CN102102687A - Hydraulic pressure source device - Google Patents
Hydraulic pressure source device Download PDFInfo
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- CN102102687A CN102102687A CN2009102609545A CN200910260954A CN102102687A CN 102102687 A CN102102687 A CN 102102687A CN 2009102609545 A CN2009102609545 A CN 2009102609545A CN 200910260954 A CN200910260954 A CN 200910260954A CN 102102687 A CN102102687 A CN 102102687A
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- Prior art keywords
- radiator
- type axial
- hydraulic pressure
- oil
- pressure source
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Abstract
The invention relates to a hydraulic pressure source device comprising an oil tank, a one-way valve, an oil filter, a safety valve, an oil returning filter, a swashplate-type axial plunger pump and a radiator, wherein the radiator, the oil returning filter, the oil tank, the swashplate-type axial plunger pump, the one-way valve and the oil filter are successively connected; the swashplate-type axial plunger pump is connected with the radiator; and the oil filter is connected with the radiator through the safety valve. Compared with the prior art, the hydraulic pressure source device has the advantages of stable working performance, long service life and the like.
Description
Technical field
The present invention relates to a kind of aircraft regular maintenance equipment, especially relate to a kind of hydraulic pressure source apparatus.
Background technique
YLY-2A type hydraulic pressure source apparatus, being mainly used to provides pressure and power supply for the hydraulic pressure detection ground installation of K8 aircraft inspection vehicle.These ground installations comprise hydraulic services multi-function test stand, pressurized strut test stand and equivalent coordination valve test stand.It can provide constant pressure and the alternating current 220V power supply of 25 ± 0.5MPa.
Original hydraulic pressure source apparatus uses ZB-34 oil pump heating value height, and noise is big.When detecting hydraulic services, under high pressure only 15 minutes, the oil temperature just up to 100 ℃ about.Have to quit work and work on again after wait oil temperature is cooled off.The process that has a strong impact on line service and make regular check on work is difficult to guarantee the rate of attendance of aircraft.If adopt the hydraulic pressure source apparatus of full import, not only cost an arm and a leg, and have the system matches problem.
Summary of the invention
Purpose of the present invention is exactly the hydraulic pressure source apparatus that a kind of stable work in work, long service life are provided for the defective that overcomes above-mentioned prior art existence.
Purpose of the present invention can be achieved through the following technical solutions:
A kind of hydraulic pressure source apparatus, this device comprises fuel tank, check valve, oily filter, safety valve, oil return filter, it is characterized in that, also comprise cam-type axial piston pump, radiator, described radiator, oil return filter, fuel tank, cam-type axial piston pump, check valve, oil filter connect successively, described cam-type axial piston pump is connected with radiator, and described oil filter is connected with radiator by safety valve.
Described cam-type axial piston pump is a variable displacement pump.
Described radiator is a fan-cooled radiator.
Compared with prior art, the present invention has the following advantages:
1, stable work in work, long service life;
2, noise is low;
3, temperature rise is low, but continuous operation.
Description of drawings
Fig. 1 is the structural representation of a kind of hydraulic pressure source apparatus of the present invention.
Embodiment
The present invention is described in detail below in conjunction with the drawings and specific embodiments.
Embodiment
As shown in Figure 1, a kind of hydraulic pressure source apparatus, this device comprises fuel tank 1, check valve 3, oil filter 4, safety valve 5, oil return filter 8, also comprise cam-type axial piston pump 2, radiator 7, described radiator 7, oil return filter 8, fuel tank 1, cam-type axial piston pump 2, check valve 3, oil filter 4 connect successively, described cam-type axial piston pump 2 is connected with radiator 7, and described oil filter 4 is connected with radiator 7 by safety valve 6.Described cam-type axial piston pump 2 is a variable displacement pump.
Add radiator 7 on the hydraulic pressure source apparatus oil circuit.This cam-type axial piston pump 2 is variable displacement pumps, and noise is low, pressure height, stable work in work, long service life.Outlet pressure is adjusted at 25.5 ± 0.5Mpa, after cam-type axial piston pump 2 starts, cam-type axial piston pump 2 with full flow 15L/min to system's fuel feeding, simultaneously also to high pressure accumulator 5 fuel feeding, when system pressure reaches the Set pressure of cam-type axial piston pump 2, high pressure oil promotes the control valve on the cam-type axial piston pump 2, the stroking mechanism of control valve operation cam-type axial piston pump 2, the output flow of cam-type axial piston pump 2 is reduced, when the output flow of cam-type axial piston pump 2 and system equate with oil mass, the stroking mechanism of cam-type axial piston pump 2 maintains a certain position, when system need increase or reduce when using oil mass, cam-type axial piston pump 2 can change output flow automatically, keeps system oil pressure.When high-pressure tightness was tested, the actual flow of cam-type axial piston pump 2 approached 0, so power consumption is very little, and temperature rise is little.Can guarantee to work long hours.
Add radiator 7 on the oil circuit of hydraulic pressure source apparatus, described radiator 7 is a fan-cooled radiator, just starts working once energising.Deep fat enters radiator 7, and radiator 7 inside are the copper conduit, and the surface has radiating fin to increase heat diffusion area, and through forced air cooling, oily temperature is minimized.Fluid is through the circulation cooling like this, and hydraulic system can reach a thermal equilibrium.Can guarantee long time continuous working.Actual test time continuous operation 8 hours, temperature is no more than 80 ℃, satisfies usage requirement.
Claims (3)
1. hydraulic pressure source apparatus, this device comprises fuel tank, check valve, oily filter, safety valve, oil return filter, it is characterized in that, also comprise cam-type axial piston pump, radiator, described radiator, oil return filter, fuel tank, cam-type axial piston pump, check valve, oil filter connect successively, described cam-type axial piston pump is connected with radiator, and described oil filter is connected with radiator by safety valve.
2. a kind of hydraulic pressure source apparatus according to claim 1 is characterized in that described cam-type axial piston pump is a variable displacement pump.
3. a kind of hydraulic pressure source apparatus according to claim 1 is characterized in that described radiator is a fan-cooled radiator.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009102609545A CN102102687A (en) | 2009-12-18 | 2009-12-18 | Hydraulic pressure source device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009102609545A CN102102687A (en) | 2009-12-18 | 2009-12-18 | Hydraulic pressure source device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102102687A true CN102102687A (en) | 2011-06-22 |
Family
ID=44155677
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009102609545A Pending CN102102687A (en) | 2009-12-18 | 2009-12-18 | Hydraulic pressure source device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102102687A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102410286A (en) * | 2011-11-08 | 2012-04-11 | 攀钢集团冶金工程技术有限公司 | Cooling system, hydraulic transmission system comprising same and vehicle |
| CN106586030A (en) * | 2017-02-20 | 2017-04-26 | 中国人民解放军海军航空工程学院青岛校区 | Flow equalizing coordination valve test table |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6026804A (en) * | 1983-07-22 | 1985-02-09 | Nissei Plastics Ind Co | Hydraulic equipment of injection molding machine |
| CN2278789Y (en) * | 1996-09-12 | 1998-04-15 | 中国第一拖拉机工程机械(集团)公司技术中心 | Hydraulic double-return loading device |
| CN201040701Y (en) * | 2007-04-20 | 2008-03-26 | 天津港第四港埠公司 | Fork lift hydraulic driving device |
| CN201582252U (en) * | 2009-12-18 | 2010-09-15 | 上海凯迪克航空工程技术有限公司 | Hydraulic pressure source device |
-
2009
- 2009-12-18 CN CN2009102609545A patent/CN102102687A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6026804A (en) * | 1983-07-22 | 1985-02-09 | Nissei Plastics Ind Co | Hydraulic equipment of injection molding machine |
| CN2278789Y (en) * | 1996-09-12 | 1998-04-15 | 中国第一拖拉机工程机械(集团)公司技术中心 | Hydraulic double-return loading device |
| CN201040701Y (en) * | 2007-04-20 | 2008-03-26 | 天津港第四港埠公司 | Fork lift hydraulic driving device |
| CN201582252U (en) * | 2009-12-18 | 2010-09-15 | 上海凯迪克航空工程技术有限公司 | Hydraulic pressure source device |
Non-Patent Citations (1)
| Title |
|---|
| 章宏甲等: "《液压传动》", 31 October 1997, 机械工业出版社 * |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102410286A (en) * | 2011-11-08 | 2012-04-11 | 攀钢集团冶金工程技术有限公司 | Cooling system, hydraulic transmission system comprising same and vehicle |
| CN102410286B (en) * | 2011-11-08 | 2014-05-21 | 攀钢集团工程技术有限公司 | Cooling system, hydraulic transmission system comprising same and vehicle |
| CN106586030A (en) * | 2017-02-20 | 2017-04-26 | 中国人民解放军海军航空工程学院青岛校区 | Flow equalizing coordination valve test table |
| CN106586030B (en) * | 2017-02-20 | 2023-10-24 | 中国人民解放军海军航空工程学院青岛校区 | Equivalent coordination valve test bench |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20110622 |
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| RJ01 | Rejection of invention patent application after publication |