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Rotor blade damping block reliability test method

A test method and rotor blade technology, applied in vibration test, mechanical component test, machine/structural component test, etc., to achieve the effect of simple test method, low test cost and short test period

Active Publication Date: 2016-12-07
AECC SHENYANG ENGINE RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] The purpose of the present invention is to provide a reliability test method for rotor blade damping blocks to solve or at least alleviate at least one problem in the background technology

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  • Rotor blade damping block reliability test method
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Embodiment Construction

[0031] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses a rotor blade damping block reliability test method, and relates to the technical field of engine testing. The rotor blade damping block reliability test method comprises the following steps that S1, a pressure load F2 is applied to the first side surface (11) of a test damping block (1), wherein the direction of the pressure load F2 is perpendicular to the first side surface (11); the pressure load is applied in a graded way, and each grade of load is increased for 10% of F2 than the last grade of load until the pressure load reaches the value of F2; and S2, a vibration load T is applied to the first side surface (11) of the test damping block (1). The beneficial effects of the rotor blade damping block reliability test method are that reliability testing can be independently performed on the damping block of a rotor blade without being performed along with testing of the complete engine so that the test method is simple, the test period is short and the test cost is low.

Description

technical field [0001] The invention relates to the technical field of engine testing, in particular to a reliability testing method for a rotor blade damping block. Background technique [0002] Adding a rubber damping block under the edge plate of the rotor blade is an effective way to suppress the vibration of the blade. At present, the reliability verification of the damping block needs to be carried out with the test run of the whole engine, which takes a long time and requires a lot of investment, especially for civil engines, which require more than 10,000 hours of service life for cold-end components (including the damping block). Contents of the invention [0003] The purpose of the present invention is to provide a reliability test method for a rotor blade damping block, so as to solve or at least alleviate at least one problem existing in the background art. [0004] The technical solution adopted in the present invention is to provide a reliability test method...

Claims

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Application Information

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IPC IPC(8): G01M7/02G01M13/00
CPCG01M7/00G01M13/00
Inventor 于连超高兴苏守丽印雪梅张海洋郑璇韩方军白志刚沈尔明
Owner AECC SHENYANG ENGINE RES INST
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