Aircraft engine casing static test method and testing assembly thereof

An aero-engine and static test technology, applied in the field of aero-engine, can solve the problems of long test time and large gap, and achieve the effect of shortening the test period, reducing the cost of scientific research, and making the test conclusions more realistic and reliable.

Active Publication Date: 2011-04-20
CHINA HANGFA SOUTH IND CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] The present invention aims to provide a static test method for an aero-engine case, which can solve the technical problems of large gap between the test result and the real situation and long test time

Method used

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  • Aircraft engine casing static test method and testing assembly thereof
  • Aircraft engine casing static test method and testing assembly thereof
  • Aircraft engine casing static test method and testing assembly thereof

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Embodiment Construction

[0029] In addition to the objects, features and advantages described above, the present invention has other objects, features and advantages. The invention will be described in further detail below with reference to the accompanying drawings, but the invention can be implemented in many different ways as defined and covered by the claims.

[0030] figure 1 It is a schematic diagram of the installation structure of the preferred embodiment of the aero-engine test assembly provided by the present invention, such as figure 1 shown. The test assembly provided by the present invention mainly includes an accessory drive casing x1, a compressor casing x2, and a combustion chamber casing x3 which are sequentially connected together. Among them, the rear end of the accessory drive casing x1 is provided with a front bearing seat 1, and the front bearing z1 is arranged in the front bearing seat 1; the front end of the combustion chamber casing x3 is provided with a middle bearing seat ...

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Abstract

The invention provides an aircraft engine casing static test method and a testing assembly thereof. The method comprises the following steps of: assembling a plurality of casings to be tested to form the testing assembly according to an actual assembly requirement of an aircraft engine; fixing the testing assembly; applying simulation load to the testing assembly; and testing according to preset testing items. In the provided test method, the casings of the aircraft engine are combined for testing, mutual influence among the plurality of casings is considered, the load transmission among the casings is more truly simulated in the process of operating the aircraft engine, tested conclusion is more true and reliable, the test period can be effectively shortened by about 2 / 3, and the cost ofscientific research is reduced.

Description

technical field [0001] The invention relates to the field of aero-engines, in particular to a static test method for an aero-engine casing and a test assembly for implementing the method. Background technique [0002] The load-bearing parts of the casing are the main components of the engine load-bearing system, and the accuracy of design analysis in this aspect directly affects the durability and reliability of the aero-engine. [0003] In order to verify whether the casing meets the requirements of the engine, it is necessary to conduct a static test on the casing. However, the investigation and understanding of domestic scientific research institutes and related domestic literature have found that the tests of casing-like load-bearing parts are all tested with a single casing. On the one hand, this test method requires correct load calculation and accurate test boundary conditions. On the other hand, the interaction between parts cannot be simulated during the test. More...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M13/00
Inventor 刘恢先胡烨鑫
Owner CHINA HANGFA SOUTH IND CO LTD
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