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Device for detecting deflection of turbine disk tongue-and-groove and method

A detection device and turbine disk technology, applied in the direction of angle/taper measurement, can solve the problems of not being able to meet the requirements of the production schedule and spending a lot of time, and achieve the effect of low cost and convenient operation

Inactive Publication Date: 2019-04-05
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] Aiming at the deficiencies in the prior art, such as the time-consuming detection of the tenon-groove deflection angle of the turbine disk and the inability to meet the requirements of the production schedule, the problem to be solved by the present invention is to provide a device and method for detecting the deflection of the tenon-groove of the turbine disk that can improve the detection speed

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  • Device for detecting deflection of turbine disk tongue-and-groove and method
  • Device for detecting deflection of turbine disk tongue-and-groove and method
  • Device for detecting deflection of turbine disk tongue-and-groove and method

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Embodiment Construction

[0028] The present invention will be further elaborated below in conjunction with the accompanying drawings of the description.

[0029] like Figure 1~6 As shown, a turbine disk tenon-groove deflection detection device of the present invention includes a positioning part, a pressing part and a measuring part, wherein the positioning part fits the tooth-shaped surface of the turbine disk through the tooth-shaped block 1, and passes through the plate 3 It is positioned with the front end of the turbine disk; the toothed block 1 is pressed into the tenon groove of the turbine disk through the pressing part; the measuring part includes a table frame 2 that can rotate relative to the toothed block 1, and the other end of the table frame 2 is sleeved on the tooth On the extension shaft of shape block 1, there is sliding bush in the middle to be convenient to rotate.

[0030] The positioning part includes a toothed block 1 and a plate 3, such as Figure 4 As shown, the tooth-shape...

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Abstract

The invention discloses a device for detecting deflection of a turbine disk tongue-and-groove and a method. The device comprises a positioning part, a pressing part, and a measuring part. The positioning part is matched with a toothed surface of the turbine disk tongue-and-groove by a toothed block, and is positioned by a plate and a front end surface of the turbine disk. The toothed block is fixed in the turbine disk tongue-and-groove by the pressing part. The measuring part comprises a dial indicator stand that is rotatable relative to the toothed block, and the other end of the dial indicator stand is sleeved on a projecting shaft of the toothed block. The device for detecting deflection of a turbine disk tongue-and-groove and the method solve the problem that the deflection of the turbine disk tongue-and-groove relative to the turbine disk is difficult to measure. The deviation of the deflection of the turbine disk tongue-and-groove relative to the turbine disk is conveniently andquickly measured through a final result, and the actual operation is convenient and fast and low in cost.

Description

technical field [0001] The invention relates to a turbine disk tenon and groove detection technology, in particular to a turbine disk tenon and groove deflection detection device and method. Background technique [0002] The turbine is an important part of the aero-engine, and the processing quality of the turbine is directly related to the performance index of the aero-engine. In the deflection detection of the tenon and groove of the turbine disk relative to the turbine disk, it is difficult to accurately measure the position deviation using conventional methods. The three-coordinate inspection is generally used in the development stage of the turbine disk. The three-coordinate inspection in the mass production stage takes a lot of time and cannot be measured. To meet the production schedule requirements, it is necessary to develop a fast and accurate detection tool. [0003] At present, no detection tool that can meet the above rapid detection requirements has been repor...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01B5/24
CPCG01B5/24
Inventor 郑松孙玉伟刘昕孙海丽宋慧军
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION