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Blade mortise adhesive tape repair device and method

A blade tenon and repair method technology, applied in the direction of material gluing, connecting components, mechanical equipment, etc., can solve problems such as inability to repair, achieve the effects of shortening the production cycle, avoiding false contact, and ensuring the repair effect

Active Publication Date: 2018-12-28
AECC AVIATION POWER CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, for the part where the thickness of the rubber strip on the tenon is in a gradual shape, the existing technology cannot be repaired

Method used

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  • Blade mortise adhesive tape repair device and method
  • Blade mortise adhesive tape repair device and method
  • Blade mortise adhesive tape repair device and method

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Embodiment Construction

[0026] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0027] Such as image 3 shown, refer to figure 1 , figure 2 and Figure 4 , the device for repairing the tenon rubber strip of the blade of the present invention includes a repair block 7, and the repair block 7 is provided with a first positioning surface 1 for fitting and positioning with the end face locking block 6-1 of the tenon 6, and is used for aligning with the bottom surface of the tenon 6 6-4 The second positioning surface 2 for fitting and positioning, and the mold part 4 for repairing the gradient rubber strip part 6-5 rubber strip matching the gradient rubber strip part 6-5 of the tenon 6, the mold part 4. A separation space 4-2 is provided near the second positioning surface 2 for separating from the glue strip on the bottom surface 6-4 of the tenon 6.

[0028] refer to Figure 2 ~ Figure 4 , as a preferred embodiment of the present...

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PUM

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Abstract

The invention belongs to the technical field of aircraft engine blade mortise repair, and particularly relates to a blade mortise adhesive tape repair device and method. The repair device comprises arepair block, and the repair block is provided with a first positioning surface for being attached to and positioned with an end face locking block of a mortise, a second positioning surface for beingattached to and positioned with the bottom surface of the mortise and a mold portion matched with an adhesive tape of a grading adhesive tape portion of the mortise for repairing the adhesive tape ofthe grading adhesive tape portion, and a separation space used for being separated from an adhesive tape of the bottom face non-repair portion of the mortise is arranged on the portion, close to thesecond positioning surface, of the mold portion. The mold portion can repair the gradient part of the adhesive tape in the gumming process of an aircraft engine blade, and the separation space used for being separated from the adhesive tape of the bottom face non-repair portion of the mortise is arranged on the portion, close to the second positioning surface, of the mold portion, so that the erroneous contact with the non-repair portion is avoided, and the repairing effect can be ensured.

Description

technical field [0001] The invention belongs to the technical field of aero-engine blade tenon repair, and in particular relates to a blade tenon rubber strip repair device and method. Background technique [0002] The current process uses tape cutting to make a mold, by sticking the tape on the tenon to ensure the position of the rubber strip, manually applying glue to the tape pasted on the tenon, and scraping the glue and tape with a blade to ensure the thickness of the glue strip . However, the existing technology cannot repair the part where the thickness of the rubber strip on the tenon is in a gradual shape. Contents of the invention [0003] In order to solve the problems existing in the prior art, the object of the present invention is to provide a blade tenon rubber strip repair device and method, which can repair the gradual change of the rubber strip during the process of applying glue to the tenon of the aero-engine blade. [0004] The purpose of the inventi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16B11/00
CPCF16B11/006
Inventor 周奋郭海孟少轩穆聪芳张新冬李晨郭洋杨林
Owner AECC AVIATION POWER CO LTD
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