満さ
せたのち、排気弁9と吸気弁8を閉じる。続けて液圧源
18から逆止め弁を経て液圧室6に低圧の液体を圧力し
てピストン1を押し上げて燃焼室4内の燃料合気を圧縮
し。This is a hydraulic pressure generating device characterized by being constituted by a heat insulating chamber 5 that blocks heat transfer from the combustion chamber 4 and a hydraulic pressure chamber 6 that makes the liquid high pressure. The example in Figure 1 is 2 equipped with an intake valve and an exhaust valve.
This is an example of a cycle engine (two-stroke cycle engine), which uses gasoline, LPG, or LNG as fuel.
The combustion chamber 4 of the device shown in FIG.
Now, when the piston 1 is at the lower limit as shown in the figure, the exhaust valve 9
The combustion chamber 4 is discharged by exhausting the combustion waste gas, and after a slight delay, the intake valve 8 is operated to pressurize the pressurized fuel mixture to scavenge the combustion waste gas and fill the combustion chamber 4 with the fuel mixture. After that, the exhaust valve 9 and the intake valve 8 are closed. Subsequently, low-pressure liquid is applied from the hydraulic pressure source 18 to the hydraulic chamber 6 through the check valve to push up the piston 1 and compress the fuel gas in the combustion chamber 4.
点火プラグ7により燃料に点火して燃焼させて燃焼室4
内を高圧にして、ピストン1. 2を一体的に押し下げ
液圧室内の液体を高圧にし、圧力液体流出配管14を経
て逆止め弁16を押し間き、内部パイロット形圧力制御
弁15の設定圧力よりも液圧が高い間はこれを経由して
アキュムレータ17に蓄える。他の圧力制御弁は点火が
らの時間経過又は液圧室の圧力又はピストン1,2の位
置を検出してこれを信号とし、パイロット圧を操作して
開閉するシーケンス弁が良い1本発明の液圧発生装置の
構成では2以上の液圧発生サイクルの期間中、液圧室の
圧力は断熱室や予圧断熱室の圧力よりも常に高くなる。The fuel is ignited and combusted by the spark plug 7 into the combustion chamber 4.
Make the pressure high inside the piston 1. 2 is pushed down integrally to make the liquid in the hydraulic pressure chamber high pressure, and the check valve 16 is pushed through the pressure liquid outflow pipe 14. It is stored in the accumulator 17 via. Another pressure control valve is a sequence valve that detects the elapsed time of the ignition, the pressure in the hydraulic pressure chamber, or the position of the pistons 1 and 2 and uses this as a signal to operate the pilot pressure to open and close. In the configuration of the pressure generating device, the pressure in the hydraulic chamber is always higher than the pressure in the insulation chamber or the preload insulation chamber during two or more hydraulic pressure generation cycles.
従って液圧室6に燃焼廃ガスなどの気体が浸入すること
は防止できる。また本発明の液圧発生装置では、燃焼室
4と液圧室6が断熱室又は予圧断熱室6によって隔離さ
れているため燃焼発熱の液圧室への伝熱を抑制すること
ができる。従って液圧媒体中に気体が浸入又は発生する
のを防ぐことができる。Therefore, it is possible to prevent gases such as combustion waste gas from entering the hydraulic chamber 6. Further, in the hydraulic pressure generating device of the present invention, since the combustion chamber 4 and the hydraulic pressure chamber 6 are isolated by the heat insulation chamber or the preload insulation chamber 6, heat transfer of combustion heat to the hydraulic pressure chamber can be suppressed. It is therefore possible to prevent gas from entering or forming into the hydraulic medium.
本発明の液圧発生装置は好ましくは第2図に示すように
、一体的に往復運動する一対のピストン1.2により中
間で内径の異なるシリンダ3内を3分割し、端から順に
大内径側に2ストロ一ク句に燃料を燃焼する燃焼室4と
、内径が変化する位置に燃料混合気を吸入して予圧し、
かつ燃焼室4からの伝熱を遮る予圧断熱室5と、小内径
側に液体を高圧にする液圧室6とにより構成い 燃焼室
4には燃料混合気に点火する点火プラグ7とピストン下
限位置で開口し燃料混合気を予圧断熱室5から導入する
掃気孔8と、ピストン下降時に掃気孔8よりも先に開口
して燃焼廃ガスを排気する排気孔9とを装備し、予圧断
熱室5には燃料混合気をキャブレタから導入する燃料混
合気導入孔10と燃焼室4へ燃料混合気を圧送する燃料
混合気排出孔11とを装備するように構成する。この装
置の予圧断熱室5内ではシリンダ内径の差により。Preferably, as shown in FIG. 2, the hydraulic pressure generating device of the present invention divides the inside of the cylinder 3 into three parts having different inner diameters in the middle by a pair of pistons 1.2 that reciprocate integrally, and the inner diameter of the cylinder 3 is divided into three parts in order from the end to the larger inner diameter side. The combustion chamber 4 burns fuel in two-stroke strokes, and the fuel mixture is sucked into the position where the inner diameter changes to prepressurize it.
It also consists of a preload insulation chamber 5 that blocks heat transfer from the combustion chamber 4, and a hydraulic pressure chamber 6 that makes liquid under high pressure on the small inner diameter side.The combustion chamber 4 has a spark plug 7 that ignites the fuel mixture and a piston lower limit. The preload insulation chamber is equipped with a scavenging hole 8 that opens at a position to introduce the fuel mixture from the preload insulation chamber 5, and an exhaust hole 9 that opens before the scavenge hole 8 when the piston descends and exhausts combustion waste gas. 5 is equipped with a fuel mixture introduction hole 10 for introducing the fuel mixture from the carburetor and a fuel mixture discharge hole 11 for pressure-feeding the fuel mixture to the combustion chamber 4. Due to the difference in cylinder inner diameter within the preload insulation chamber 5 of this device.
ピストン1,2が上昇中には容積が増加し、ピストンが
下降中には容積が減少するので、ピストンが上昇中には
燃料混合気を燃料混合気導入孔10を経て予圧断熱室5
内に吸引し、ピストンが下降中には燃料混合気を圧縮加
圧して、燃料混合気排出孔11を経てピストン下限位置
で開口する掃気孔8から燃焼室4内に燃料混合気を噴射
することができる。第2図に示す装置は掃気孔8と排気
孔9を装備する2サイクルエンジンの例であるが。When the pistons 1 and 2 are rising, the volume increases, and when the pistons are falling, the volume decreases. Therefore, while the pistons are rising, the fuel mixture is passed through the fuel mixture introduction hole 10 to the preload insulation chamber 5.
While the piston is moving downward, the fuel mixture is compressed and pressurized, and the fuel mixture is injected into the combustion chamber 4 from the scavenging hole 8 that opens at the lower limit position of the piston via the fuel mixture discharge hole 11. Can be done. The device shown in FIG. 2 is an example of a two-stroke engine equipped with a scavenging hole 8 and an exhaust hole 9.
これに第1図に示す吸気弁と排気弁を付は加えることが
でき、ガソリンやLPGやLNGを燃料とするが9点火
プラグ7の代わりに燃料噴射ノズルを用いて灯油や前記
の燃料を噴射することもできる。第2図の装置の燃焼室
4ではピストンlが同図の様に下限にある時に、排気孔
9が開口し、これより僅かに遅れて掃気孔8が間口する
。第2図の装置に排気弁と吸気弁を付は加える場合には
。The intake valve and exhaust valve shown in Fig. 1 can be added to this, and gasoline, LPG, or LNG is used as fuel, but instead of the spark plug 7, a fuel injection nozzle is used to inject kerosene or the above-mentioned fuel. You can also. In the combustion chamber 4 of the apparatus shown in FIG. 2, the exhaust hole 9 opens when the piston 1 is at the lower limit as shown in the figure, and the scavenging hole 8 opens slightly later than this. When adding or adding an exhaust valve and an intake valve to the device shown in Figure 2.
ピストンの位置によって自動的に開閉する掃気孔と排気
孔のの開閉に同調して排気弁8を開いて燃焼廃ガスを排
気し、これより僅かに遅れて吸気弁8を開いて加圧した
燃料混合気により掃気して燃焼廃ガスを追い出すと共に
燃焼室内に燃料混合気を充満させたのち、排気弁と吸気
弁を閉じる。続けて液圧源18から逆止め弁を経て液圧
室6に低圧の液体を圧入してシリンダ2を押し上げて燃
焼室内の燃料合気を圧縮い 点火プラグ7により燃料に
点火し燃焼させ、燃焼室4内を高圧にしてピストン1.
2を一体的に押し下げ液圧室に於て液体を高圧にし、
圧力液体流出配管14の逆止め弁16を押し開く、制御
弁15の少なくとも一つは内部パイロット圧により開閉
する圧力制御弁が良く、この設定圧力よりも液圧が高い
間はこれを経由してアキュムレータ17に蓄える。その
他の制御弁は点火からの時間経過又は液圧室の圧力又は
ピストン1,2の位置を検出してこれを信号とし。The exhaust valve 8 is opened in synchronization with the opening and closing of the scavenging and exhaust holes, which automatically open and close depending on the position of the piston, to exhaust combustion waste gas, and the intake valve 8 is opened slightly later than this to exhaust the pressurized fuel. After scavenging with the mixture to expel combustion waste gas and filling the combustion chamber with the fuel mixture, the exhaust valve and intake valve are closed. Next, low-pressure liquid is injected from the hydraulic pressure source 18 into the hydraulic pressure chamber 6 through the check valve, pushing up the cylinder 2 and compressing the fuel air in the combustion chamber.The fuel is ignited by the spark plug 7 and combusted. The pressure inside the chamber 4 is high and the piston 1.
2 is pushed down integrally to make the liquid high pressure in the hydraulic pressure chamber,
At least one of the control valves 15 that pushes open the check valve 16 of the pressure liquid outflow pipe 14 is preferably a pressure control valve that opens and closes using internal pilot pressure. It is stored in the accumulator 17. Other control valves detect the passage of time from ignition, the pressure in the hydraulic chamber, or the positions of the pistons 1 and 2, and use this as a signal.
パイロット圧を操作して開閉するシーケンス弁が良い、
液圧室の圧力はピストンが下降中は時間の経過と共に低
下する傾向にあり、従って後で開く制御弁はど低圧の液
体を通し、アキュムレータに圧力媒体を蓄えることにな
る。A sequence valve that opens and closes by controlling pilot pressure is good.
The pressure in the hydraulic chamber tends to decrease over time during the downward movement of the piston, so that the control valve that opens later will pass lower pressure liquid and store pressure medium in the accumulator.
本発明の液圧発生装置は第3図や第4図に示す様に、複
数のシリンダを対向させるのが良い、第3図の例では、
一体的に往復運動する一対のピストンIA、2Aにより
各々のシリンダ3A、3B内を3分割し、端から順に燃
料を燃焼する燃焼室4A、4Bと、燃焼室からの伝熱を
遮る予圧断熱室5A、5Bと、1体を高圧にする液圧室
6A。The hydraulic pressure generating device of the present invention preferably has a plurality of cylinders facing each other as shown in FIGS. 3 and 4. In the example shown in FIG.
Each cylinder 3A, 3B is divided into three by a pair of pistons IA, 2A that reciprocate integrally, and combustion chambers 4A, 4B burn fuel sequentially from the end, and a preload insulation chamber blocks heat transfer from the combustion chamber. 5A, 5B, and a hydraulic chamber 6A that makes one body high pressure.
6Bとにより構成し、この様な液圧発生装置対のピスト
ンロッド12を液圧室側において連結し。6B, and the piston rods 12 of such a pair of hydraulic pressure generators are connected on the hydraulic pressure chamber side.
両側のピストンを一体的に往復運動させる。この場合に
は燃焼室内の燃料混合気の圧縮は、対向する燃焼室内の
燃料Φ燃焼膨張力によって行か 第3図に示した装置は
2ストロークエンジンの例であり、この場合にも第2図
の例で述べたと同じ様な用い方ができる。第4図に示し
た装置は4ストロークエンジンの例であり、4本のシリ
ンダの燃焼室が順次、吸入、圧縮、燃焼、排気の4工程
をとる点が、前記の説明と異なる点である1例えば第4
図において燃焼室4Aで吸入工程が完了せんとする時、
燃焼室4Bでは圧縮工程が完了せんとしており、燃焼室
4Cでは燃焼工程が完了せんとしており、燃焼室4Dで
は排気工程が完了せんとしている。The pistons on both sides reciprocate integrally. In this case, the fuel mixture in the combustion chamber is compressed by the combustion expansion force of the fuel Φ in the opposing combustion chamber. It can be used in the same way as described in the example. The device shown in Fig. 4 is an example of a four-stroke engine, and differs from the above explanation in that the combustion chambers of the four cylinders sequentially undergo four steps: suction, compression, combustion, and exhaust. For example, the fourth
In the figure, when the intake process is about to be completed in the combustion chamber 4A,
The compression process is about to be completed in the combustion chamber 4B, the combustion process is about to be completed in the combustion chamber 4C, and the exhaust process is about to be completed in the combustion chamber 4D.
本発明の液圧発生装置は液圧室6に逆止め機構付き液体
流入配管13と逆止め機構付き圧力液体流出配管14と
を連結し、圧力液体流出配管には異なる圧力で作動する
複数の圧力制御弁15と。The hydraulic pressure generating device of the present invention connects a liquid inflow pipe 13 with a non-return mechanism and a pressure liquid outflow pipe 14 with a non-return mechanism to a liquid pressure chamber 6, and the pressure liquid outflow pipe has a plurality of pressures operating at different pressures. and a control valve 15.
それぞれの圧力制御弁の後にアキュムレータを連結する
ことが望ましい1本発明装置に於て、液圧室に内で高圧
になった液体は、圧力液体流出配管14の逆止め弁16
を押し開く、制御弁15の少なくとも一つは内部パイロ
ット圧により開閉する圧力制御弁が良く、この設定圧力
よりも液圧が高い間はこれを経由してアキュムレータ1
7に蓄える。その他の制御弁は点火からの時間経過又は
液圧室の圧力又はピストン1,2の位置を検出してこれ
を信号とし、パイロット圧を操作して開閉するシーケン
ス弁が良い、液圧室の圧力はピストンが下降中は時間の
経過と共に低下する傾向にあり。In the device of the present invention, it is desirable to connect an accumulator after each pressure control valve, and the liquid that has become high pressure in the hydraulic chamber is discharged through the check valve 16 of the pressure liquid outflow pipe 14.
It is preferable that at least one of the control valves 15 is a pressure control valve that is opened and closed by internal pilot pressure, and that the accumulator 1 is
Store in 7. Other control valves should be sequence valves that detect the passage of time from ignition or the pressure in the hydraulic chamber or the position of pistons 1 and 2 and use this as a signal to open and close by manipulating the pilot pressure.The pressure in the hydraulic chamber tends to decrease over time while the piston is descending.
従って後で開く制御弁はど低圧の液体を通し、アキュム
レータに圧力媒体を蓄えることになる1以上のように構
成することによってピストンの下降にともなって次第に
低下する圧力を、高圧から低圧まで段階的に複数の液圧
媒体を取り出して蓄え。Therefore, by configuring one or more of the control valves, which open later, to pass the low-pressure liquid and store the pressure medium in the accumulator, the pressure that gradually decreases as the piston descends is gradually reduced from high pressure to low pressure. extracts and stores multiple hydraulic media.
エネルギ変換効率を向上させることができる。Energy conversion efficiency can be improved.
(発明の効果)
本発明の液圧発生装置によって前述の従来技術の問題点
が克服できる。すなはち本発明の液圧発生装置では内燃
機間での燃焼エネルギを直接的に液圧に変換できるため
にエネルギ変換効率が優れており、断熱室を設けること
によって液圧媒体中に燃焼廃ガスの混入を防ぎかつ液圧
媒体への伝熱を防ぐことができ、ざらに液圧室に複数の
圧力制御弁とそれに続くアキュムレータを燃焼熱の伝熱
により液圧媒体が昇温し気化するのを防ぐ液圧発生装置
を提供する接続することによってエネルギ変換効率を一
層向上させることができる。またシリンダ内径を中間で
異ならせることによって燃料混合気を予圧することや9
本発明の同種の装置を対向させてピストンロットを連結
して一体的に往復運動させることによって装置の運転を
容易にすることもできる。(Effects of the Invention) The problems of the prior art described above can be overcome by the hydraulic pressure generating device of the present invention. In other words, the hydraulic pressure generating device of the present invention has excellent energy conversion efficiency because it can directly convert combustion energy between internal combustion engines into hydraulic pressure, and by providing a heat insulating chamber, combustion waste gas is removed from the hydraulic medium. The hydraulic pressure chamber has multiple pressure control valves and the following accumulators, which prevent the hydraulic medium from heating up and vaporizing due to the transfer of combustion heat. The energy conversion efficiency can be further improved by connecting a hydraulic pressure generating device that prevents this from occurring. In addition, by making the inner diameter of the cylinder different in the middle, it is possible to prepress the fuel mixture.
It is also possible to facilitate the operation of the apparatus by arranging similar apparatuses of the present invention to face each other and connecting the piston rods so that they reciprocate integrally.
従来のエンジンの出力の効率が低い原因は、エンジンの
回転数が2000〜8000rpmと極めて高いために
、高温高圧のエネルギを十分に利用できずに廃ガスとし
て大気中に放出したことや、ピストンの往復運動をコン
ロッドとクランクシャフトによって回転運動に変換する
過程でのエネルギ損失が大きいことにあったが9本発明
の装置ではエンジンのピストン移動速度はエネルギ変換
が十分に行える程度に遅く、また燃料から液圧へのエネ
ルギ変換が直接的であり運動エネルギなどのエネルギ損
失が小さい。The reason for the low output efficiency of conventional engines is that the engine speed is extremely high (2000 to 8000 rpm), so the high temperature and high pressure energy cannot be fully utilized and is released into the atmosphere as waste gas, and the piston The energy loss in the process of converting reciprocating motion into rotary motion by the connecting rod and crankshaft was large.9 However, in the device of the present invention, the piston movement speed of the engine is slow enough to perform energy conversion, and the Energy conversion to hydraulic pressure is direct, and energy loss such as kinetic energy is small.
第1図ないし第4図は本発明装置の概念図であって、第
1図はシリンダの内径が等しい例、第2図はシリンダの
内径が異なる例、第3図は2本のシリンダを対向させた
例、第4図は本のシリンダを対向させた例である。
1、IA、1B、IC,ID:ピストン。
2.2A、2B、2C,2D:ピストン。
3.3A、3B、3C,3Dニジリンダ。
4.4A、4B、4C,4D:燃焼室。
5.5A、58.5C,50:断熱室、予圧断熱室。
6.6A、6B、6C,6D:液圧室。
?、7A、7B、VC,70:点火プラグ、燃料噴射ノ
ズル。
8.8A、88.8C,80:吸気弁、掃気孔。
9.9A、98.9C,9D:排気弁、排気孔。
10、IOA、IOB、IOC,100:燃料混合気導
入孔。
11、IIA、11B、IIC,110:燃料混合気排
出孔。
12.12A、12B、12C,120:ピストンロッ
ド。
3、+3A、13B、13C,+30:液体流人配管。
4.14A、14B、+4C,14D:圧力液体流出配
管。
5゜15A、15B、+5C,!5D:圧力制御弁、シ
ーケンス弁。
6.16A、16B、16C,!6D:逆止め弁。
7:アキュムレータ。Figures 1 to 4 are conceptual diagrams of the device of the present invention, in which Figure 1 shows an example in which the cylinders have the same inner diameter, Figure 2 shows an example in which the cylinders have different inner diameters, and Figure 3 shows two cylinders facing each other. FIG. 4 shows an example in which the book cylinders are placed opposite each other. 1, IA, 1B, IC, ID: Piston. 2.2A, 2B, 2C, 2D: Piston. 3.3A, 3B, 3C, 3D Niji Linda. 4.4A, 4B, 4C, 4D: Combustion chamber. 5.5A, 58.5C, 50: insulation chamber, preload insulation chamber. 6.6A, 6B, 6C, 6D: Hydraulic pressure chamber. ? , 7A, 7B, VC, 70: Spark plug, fuel injection nozzle. 8.8A, 88.8C, 80: Intake valve, scavenging hole. 9.9A, 98.9C, 9D: Exhaust valve, exhaust hole. 10, IOA, IOB, IOC, 100: Fuel mixture introduction hole. 11, IIA, 11B, IIC, 110: Fuel mixture discharge hole. 12.12A, 12B, 12C, 120: Piston rod. 3, +3A, 13B, 13C, +30: Liquid flow pipe. 4.14A, 14B, +4C, 14D: Pressure liquid outflow piping. 5゜15A, 15B, +5C,! 5D: Pressure control valve, sequence valve. 6.16A, 16B, 16C,! 6D: Check valve. 7: Accumulator.
Claims (1)
ダ内を3分割し、端から順に燃料を燃焼する燃焼室と、
燃焼室からの伝熱を遮る断熱室と、液体を高圧にする液
圧室とにより構成することを特徴とする液圧発生装置。 2、一体的に往復運動する一対のピストンにより中間で
内径の異なるシリンダ内を3分割し、端から順に大内径
側に2ストローク毎に燃料を燃焼する燃焼室と、内径が
変化する位置に燃料混合気を吸入して予圧し、かつ燃焼
室からの伝熱を遮る予圧断熱室と、小内径側に液体を高
圧にする液圧室とにより構成し、燃焼室には燃料混合気
に点火する点火プラグとピストン下限位置で開口し燃料
混合気を予圧断熱室から導入する掃気孔と、ピストン下
降時に掃気孔よりも先に開口して燃焼廃ガスを排気する
排気孔とを装備し、予圧断熱室には燃料混合気をキャブ
レタから導入する燃料混合気導入孔と燃焼室へ燃料混合
気を圧送する燃料混合気排出孔とを装備することを特徴
とする液圧発生装置。 3、一体的に往復運動する一対のピストンによりシリン
ダ内を3分割し、端から順に燃料を燃焼する燃焼室と、
燃焼室からの伝熱を遮る断熱室と、液体を高圧にする液
圧室とにより構成し、この様な液圧発生装置対のピスト
ンロッドを液圧室側において連結し、ピストンを一体的
に往復運動させることを特徴とする液圧発生装置。 4、液圧室に逆止め機構付き液体流入配管と逆止め機構
付き圧力液体流出配管とを連結し、圧力液体流出配管に
は異なる圧力で作動する複数の圧力制御弁と、それぞれ
の圧力制御弁の後にアキュムレータを連結することを特
徴とする請求項1ないし3のいずれかに記載する液圧発
生装置。[Claims] 1. A combustion chamber that divides the inside of the cylinder into three parts by a pair of pistons that reciprocate integrally and burns fuel sequentially from the end;
A hydraulic pressure generator characterized by comprising an insulating chamber that blocks heat transfer from a combustion chamber and a hydraulic chamber that pressurizes a liquid. 2. A pair of pistons that reciprocate integrally divides the inside of the cylinder into three parts with different inner diameters in the middle, and a combustion chamber that burns fuel every two strokes from the end to the large inner diameter side, and a combustion chamber that burns fuel at the position where the inner diameter changes. Consists of a preload insulation chamber that sucks in and prepressurizes the mixture and blocks heat transfer from the combustion chamber, and a hydraulic pressure chamber that pressurizes the liquid on the small inner diameter side, and ignites the fuel mixture in the combustion chamber. Equipped with a scavenging hole that opens at the lower limit position of the spark plug and piston and introduces the fuel mixture from the preload insulation chamber, and an exhaust hole that opens before the scavenge hole when the piston descends to exhaust combustion waste gas. A hydraulic pressure generating device characterized in that a chamber is equipped with a fuel mixture introduction hole for introducing a fuel mixture from a carburetor and a fuel mixture discharge hole for pressure-feeding a fuel mixture to a combustion chamber. 3. A combustion chamber that divides the inside of the cylinder into three parts by a pair of pistons that reciprocate in unison, and burns fuel sequentially from the end;
It consists of an insulating chamber that blocks heat transfer from the combustion chamber and a hydraulic chamber that pressurizes the liquid.The piston rods of such a hydraulic pressure generating device pair are connected on the hydraulic pressure chamber side, and the piston is integrated. A hydraulic pressure generating device characterized by reciprocating motion. 4. A liquid inflow pipe with a non-return mechanism and a pressure liquid outflow pipe with a non-return mechanism are connected to the liquid pressure chamber, and the pressure liquid outflow pipe includes a plurality of pressure control valves that operate at different pressures, and each pressure control valve. 4. The hydraulic pressure generating device according to claim 1, wherein an accumulator is connected after the hydraulic pressure generating device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63298618A JPH02146271A (en) | 1988-11-27 | 1988-11-27 | Hydraulic pressure generating device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63298618A JPH02146271A (en) | 1988-11-27 | 1988-11-27 | Hydraulic pressure generating device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH02146271A true JPH02146271A (en) | 1990-06-05 |
Family
ID=17862060
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP63298618A Pending JPH02146271A (en) | 1988-11-27 | 1988-11-27 | Hydraulic pressure generating device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH02146271A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020160847A1 (en) * | 2019-02-08 | 2020-08-13 | Eaton Intelligent Power Limited | Pressure boost system |
-
1988
- 1988-11-27 JP JP63298618A patent/JPH02146271A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020160847A1 (en) * | 2019-02-08 | 2020-08-13 | Eaton Intelligent Power Limited | Pressure boost system |
| CN113439158A (en) * | 2019-02-08 | 2021-09-24 | 伊顿智能动力有限公司 | Supercharging system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| AU2011227527B2 (en) | Split-cycle engine with high residual expansion ratio | |
| US5103645A (en) | Internal combustion engine and method | |
| CN201826953U (en) | Two-stroke cylinder piston engine | |
| US6551076B2 (en) | Fuel/hydraulic engine system | |
| EP1992805A1 (en) | Reciprocating machine | |
| JP2010285977A (en) | Built-in compressor type six-stroke engine exclusive for hydrogen | |
| CN109469557B (en) | Self-adaptive compressed air continuous combustion piston engine | |
| US9175641B2 (en) | Multi-cycle stratified internal combustion system | |
| JPH02146271A (en) | Hydraulic pressure generating device | |
| WO2008092218A1 (en) | An internal combustion engine with extended stroke | |
| Jangalwa et al. | Scuderi split cycle engine: a review | |
| CN117328994B (en) | A two-stage combustion multi-stroke cycle system and method with controllable intake and exhaust valves | |
| US6244826B1 (en) | Gaseous piston method for suction and compression in closed chamber gas equipments | |
| CN113309594B (en) | Compressed air fuel engine | |
| CN203271950U (en) | Piston punching self-ignition pulse jet engine | |
| CN116608042A (en) | Two-stroke method for internal combustion engine | |
| KR100812558B1 (en) | A rating engine | |
| KR101129125B1 (en) | Gas mixture compressor | |
| CN104005846A (en) | Fuel-selectable piston type two-travel engine | |
| CN112065570A (en) | Plunger Homogeneous Compression Ignition Engine | |
| CN115263543A (en) | Engine and generator | |
| Ab Sota | Water Injection System Design for Six Stroke Engine | |
| CN111336009A (en) | Pressure explosion internal combustion type high-auxiliary transmission power generation mechanism | |
| CN103410622A (en) | KR gasoline internal combustion engine | |
| CN111828165A (en) | Piston screw HCCI engine |