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Method for measuring strain of connecting piece of pull rod linkage mechanism

A linkage mechanism and strain measurement technology, applied in measurement devices, instruments, optical devices, etc., can solve the problems of inaccurate measurement and limited space of measurement parts, and achieve the effect of reducing development cost and shortening development cycle.

Inactive Publication Date: 2016-11-09
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0004] The purpose of the present invention is to provide a method for measuring the strain of the connecting part of the tie rod linkage mechanism, which can solve the problems of current measurement methods or inaccurate measurement, or limited to the space of the measurement part.

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  • Method for measuring strain of connecting piece of pull rod linkage mechanism
  • Method for measuring strain of connecting piece of pull rod linkage mechanism
  • Method for measuring strain of connecting piece of pull rod linkage mechanism

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Embodiment Construction

[0019] 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 making creative efforts belong to the protection scope of the present invention. Embodiments of the present invention will be described in detail b...

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Abstract

The invention relates to a method for measuring the strain of the connecting piece of a pull rod linkage mechanism. The method captures a sensed image of a connection position by using double cameras, may measure the strain gradient of the curved connecting piece, and comprises a step 1 of establishing a non-contact measurement coordinate system; a step 2 of discretizing a curved structure to be measured in order to divide the curved structure to be measured into a plurality of area units, observing the area units by using the double cameras at two different points of sight in order to obtain the sensed images, and obtaining the 3D morphological information of the surface of an object by computing and analyzing the parallax of the area units in different sensed images; a step 3 of computing the spatial positions, in the measurement coordinate system, of measuring points in the curved surface to be measured; and a step 4 of performing subarea point-by-point fitting on a displacement field by using a fitting process to obtain full-field strain. The method for measuring the strain of the connecting piece of a pull rod linkage mechanism overcomes the defects of a conventional strain gage measurement method, shortens a development period, and reduces development cost.

Description

technical field [0001] The invention belongs to the technical field of structural strength analysis, and in particular relates to a method for measuring the strain of a connecting piece of a tie rod linkage mechanism. Background technique [0002] With the improvement of the flight performance of modern aircraft, the linkage mechanism of the high-lift accretion device is widely used, see figure 1 As shown, A, B, C, and D in the figure are the connection positions. Connecting parts with large gaps in the linkage mechanism under the action of large concentrated loads (see figure 2 As shown) a new measurement method is urgently needed for strength assessment and calculation, which has become an important content of structural strength analysis. [0003] Regarding the strain measurement method of the large gap structure of the linkage mechanism, the strain gauge method is mainly used at present, and the strain gauge measurement method has high requirements on the measurement ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01B11/16
CPCG01B11/16
Inventor 郑茂亮范瑞娟王利国魏洪李健李海林
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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