Air inlet and outlet connector device for annular radiator

An annular radiator and interface device technology, applied in the field of aircraft testing, can solve the problems of high use cost of the engine in the exhaust section, loss of test pieces, and long construction period, and achieve the effects of shortening the construction period, reliable performance and simple structure

Active Publication Date: 2021-03-09
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the actual flight of the aircraft, the air intake in the air inlet is huge, and it is often impossible to provide a matching air supply in the ground test environment
In addition, the configuration of the intake port is complex, and the engine in the exhaust section is expensive to use. Using the intake and exhaust interface scheme of a real aircraft has man

Method used

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  • Air inlet and outlet connector device for annular radiator
  • Air inlet and outlet connector device for annular radiator
  • Air inlet and outlet connector device for annular radiator

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Embodiment Construction

[0039] In order to make the purpose, technical solution and advantages of the application more clear, the technical solution in the embodiment of the application will be described in more detail below in conjunction with the drawings in the embodiment of the application.

[0040] In order to overcome the problems in the prior art, the present application provides an air intake and exhaust interface device for an annular radiator, which mainly includes: an air intake for simulating an air intake channel composed of an air intake inner cylinder 10 and an air intake outer cylinder 20 The interface assembly, the exhaust inner cylinder 30 and the exhaust outer cylinder 40 form the exhaust interface assembly for simulating the engine, the annular radiator is arranged between the air intake interface assembly and the exhaust interface assembly, and the air intake interface assembly and the exhaust The interface components are fixed by a positioning link 80 .

[0041] Such as figure ...

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Abstract

The invention provides an air inlet and outlet connector device for an annular radiator. The air inlet and outlet connector device comprises an air inlet connector assembly, an air outlet connector assembly and the annular radiator, the air inlet connector assembly comprises an air inlet inner barrel and an air inlet outer barrel, the air outlet connector assembly comprises an air outlet inner barrel and an air outlet outer barrel, the annular radiator is arranged between the air inlet connector assembly and the air outlet connector assembly, and the air inlet connector assembly and the air outlet connector assembly are fixed through a positioning connecting rod. According to the air inlet and outlet connector device for the annular radiator, the annular radiator can be rapidly replaced, the test environment building period is effectively shortened, the structure is simple, the performance is reliable, a movable connector is adopted, repeated utilization can be achieved, and the test requirement of the annular radiator is met at low cost.

Description

technical field [0001] The application belongs to the technical field of aircraft testing, and in particular relates to an air intake and exhaust interface device of an annular radiator. Background technique [0002] In the aircraft environmental control system, the contradiction between heat sink and heat dissipation is more prominent. As a section of the engine intake passage, the annular radiator can effectively use the cold resource of ram air and become an important part of the environmental control system. Therefore, a device with a matching annular radiator bleed air interface is required to ensure the normal operation of the system. [0003] The bleed air inlet of the annular radiator in the real aircraft is the aircraft intake, and the exhaust outlet is the engine. In the actual flight of the aircraft, the air intake in the air inlet is huge, and it is often impossible to provide a matching air supply in the ground test environment. Moreover, the configuration of ...

Claims

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Application Information

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IPC IPC(8): F28F9/26F28F11/02
CPCF28F9/262F28F11/02
Inventor 李春贺姜文宿可王冠男赵百玲
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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