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Auxiliary loading device for turbine engine casing rigidity test

A technology of turbine engine and loading device, which is applied in the direction of measuring device, machine/structural component testing, elastic testing, etc., can solve the problems of unsuitable aero-engine casing structure, etc., and achieve consistent parallelism and easy parallelism Effect

Active Publication Date: 2020-12-15
AECC COMML AIRCRAFT ENGINE CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] At present, there are relatively few auxiliary loading devices for stiffness tests, and they are not suitable for aero-engine case structures

Method used

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  • Auxiliary loading device for turbine engine casing rigidity test
  • Auxiliary loading device for turbine engine casing rigidity test
  • Auxiliary loading device for turbine engine casing rigidity test

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Embodiment Construction

[0026] The present invention will be further described below in conjunction with specific embodiment and accompanying drawing, set forth more details in the following description so as to fully understand the present invention, but the present invention can obviously be implemented in many other ways different from this description, Those skilled in the art can make similar promotions and deductions based on actual application situations without violating the connotation of the present invention, so the content of this specific embodiment should not limit the protection scope of the present invention.

[0027] It should be noted that the drawings are only examples, and they are not drawn according to the same scale, and should not be taken as limitations on the protection scope of the actual claims of the present invention.

[0028] Such as figure 1 , figure 2 As shown, the turbine engine casing rigidity test auxiliary loading device includes an upper transition section 2 co...

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Abstract

The invention aims at providing an auxiliary loading device of stiffness testing of a turbine engine case, thereby carrying out loading of tensile, bending, torsional stiffness tests. A loading disk has a loading center disposed coaxially with a tested case. The upper end of an upper transfer segment is connected to the loading disk and the lower end is connected to the upper end of the tested case. The upper end of a lower transfer segment is connected with the lower end of the tested case. A grounding disk is fixed on the base and is connected with the lower end of the lower transfer segment. A plurality of vertical actuating cylinders are arranged in a vertical direction; one end of each vertical actuating cylinder is connected to a vertical loading point of the loading disk; and the vertical loading points are distributed symmetrically around the loading center as the center. A plurality of horizontal actuating cylinders are arranged in a horizontal direction; one end of each horizontal actuating cylinder is connected to a horizontal loading point on the loading disk; the horizontal loading points are arranged in a diameter direction of the loading disk; one horizontal loadingpoint is arranged at the loading center; and the rest horizontal loading points are distributed symmetrically around the loading center as the center. A bracket beam is used for mounting the horizontal actuating cylinders.

Description

technical field [0001] The invention relates to a turbine engine test device, in particular to an auxiliary loading device for realizing the stiffness test of the turbine engine casing. Background technique [0002] Aeroengine stator casing is the skeleton of the engine. With the development of high speed and high thrust-to-weight ratio of aeroengine, the casing is mostly designed as a thin-walled cylindrical structure with weak rigidity. The rigidity of the casing has a great influence on the supporting stiffness of the rotor and the critical speed. The rigidity of the casing will also affect the layout of the vibration measuring points of the whole machine, etc., and with the development of finite element technology, the finite element analysis of components and the whole machine has been widely used in engineering practice, but it is necessary to test based on the stiffness characteristics The data is used to check and calibrate the finite element model, so it is necessar...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M5/00
CPCG01M5/005
Inventor 宋会英唐振南王少辉郑李鹏
Owner AECC COMML AIRCRAFT ENGINE CO LTD