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Loading device for load calibration test of engine hanging installation joint

A technology for installing joints and loading devices, which is used in engine testing, measuring devices, and testing of machine/structural components. It can solve problems such as large load loading of difficult-to-engine rear suspension joints, and achieve the effect of improving test safety.

Active Publication Date: 2022-07-29
国机集团北京飞机强度研究所有限公司
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Problems solved by technology

[0005] In view of this, the purpose of the present invention is to overcome the deficiencies in the prior art above, and propose a load calibration test loading device for the engine suspension installation joint, so as to solve the difficulty in the prior art for the main suspension joint and the rear suspension joint of a certain type of engine. The problem with large payloads

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  • Loading device for load calibration test of engine hanging installation joint
  • Loading device for load calibration test of engine hanging installation joint
  • Loading device for load calibration test of engine hanging installation joint

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Embodiment Construction

[0030] The present invention will be further described below with reference to the accompanying drawings and specific embodiments.

[0031] see figure 2 and image 3 , the embodiment of the present invention provides a loading device suitable for the load calibration of the main suspension joint and the rear suspension joint of a certain type of aircraft. The test device includes: a hollow rectangular tube structure 8, a main suspension vertical loading assembly 39 , the main suspension heading loading assembly 40, the rear suspension aviation loading assembly, the rear suspension vertical loading assembly, and the front brace restraint assembly.

[0032] The bottom of the hollow rectangular tube structure 8 is welded by a horizontal rectangular long tube and two short tubes intersecting with the rectangular long tube. Two single-ear joints are welded above the short tubes for connecting the main suspension joints vertically. Loading assembly 39; a steel plate is welded at ...

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Abstract

The embodiment of the present invention provides a load calibration test loading device for an engine suspension installation joint, which relates to the technical field of load calibration test loading devices, so as to solve the problem that it is difficult to load the main engine suspension joint and the rear suspension joint with large loads in the prior art. . The load calibration test loading device uses the strain electrical measurement method to measure their flight loads. The device can not only complete the heading and vertical loading calibration of the main suspension joints, but also apply restraint loads on the front support joints and rear support joints. On the suspension joint, the heading and vertical load calibration of the rear suspension joint can be completed, and the restraint load can be applied to the front brace joint and the main suspension joint, which saves a lot of economic cost, time cost and labor cost. The device of the invention has ingenious design, convenient installation and use, easy disassembly and assembly, and can meet the use requirements of multiple sites; the device of the invention can be realized by simple mechanical processing, and the cost is low.

Description

technical field [0001] The invention relates to the technical field of a load calibration test loading device, in particular to a load calibration test loading device for an engine hanging installation joint. Background technique [0002] The engine hanger installation joint is an important force transmission component on the wing. It is used to install the engine hanger (the engine compartment is connected below the hanger), and it is the hub that transmits the engine's gravity and thrust to the wing. A certain type of transport aircraft engine suspension installation joints are divided into front support joints, inner main suspension joints, outer main suspension joints, rear suspension joints, and side tie rod joints, such as figure 1 shown. The front brace joint and the side tie rod joint are connected to the engine suspension through intermediate tension and compression rods, and their loads can be obtained by measuring these intermediate tension and compression rods. ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M15/02
CPCG01M15/02
Inventor 蓝洲远刘克格赵丽娜刘彦鹏韩小进段垚奇田兆锋
Owner 国机集团北京飞机强度研究所有限公司
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