TWI686589B - High resolution flow damping device - Google Patents
High resolution flow damping device Download PDFInfo
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- TWI686589B TWI686589B TW107143827A TW107143827A TWI686589B TW I686589 B TWI686589 B TW I686589B TW 107143827 A TW107143827 A TW 107143827A TW 107143827 A TW107143827 A TW 107143827A TW I686589 B TWI686589 B TW I686589B
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- 238000013016 damping Methods 0.000 title abstract 2
- 230000007246 mechanism Effects 0.000 claims abstract description 23
- 238000007789 sealing Methods 0.000 claims description 11
- 239000000758 substrate Substances 0.000 abstract 3
- 238000012360 testing method Methods 0.000 description 12
- 238000010586 diagram Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
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Abstract
Description
本發明是指一種高解析度阻流裝置,特別是指一種具有多個活塞可以精密控制風阻的阻流裝置。 The invention refers to a high-resolution choke device, in particular to a choke device with multiple pistons that can precisely control wind resistance.
目前,風扇在進行性能測試時需製作風量風壓PQ特性曲線,用以作為判斷該風扇性能的標準。請參閱圖1,圖1所繪示為一典型測試所得知的PQ曲線,所謂PQ曲線為經過風扇對空氣做功後之空氣靜壓(P)及出口之空氣流量(Q)所作之曲線,測試時主要控制量測儀器(以下簡稱風洞)之空氣流量進行量測。在傳統風洞中多使用只具有百頁擋板(louver)阻流裝置或單一活塞的阻流裝置以控制風洞中通過之空氣流量,但是上述的阻流裝置多無法兼顧風洞流量全量程及快速且精準控制通過風洞之空氣流量,造成拖慢測試效率,甚至無法達成目標量測流量點。因此,如何使風洞同時具有可量測空氣流量範圍廣泛及快速且精準的控制風洞之空氣流量的能力,以減少完成測試時間並增加測試效率是值得本領域具有通常知識者去思量的。 At present, the fan needs to make a PQ characteristic curve of air volume and air pressure when performing performance testing, which is used as a criterion for judging the performance of the fan. Please refer to FIG. 1. FIG. 1 shows a known PQ curve obtained by a typical test. The so-called PQ curve is the curve of the static air pressure (P) and the outlet air flow (Q) after the fan performs work on the air. The test The main control instrument (hereinafter referred to as wind tunnel) air flow measurement. In traditional wind tunnels, a louver baffle device or a single-piston choke device is often used to control the air flow through the wind tunnel, but many of the above choke devices cannot take into account the full range and speed of the wind tunnel flow. Precisely control the air flow through the wind tunnel, which will slow down the test efficiency and even fail to reach the target measurement flow point. Therefore, how to make the wind tunnel have the ability to measure the air flow in a wide range and quickly and accurately control the air flow of the wind tunnel to reduce the time to complete the test and increase the test efficiency is worth considering by those with ordinary knowledge in the art.
本發明之目的在於提供一種高解析度阻流裝置,控制空氣流量有很高的解析度且可以大幅提升測試效率。 The purpose of the present invention is to provide a high-resolution choke device that controls air flow with high resolution and can greatly improve test efficiency.
本發明之高解析度阻流裝置包括一層板、一上蓋及一活塞機構,其中該上蓋與該活塞機構設置於該層板上,該層板還包括一第一風口與一第二風口。該活塞機構包括一第一升降桿、一第二升降桿、一小活塞及一大活塞,其中該小活塞設置於該第一升降桿上,而該大活塞設置於該第二升降桿上,此外,該小活塞適於藉由該第一升降桿往該第一風口移動,該大活塞適於藉由該第二升降桿往該第二風口移動。在另一高解析度阻流裝置中,該第二風口不是設置於該層板上,而是設置於該大活塞上。 The high-resolution choke device of the present invention includes a layer plate, an upper cover, and a piston mechanism, wherein the upper cover and the piston mechanism are disposed on the layer plate, and the layer plate further includes a first tuyere and a second tuyere. The piston mechanism includes a first lifting rod, a second lifting rod, a small piston and a large piston, wherein the small piston is disposed on the first lifting rod, and the large piston is disposed on the second lifting rod, In addition, the small piston is suitable for moving to the first tuyere by the first lifting rod, and the large piston is suitable for moving to the second tuyere by the second lifting rod. In another high-resolution choke device, the second tuyere is not provided on the shelf, but on the large piston.
在上述之高解析度阻流裝置,還包括一第一環狀密封結構,用以讓該小活塞與該第一風口關閉時緊密接合,以及一第二環狀密封結構,用以讓該大活塞與該第二風口關閉時緊密接合。 The above-mentioned high-resolution choke device further includes a first annular sealing structure for tightly engaging the small piston with the first tuyere, and a second annular sealing structure for making the large The piston is tightly engaged when the second tuyere is closed.
在上述之另一高解析度阻流裝置,其中該大活塞的軸線與該小活塞的軸線相重合。 In another high-resolution choke device described above, the axis of the large piston coincides with the axis of the small piston.
在上述之兩種高解析度阻流裝置,其中大活塞數目為多個,小活塞數目為多個。 In the above two high-resolution choke devices, there are multiple large pistons and multiple small pistons.
100:高解析度阻流裝置 100: High-resolution choke device
102:上蓋 102: upper cover
104:層板 104: shelf
106:第一風口 106: The first tuyere
108:第二風口 108: Second tuyere
110:小活塞 110: small piston
112:大活塞 112: Big Piston
114:第二升降桿 114: Second lift lever
116:第一升降桿 116: The first lifting rod
118:活塞機構 118: Piston mechanism
200:高解析度阻流裝置 200: high-resolution choke device
202:上蓋 202: upper cover
204:層板 204: shelf
206:第一風口 206: The first tuyere
208:第二風口 208: Second tuyere
210:小活塞 210: small piston
212:大活塞 212: Big Piston
214:第二升降桿 214: The second lifting rod
216:第一升降桿 216: The first lifting rod
218:活塞機構 218: Piston mechanism
圖1所繪示為一典型測試所得知的PQ曲線。 Figure 1 shows a known PQ curve obtained from a typical test.
圖2所繪示為本實施例之高解析度阻流裝置100外觀。
FIG. 2 illustrates the appearance of the high-
圖3所繪示為本實施例之高解析度阻流裝置100內部構造。
FIG. 3 illustrates the internal structure of the high-
圖4A~4C所繪示為本實施例之高解析度阻流裝置100各階段做動狀態圖。
4A to 4C are diagrams illustrating the operation states of the high-
圖5所繪示為另一實施例之高解析度阻流裝置200外觀。
FIG. 5 illustrates the appearance of the high-
圖6所繪示為另一實施例之高解析度阻流裝置200內部構造。
FIG. 6 illustrates the internal structure of the high-
圖7A~7C所繪示為本實施例之高解析度阻流裝置200各階段做動狀態圖。
7A to 7C are diagrams illustrating the operation states of the high-
請參閱圖2及圖3,圖2所繪示為本實施例之高解析度阻流裝置100外觀,圖3所繪示為本實施例之高解析度阻流裝置100內部構造。高解析度阻流裝置100包括一上蓋102、一層板104及一活塞機構118。其中,活塞機構118包括一第一升降桿116、一第二升降桿114、一小活塞110及一大活塞112,而小活塞110是設置於第一升降桿116上,大活塞112是設置於第二升降桿上114。此外,上蓋102及活塞機構118皆設置於層板104之上,並與層板104緊密結合使空氣不會洩漏,其中層板104還包括一第一風口106及一第二風口108,第一風口106較小並設置有一第一環狀密封機構(未繪示)能與小活塞110做緊密結合使空氣不會洩漏,第二風口108較大並設置有一第二環狀密封結構(未繪示)能與大活塞112做緊密結合使空氣不會洩漏。在本實施例中,第一環狀密封機構與第二環狀密封結構例如為一環狀橡膠墊片或一環狀橡膠圓環。
Please refer to FIGS. 2 and 3. FIG. 2 illustrates the appearance of the high-
在本實施例中,以一個大活塞112、一個小活塞110、一第一風口106與一第二風口108為例,但在本領域具有通常知識者皆知,可以在高解析度阻流裝置100中再多增設更多的活塞和風口互相搭配,例如可以再多增設二個活塞與二個風口,且多增設的活塞與多增設的風口互相配合,且這些活塞和風口的大小也可以不同於本實施例中的大活塞112、小活塞110、第一風口106、與第二風口108。
In this embodiment, a
請參閱圖4A~4C,圖4A~4C所繪示為本實施例運作中的3種狀態,圖4A所繪示為第一風口106與第二風口108全開的狀態,小活塞110與大活塞112靠著第一升降桿116與第二升降桿114皆懸空收起,此狀態下空氣流量最大。圖4B所繪示
為第一風口106全開而第二風口108關閉的狀態,大活塞112透過第二升降桿114降下將第二風口108關閉,因此只剩下較小的第一風口106處於全開狀態以此降低空氣流量,之後靠著第一升降桿116控制小活塞110下降慢慢關閉第一風口106使空氣流量緩緩下降。圖4C所繪示為第一風口106與第二風口108全閉的狀態,此時小活塞110已靠著第一升降桿116下降到最後完全關閉第一風106口時,此狀態下空氣流量為零。在本實施例中,高解析度阻流裝置100可以透過移動不洞活塞來達成不同精準度空氣流量的控制,例如:高解析度阻流裝置100可以先行透過移動大活塞112來大幅度調整風洞之空氣流量,當到達目標空氣流量附近後,再讓大活塞112固定不動,只移動小活塞110來小幅度調整風洞之空氣流量。
Please refer to FIGS. 4A to 4C. FIGS. 4A to 4C illustrate three states in the operation of this embodiment. FIG. 4A illustrates the state in which the
請參閱圖5及圖6,圖5所繪示為另一實施例之高解析度阻流裝置200外觀,圖6所繪示為另一實施例之高解析度阻流裝置200內部構造。高解析度阻流裝置200包括一上蓋202、一層板204及一活塞機構218。其中,活塞機構218包括一第一升降桿216、一第二升降桿214、一小活塞210及一大活塞212,而小活塞210是設置於第一升降桿216上,大活塞212是設置於第二升降桿上214,其中小活塞210與大活塞212兩者中心軸線相重合。此外,上蓋202及活塞機構218皆設置於層板204之上,並與層板204緊密結合使空氣不會洩漏,其中層板204還包括一第二風口208,而大活塞212還包括一第一風口206。第一風口206較小並設置有一第一環狀密封機構(未繪示)能與小活塞210做緊密結合使空氣不會洩漏,第二風口208較大並設置有一第二環狀密封結構(未繪示)能與大活塞212做緊密結合使空氣不會洩漏。在本實施例中,第一環狀密封機構與第二環狀密封結構例如為一環狀橡膠墊片或一環狀橡膠圓環。
Please refer to FIGS. 5 and 6. FIG. 5 illustrates the appearance of the high-
在本實施例中,以一個大活塞212、一個小活塞210、一第一風口206與一第二風口208為例,但在本領域具有通常知識者皆知,可以在高解析度阻流裝置200中再多增設更多的活塞和風口互相搭配,例如可以再多增設二個活塞與二個風口,且多增設的活塞與多增設的風口互相配合,且這些活塞和風口的大小也可以不同於本實施例中的大活塞212、小活塞210、第一風口206、與第二風口208。
In this embodiment, a
請參閱圖7A~7C,圖7A~7C所繪示為本實施例運作中的3種狀態,圖7A所繪示為第一風口206與第二風口208全開的狀態,小活塞210與大活塞212靠著第一升降桿216與第二升降桿214皆懸空收起,此狀態下空氣流量最大。圖7B所繪示為第一風口206全開而第二風口208關閉的狀態,透過第二升降桿214降下大活塞212將第二風口208關閉,因此只剩設置於大活塞212上風口較小的第一風口206處於全開狀態,以此降低空氣流量,之後靠著第一升降桿216控制小活塞210下降慢慢關閉第一風口206使空氣流量緩緩下降。圖7C所繪示為第一風口206與第二風口208全閉的狀態,此時小活塞210已靠著第一升降桿216下降到最後完全關閉第一風口206時,此狀態下空氣流量為零。在本實施例中,高解析度阻流裝置200可以透過移動不洞活塞來達到不同空氣流量的精準度控制,例如:高解析度阻流裝置200可以先行透過移動大活塞212來大幅度調整風洞之空氣流量,當到達目標空氣流量附近後,大活塞212固定不動,只移動小活塞210來小幅度調整風洞之空氣流量。
Please refer to FIGS. 7A-7C. FIGS. 7A-7C illustrate three states in the operation of this embodiment. FIG. 7A depicts a state where the
綜上所述,可知本發明之高解析度阻流裝置,在進行測試時能使用單一風洞就能涵蓋測試整體大風量與小風量之量程範圍,不需測試中途更換風洞阻流裝置,進而減少完成測試所需時間增加測試效率。雖然本發明已以較佳實施例 揭露如上,然其並非用以限定本發明,任何所屬技術領域中具有通常知識者,在不脫離本發明之精神和範圍內,當可作些許之更動與潤飾,因此本發明之保護範圍當視後附之申請專利範圍所界定者為準。 In summary, it can be seen that the high-resolution choke device of the present invention can use a single wind tunnel to cover the range of the entire large and small air volume during the test, without replacing the wind tunnel choke device during the test, thereby reducing The time required to complete the test increases test efficiency. Although the present invention has The disclosure is as above, but it is not intended to limit the present invention. Any person with ordinary knowledge in the technical field can make some changes and modifications within the spirit and scope of the present invention, so the scope of protection of the present invention should be regarded as The scope of the attached patent application shall prevail.
200:高解析度阻流裝置 200: high-resolution choke device
206:第一風口 206: The first tuyere
208:第二風口 208: Second tuyere
210:小活塞 210: small piston
212:大活塞 212: Big Piston
214:第二升降桿 214: The second lifting rod
216:第一升降桿 216: The first lifting rod
218:活塞機構 218: Piston mechanism
Claims (6)
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| Application Number | Priority Date | Filing Date | Title |
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| TW107143827A TWI686589B (en) | 2018-12-06 | 2018-12-06 | High resolution flow damping device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW107143827A TWI686589B (en) | 2018-12-06 | 2018-12-06 | High resolution flow damping device |
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| Publication Number | Publication Date |
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| TWI686589B true TWI686589B (en) | 2020-03-01 |
| TW202022328A TW202022328A (en) | 2020-06-16 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI833464B (en) * | 2022-11-24 | 2024-02-21 | 長聖儀器股份有限公司 | Thermal resistance measurement results consistency device for cooling modules |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3068690A (en) * | 1958-04-11 | 1962-12-18 | North American Aviation Inc | Wind tunnel testing |
| US4372159A (en) * | 1981-06-17 | 1983-02-08 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Aeroelastic instability stoppers for wind tunnel models |
| TWM272983U (en) * | 2004-12-10 | 2005-08-11 | Yu Jia Technology Co Ltd | Wind channel aperture control device of wind tunnel testing apparatus |
| TWM283173U (en) * | 2005-04-20 | 2005-12-11 | Chien Entpr Co Ltd U | Wind tunnel testing device |
| TWM287433U (en) * | 2005-08-31 | 2006-02-11 | Chien Entpr Co Ltd U | Nozzle replacement structure for wind tunnel testing device |
-
2018
- 2018-12-06 TW TW107143827A patent/TWI686589B/en not_active IP Right Cessation
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3068690A (en) * | 1958-04-11 | 1962-12-18 | North American Aviation Inc | Wind tunnel testing |
| US4372159A (en) * | 1981-06-17 | 1983-02-08 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Aeroelastic instability stoppers for wind tunnel models |
| TWM272983U (en) * | 2004-12-10 | 2005-08-11 | Yu Jia Technology Co Ltd | Wind channel aperture control device of wind tunnel testing apparatus |
| TWM283173U (en) * | 2005-04-20 | 2005-12-11 | Chien Entpr Co Ltd U | Wind tunnel testing device |
| TWM287433U (en) * | 2005-08-31 | 2006-02-11 | Chien Entpr Co Ltd U | Nozzle replacement structure for wind tunnel testing device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI833464B (en) * | 2022-11-24 | 2024-02-21 | 長聖儀器股份有限公司 | Thermal resistance measurement results consistency device for cooling modules |
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| TW202022328A (en) | 2020-06-16 |
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