CN106500950A - A kind of efficient large scale injection piping installation of air intake test - Google Patents

A kind of efficient large scale injection piping installation of air intake test Download PDF

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Publication number
CN106500950A
CN106500950A CN201611092602.XA CN201611092602A CN106500950A CN 106500950 A CN106500950 A CN 106500950A CN 201611092602 A CN201611092602 A CN 201611092602A CN 106500950 A CN106500950 A CN 106500950A
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CN
China
Prior art keywords
air intake
injector
effusion meter
stable section
wind
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
Application number
CN201611092602.XA
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Chinese (zh)
Inventor
李长坤
滕鹏
唐滨滨
李家宏
王玉琢
杜羽
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AVIC Aerodynamics Research Institute
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AVIC Aerodynamics Research Institute
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Filing date
Publication date
Application filed by AVIC Aerodynamics Research Institute filed Critical AVIC Aerodynamics Research Institute
Priority to CN201611092602.XA priority Critical patent/CN106500950A/en
Publication of CN106500950A publication Critical patent/CN106500950A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/02Wind tunnels
    • G01M9/04Details

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

A kind of efficient large scale injection piping installation of air intake test, belongs to wind-tunnel technique field, and the present invention does not reach air intake duct actual flow in order to solve the problems, such as to fully rely on wind-tunnel flowing punching press.After effusion meter, effusion meter, after diffuser, effusion meter, after stable section, flow control valve, regulating valve, after stable section, regulating valve, before diffuser, injector, stable section and injector are sequentially connected with, and be located on same axis, and path is formed, its overall pipeline is arranged on wind-tunnel center.A kind of efficient large scale injection piping installation of air intake test of the invention can produce the air intake duct necessary flow met installed in pipeline front end under the ejector action of high pressure gas, and air intake duct wind tunnel test can be made to realize that big flow is simulated.

Description

A kind of efficient large scale injection piping installation of air intake test
Technical field
The present invention relates to a kind of injection piping installation, and in particular to a kind of efficient large scale injection pipeline dress of air intake test Put, belong to wind-tunnel technique field.
Background technology
Air intake duct directly affects the cooperation of aircraft and engine as stream in aircraft and outflow interface unit, its performance Performance, air intake duct are designed by aircraft type unit, pay close attention to loss of the air intake duct under design discharge, steady dynamic distortion ginseng Number, stall margin etc., these parameters are general by wind tunnel test acquisition and checking in the airplane design stage, and air intake duct wind-tunnel is tried Test, generally the actual stream of air intake duct is not reached flowing punching press using without the independent air intake test mode of electromotor, fully relying on wind-tunnel Amount, simulating Flow Field In An Inlet, injector is used as a kind of fluid conveying being widely used in the draw inlet road that need to take measures Device, has more application in terms of simulation Flow Field In An Inlet, and in air intake duct wind tunnel test, injector is arranged in pipeline, Composition injection pipeline, produces the air intake duct necessary flow met installed in pipeline front end under the ejector action of high pressure gas;Existing Partial-air admission road test pipe-line system, by pipeline size limitation, flow simulation ability can not meet big flow air intake test Demand, if the whole wind-tunnel pipe-line system of transformation, will pay larger cost, aspiration will install effusion meter, Flow-rate adjustment in addition The devices such as valve, circuit design are slightly unreasonable, and line loss will be caused to be increased dramatically.Accordingly, it would be desirable to a kind of wind-tunnel air intake test Efficiently large scale injection piping installation, to meet air intake duct necessary flow, improves air intake test ability.
Content of the invention
It is an object of the invention to provide a kind of efficient large scale injection piping installation of air intake test, to solve because of air intake duct Underfed and the problem of big flow simulation test can not be carried out.
A kind of efficient large scale injection piping installation of air intake test includes diffuser, stream after effusion meter, effusion meter Stable section and injector before diffuser, injector after stable section, regulating valve after stable section, flow control valve, regulating valve after gauge;
Stable section, regulating valve after stable section, flow control valve, regulating valve after diffuser, effusion meter after effusion meter, effusion meter Before diffuser, injector, stable section and injector are sequentially connected with afterwards, and are located on same axis, and form path, its integral tube Road is arranged on wind-tunnel center.
Preferably:Effusion meter is connected with wind-tunnel air intake port pipeline.
Preferably:Injector is provided with high pressure connector, and injector is connected with high-pressure air source by high pressure connector.
The present invention is had the effect that compared with existing product:Air intake test simulation of flow field energy can be significantly improved Power, pipeline suction flow are big, and loss is little, has flow measurement and regulating power concurrently, does not destroy the original air intake duct pipe-line system of wind-tunnel.
Description of the drawings
Fig. 1 is a kind of front view figure of the efficient large scale injection piping installation of air intake test of the present invention;
Fig. 2 is the side view of Fig. 1.
In figure:After 1- effusion meters, 2- effusion meters, after diffuser, 3- effusion meters, stable section, 4- effusion meter regulating valves, 5- are adjusted Stable section, 8- injectors, 9- high pressure connectors before diffuser, 7- injectors after stable section, 6- regulating valves after valve.
Specific embodiment
The preferred embodiment of the present invention is elaborated below according to accompanying drawing.
As shown in Figure 1 to Figure 2, a kind of efficient large scale injection piping installation of air intake test of the present invention includes flowing Expand after stable section 5, regulating valve after stable section 3, flow control valve 4, regulating valve after diffuser 2, effusion meter after gauge 1, effusion meter Stable section 7 and injector 8 before scattered section 6, injector;
Stable after stable section 3, flow control valve 4, regulating valve after diffuser 2, effusion meter after the effusion meter 1, effusion meter After section 5, regulating valve, before diffuser 6, injector, stable section 7 and injector 8 are sequentially connected with, and are located on same axis, and are formed Path, its overall pipeline are arranged on wind-tunnel center, and effusion meter 1 is connected on the pipeline of air channel air intake duct part, and injector 8 is connected with High-pressure air source, high pressure gas expand to form supersonic airstream through injector nozzle, injection air intake duct low-pressure air current, enter after mixing In wind-tunnel diffuser, and then the purpose for simulating Flow Field In An Inlet is reached, can be to pipeline by effusion meter 1 and flow control valve 4 Interior air-flow flow is measured and regulation.
Further:The efficient large scale injection piping installation of air intake test of the invention substantially increases the examination of air intake duct wind-tunnel The analog capability of flow field is tested, maximum outside diameter 458mm, maximum analog flow bring up to 3.2kg/s, this device pipe from 1.8kg/s The optimized modular design of road rectifying part, line loss are little, and induction efficiency improved 0.12 more originally, this piping installation be applied to into Stable in air flue wind tunnel test, install, it is convenient to dismantle.
Further:Injector 8 is provided with high pressure connector 9, and injector 8 is connected with high-pressure air source by high pressure connector 9.
Present embodiment is the exemplary illustration to this patent, does not limit its protection domain, people in the art Member can also be locally changed to which, as long as no the spirit beyond this patent, all in the protection domain of this patent.

Claims (3)

1. the efficient large scale injection piping installation of a kind of air intake test, it is characterised in that:After including effusion meter (1), effusion meter Diffuser after stable section (5), regulating valve after stable section (3), flow control valve (4), regulating valve after diffuser (2), effusion meter (6), stable section (7) and injector (8) before injector;
Behind effusion meter (1), effusion meter after diffuser (2), effusion meter after stable section (3), flow control valve (4), regulating valve After stable section (5), regulating valve, before diffuser (6), injector, stable section (7) and injector (8) are sequentially connected with, and are located at same axle On line, and path is formed, its overall pipeline is arranged on wind-tunnel center.
2. the efficient large scale injection piping installation of a kind of air intake test according to claim 1, it is characterised in that:Flow Meter (1) is connected with wind-tunnel air intake port pipeline.
3. the efficient large scale injection piping installation of a kind of air intake test according to claim 1 and 2, it is characterised in that: Injector (8) is provided with high pressure connector (9), and injector (8) is connected with high-pressure air source by high pressure connector (9).
CN201611092602.XA 2016-12-02 2016-12-02 A kind of efficient large scale injection piping installation of air intake test Pending CN106500950A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611092602.XA CN106500950A (en) 2016-12-02 2016-12-02 A kind of efficient large scale injection piping installation of air intake test

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611092602.XA CN106500950A (en) 2016-12-02 2016-12-02 A kind of efficient large scale injection piping installation of air intake test

Publications (1)

Publication Number Publication Date
CN106500950A true CN106500950A (en) 2017-03-15

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CN201611092602.XA Pending CN106500950A (en) 2016-12-02 2016-12-02 A kind of efficient large scale injection piping installation of air intake test

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111855132A (en) * 2020-08-28 2020-10-30 中国航空工业集团公司沈阳空气动力研究所 Flutter test safety protection system and method
CN113945355A (en) * 2021-09-21 2022-01-18 中国航空工业集团公司西安飞机设计研究所 Air inlet duct wind tunnel test simulation system under shock wave
CN117329740A (en) * 2023-11-29 2024-01-02 中国航空工业集团公司金城南京机电液压工程研究中心 Injection assembly and aircraft thermal management system

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CN206192621U (en) * 2016-12-02 2017-05-24 中国航空工业集团公司哈尔滨空气动力研究所 Experimental high -efficient jumbo size of intake duct is drawn and is penetrated piping installation

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CN103499447A (en) * 2013-10-09 2014-01-08 北京动力机械研究所 Zero mach number testing device applied to turbine engine
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CN204495535U (en) * 2015-03-20 2015-07-22 中国航天空气动力技术研究院 1.2 meters of magnitude wind-tunnel represent dynamically injectors
CN104848904A (en) * 2015-06-05 2015-08-19 中国航天空气动力技术研究院 Air duct flow measuring system
CN105628331A (en) * 2015-12-28 2016-06-01 中国航天空气动力技术研究院 Energy-saving environment-friendly layout of large-scale routine hypersonic wind tunnel
CN206192621U (en) * 2016-12-02 2017-05-24 中国航空工业集团公司哈尔滨空气动力研究所 Experimental high -efficient jumbo size of intake duct is drawn and is penetrated piping installation

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111855132A (en) * 2020-08-28 2020-10-30 中国航空工业集团公司沈阳空气动力研究所 Flutter test safety protection system and method
CN113945355A (en) * 2021-09-21 2022-01-18 中国航空工业集团公司西安飞机设计研究所 Air inlet duct wind tunnel test simulation system under shock wave
CN113945355B (en) * 2021-09-21 2024-01-30 中国航空工业集团公司西安飞机设计研究所 Air inlet channel wind tunnel test simulation system under shock wave
CN117329740A (en) * 2023-11-29 2024-01-02 中国航空工业集团公司金城南京机电液压工程研究中心 Injection assembly and aircraft thermal management system
CN117329740B (en) * 2023-11-29 2024-01-30 中国航空工业集团公司金城南京机电液压工程研究中心 Injection assembly and aircraft thermal management system

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Application publication date: 20170315