CN105781956A - Booster pump tester - Google Patents
Booster pump tester Download PDFInfo
- Publication number
- CN105781956A CN105781956A CN201610021567.6A CN201610021567A CN105781956A CN 105781956 A CN105781956 A CN 105781956A CN 201610021567 A CN201610021567 A CN 201610021567A CN 105781956 A CN105781956 A CN 105781956A
- Authority
- CN
- China
- Prior art keywords
- fuel tank
- booster pump
- fuel
- support body
- regulator valve
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B51/00—Testing machines, pumps, or pumping installations
Abstract
The invention belongs to finished product checking tools and relates to a booster pump tester. The booster pump tester is used for checking the performance of aircraft fuel oil booster pumps before installation. At present, special booster pump checking testers and the link of secondary inspection of booster pumps are lacked during inspection of the booster pumps in the aerospace field. The booster pump tester can ensure operation in a narrow and small space and can meet the precision requirement of force measuring. The forcemeter is small, exquisite, flexible, easy to operate and low in manufacturing cost.
Description
Technical field
The invention belongs to finished product checking tool, relate to a kind of booster pump exerciser, for the qualification before aircraft fuel oil booster pump is installed.
Background technology
At present, aviation field, when booster pump is detected, lacks special booster pump verification exerciser, booster pump lacks the link of secondary check.
Summary of the invention
The invention provides the exerciser checking that fuel oil increases pump performance.
A kind of fuel pressurization pump test machine, for the qualification before aircraft fuel oil booster pump is installed, including fuel tank, support body, pipeline, pressure regulator valve, effusion meter, Pressure gauge and bearing；Wherein said pressure regulator valve, effusion meter and Pressure gauge are arranged on support body；Described fuel tank is connected by bearing with support body, and fuel tank is turning structure, and fuel tank sidewall is oil-out, and top is oil return opening, and pipeline is flexible pipe, oil circuit path from the oil-out of fuel tank through pressure regulator valve, effusion meter and Pressure gauge to oil return opening；During test, booster pump is arranged on the lower surface of fuel tank.
Described fuel tank is rectangular structure, and there is fuel tank cap upper surface；It is welded to connect plate in fuel tank both sides to be connected by axle and lining with the bearing block on support body, it may be achieved the upset of fuel tank.
Before test, overturn fuel tank, booster pump is installed on fuel tank lower surface；Install, again overturn fuel tank, open fuel tank cap, to tank filling.
Described pressure regulator valve, effusion meter and Pressure gauge are arranged on the side of described support body, and during fuel tank upset, above-mentioned pressure regulator valve, effusion meter and Pressure gauge do not overturn together.
Beneficial effects of the present invention: fuel pressurization pump test machine of the present invention can ensure to operate at small space, can meet again the required precision of dynamometry.This ergometer is small and exquisite flexibly, simple to operate, cheap for manufacturing cost.
Accompanying drawing explanation
Fig. 1 is the schematic diagram of booster pump exerciser of the present invention.
Detailed description of the invention
The concrete structure of the present invention illustrates in conjunction with accompanying drawing 1.
A kind of fuel pressurization pump test machine, for the qualification before aircraft fuel oil booster pump is installed, including fuel tank 1, support body 2, pipeline 3, pressure regulator valve 4, effusion meter 5, Pressure gauge 6 and bearing 7；Wherein said pressure regulator valve 4, effusion meter 5 and Pressure gauge 6 are arranged on support body 2；Described fuel tank 1 and support body 2 is connected by bearing 7, and fuel tank 1 is turning structure, and fuel tank 1 sidewall is oil-out, and top is oil return opening, and pipeline 3 is flexible pipe, oil circuit path from the oil-out of fuel tank 1 through pressure regulator valve 4, effusion meter 5 and Pressure gauge 6 to oil return opening；During test, booster pump is arranged on the lower surface of fuel tank 1.
Described fuel tank 1 is rectangular structure, and there is fuel tank cap upper surface；It is welded to connect plate in fuel tank 1 both sides to be connected by axle and lining with the bearing block on support body 2, it may be achieved the upset of fuel tank.
Before test, overturn fuel tank 1, booster pump is installed on fuel tank lower surface；Installing, upset fuel tank 1, opens fuel tank cap, to tank filling again.
Described pressure regulator valve 4, effusion meter 5 and Pressure gauge 6 are arranged on the side of described support body 2, and during fuel tank upset, above-mentioned pressure regulator valve 4, effusion meter 5 and Pressure gauge 6 do not overturn together.
Claims (4)
1. a fuel pressurization pump test machine, for the qualification before aircraft fuel oil booster pump is installed, it is characterised in that: include fuel tank (1), support body (2), pipeline (3), pressure regulator valve (4), effusion meter (5), Pressure gauge (6) and bearing (7)；Wherein said pressure regulator valve (4), effusion meter (5) and Pressure gauge (6) are arranged on support body (2)；Described fuel tank (1) is connected by bearing (7) with support body (2), fuel tank (1) is turning structure, fuel tank (1) sidewall is oil-out, top is oil return opening, pipeline (3) is flexible pipe, oil circuit path from the oil-out of fuel tank (1) through pressure regulator valve (4), effusion meter (5) and Pressure gauge (6) to oil return opening；During test, booster pump is arranged on the lower surface of fuel tank (1).
2. fuel pressurization pump test machine according to claim 1, it is characterised in that: described fuel tank (1) is rectangular structure, and there is fuel tank cap upper surface；It is welded to connect plate in fuel tank (1) both sides to be connected by axle and lining with the bearing block on support body (2), it may be achieved the upset of fuel tank.
3. fuel pressurization pump test machine according to claim 2, it is characterised in that: before test, upset fuel tank (1), booster pump is installed on fuel tank lower surface；Install, again overturn fuel tank (1), open fuel tank cap, to tank filling.
4. fuel pressurization pump test machine according to claim 3, it is characterized in that: described pressure regulator valve (4), effusion meter (5) and Pressure gauge (6) are arranged on the side of described support body (2), during fuel tank upset, above-mentioned pressure regulator valve (4), effusion meter (5) and Pressure gauge (6) do not overturn together.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610021567.6A CN105781956A (en) | 2016-01-13 | 2016-01-13 | Booster pump tester |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610021567.6A CN105781956A (en) | 2016-01-13 | 2016-01-13 | Booster pump tester |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105781956A true CN105781956A (en) | 2016-07-20 |
Family
ID=56402442
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610021567.6A Pending CN105781956A (en) | 2016-01-13 | 2016-01-13 | Booster pump tester |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105781956A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108443131A (en) * | 2018-01-26 | 2018-08-24 | 平高东芝（河南）开关零部件制造有限公司 | The experimental rig and test method of a kind of hydraulic operation mechanism parts |
| CN109580105A (en) * | 2018-12-20 | 2019-04-05 | 中国航空工业集团公司金城南京机电液压工程研究中心 | A kind of reversed leakage test process unit |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201531405U (en) * | 2009-10-21 | 2010-07-21 | 湖南机油泵股份有限公司 | Oil pump analogue flow test device |
| CN201568280U (en) * | 2009-11-10 | 2010-09-01 | 江西洪都航空工业集团有限责任公司 | Miniaturized testing device for oil fuel booster pump of aircraft |
| CN201891592U (en) * | 2010-12-10 | 2011-07-06 | 湖南机油泵股份有限公司 | Engine oil pump detection system |
| CN102192065A (en) * | 2010-03-18 | 2011-09-21 | 上海航新航宇机械技术有限公司 | Device for detecting function of oil fuel booster pump of civil aircraft |
| CN202597053U (en) * | 2012-05-29 | 2012-12-12 | 合肥今典机械科技有限公司 | Delivery performance and life test device system for gear oil pump |
| CN202946361U (en) * | 2012-11-27 | 2013-05-22 | 芜湖亚奇汽车部件有限公司 | Fuel tank turning detecting experiment table |
| CN203011634U (en) * | 2012-11-28 | 2013-06-19 | 江苏东方汽车装饰件总厂 | Overturn testing machine for fuel tank |
-
2016
- 2016-01-13 CN CN201610021567.6A patent/CN105781956A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201531405U (en) * | 2009-10-21 | 2010-07-21 | 湖南机油泵股份有限公司 | Oil pump analogue flow test device |
| CN201568280U (en) * | 2009-11-10 | 2010-09-01 | 江西洪都航空工业集团有限责任公司 | Miniaturized testing device for oil fuel booster pump of aircraft |
| CN102192065A (en) * | 2010-03-18 | 2011-09-21 | 上海航新航宇机械技术有限公司 | Device for detecting function of oil fuel booster pump of civil aircraft |
| CN201891592U (en) * | 2010-12-10 | 2011-07-06 | 湖南机油泵股份有限公司 | Engine oil pump detection system |
| CN202597053U (en) * | 2012-05-29 | 2012-12-12 | 合肥今典机械科技有限公司 | Delivery performance and life test device system for gear oil pump |
| CN202946361U (en) * | 2012-11-27 | 2013-05-22 | 芜湖亚奇汽车部件有限公司 | Fuel tank turning detecting experiment table |
| CN203011634U (en) * | 2012-11-28 | 2013-06-19 | 江苏东方汽车装饰件总厂 | Overturn testing machine for fuel tank |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108443131A (en) * | 2018-01-26 | 2018-08-24 | 平高东芝（河南）开关零部件制造有限公司 | The experimental rig and test method of a kind of hydraulic operation mechanism parts |
| CN108443131B (en) * | 2018-01-26 | 2020-04-28 | 平高东芝（河南）开关零部件制造有限公司 | Testing device and testing method for oil pressure operating mechanism parts |
| CN109580105A (en) * | 2018-12-20 | 2019-04-05 | 中国航空工业集团公司金城南京机电液压工程研究中心 | A kind of reversed leakage test process unit |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101566527B (en) | Hydraulic control unit performance test station for stability control system in vehicle dynamics | |
| CN103267620B (en) | Testing device for functional characteristic test of valve | |
| CN105781956A (en) | Booster pump tester | |
| CN104034490A (en) | Insulator water-pressure tightness test device | |
| CN103616130B (en) | Pressure transducer proving installation | |
| CN205424078U (en) | Quick detecting system of axial deformation of butterfly valve valve plate | |
| CN209043562U (en) | A kind of fuel tank vibration test tooling | |
| CN103604565A (en) | Hydraulic seal and hydraulic movement testing device for aero-engine assembly field | |
| CN203551197U (en) | Pressure sensor test device | |
| CN204064588U (en) | Insulator water pressure air tightness tester | |
| CN202494561U (en) | Portable safety valve calibrator | |
| CN201819774U (en) | Fuel hose sealing performance testing device | |
| CN201339205Y (en) | Pile body self-reflection force balance loading box | |
| CN103091051A (en) | Leakage test device for oil bottom shell | |
| CN204116060U (en) | Train pressurized cylinder test fixture | |
| CN204387652U (en) | A kind of roller-mill bearing lubricating oil path detection device | |
| CN202560697U (en) | Device for detecting direct-acting relief valve and pilot relief valve of engineering mechanical hydraulic system | |
| CN104236831A (en) | Ramjet random vibration test fault diagnosis method | |
| CN204359424U (en) | Head tank Weighing module precision checking device | |
| CN204575141U (en) | Non-return valve flow detector | |
| CN207502188U (en) | Fuel tank of vehicle mechanical robustness testing platform | |
| CN102297643B (en) | Hole position detection combined structure | |
| CN201636133U (en) | Helicopter hydraulic system debugging device | |
| CN205423131U (en) | Experimental device for measure reverse sealing performance of pump case body | |
| CN202074907U (en) | Hole position degree detection composite structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160720 |