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A riveting device for assembly and riveting of reverse push door of aero-engine

A technology of aero-engine and push-reverse door, which is applied in the direction of feeding device, positioning device, storage device, etc., can solve the problems of low processing efficiency, affecting parts assembly, and parts quality fluctuation, and achieves the improvement of work efficiency, installation, positioning and disassembly. The effect of convenience and stability guarantee

Active Publication Date: 2016-05-18
AECC AERO SCI & TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The existing process equipment only has the function of clamping and fixing. Although it can prevent the parts from shaking during processing, the positioning reference of the existing process equipment does not coincide with the assembly reference of the parts, which affects the assembly of the parts and eventually leads to The quality of parts fluctuates greatly, making it difficult to achieve uniform quality standards
Moreover, using the existing technology and equipment to assemble and rivet the reverse push door of the aeroengine still has the disadvantages of low processing efficiency and high labor intensity of the operators.

Method used

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  • A riveting device for assembly and riveting of reverse push door of aero-engine
  • A riveting device for assembly and riveting of reverse push door of aero-engine
  • A riveting device for assembly and riveting of reverse push door of aero-engine

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Experimental program
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Embodiment 1

[0026] In this embodiment, the structure of the device used for riveting the reverse push door assembly of the aeroengine is as follows: Picture 1-1 , 1-2 As shown in and 1-3, the structure of the riveted reverse sliding door to be assembled is as follows diagram 2-1 , 2-1 and 2-3. The reverse push door assembly riveting device includes a profile frame 1, which is fixedly arranged on the profile frame stand for connecting and positioning the fulcrum members installed on the two side frames of the riveted reverse push door to be assembled and the positioning member for riveting the reverse push door to be assembled. The inner panel leather surface layer 25 and the outer panel leather surface layer 24 are clamped on the inner clamping plate and the outer clamping plate on the frame surface of the reverse push door body, and are fixedly arranged on the frame bottom frame for supporting the riveted reverse push door to be assembled The support assembly of the lower frame and t...

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PUM

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Abstract

The invention provides a reverse push door assembly riveting device for aircraft engine, which comprises a fixture, positioning components, an inner snap gauge, an outer snap gauge and a support base component. The positioning components are fixed on the erect frame of the fixture and are used to connect and position to stationary members on the two sides frames of a reverting push door to be assembled. The inner snap gauge and the outer snap gauge are used to cover and clamp the inner and outer board panels to the door frame surfaces of the reverting push door to be assembled. The support base component is fixed on the base of the fixture and is used to support the lower frame of the reverting push door to be assembled. The positioning components are four and symmetrically disposed on the erecting frames on the two sides of the fixture. The distance of two stationary members at the same side of the erecting frame of the fixture is the same as the designed distance of the two up-and-down stationary members at one side frames of the reverting push door to be assembled. The distance of two stationary members at the same side of the erecting frame of the fixture is the same as the designed distance of the two up-and-down stationary members at one side frames of the reverting push door to be assembled. Each positioning component is respectively matched with each corresponding stationary members of the reverting push door.

Description

technical field [0001] The invention belongs to the field of aero-engine assembly, in particular to a riveting device for assembly and riveting of an aero-engine reverse push door. Background technique [0002] The anti-push door is an important part of the propulsion device of the aero-engine. Its structure is complex, and it needs to be assembled and riveted smoothly with the help of corresponding technological equipment. The existing process equipment only has the function of clamping and fixing. Although it can prevent the parts from shaking during processing, the positioning reference of the existing process equipment does not coincide with the assembly reference of the parts, which affects the assembly of the parts and eventually leads to The quality of parts fluctuates greatly, making it difficult to achieve uniform quality standards. In addition, the use of existing technology and equipment to assemble and rivet the reverse push door of the aeroengine still has the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B21D39/02B21D43/00
CPCB21D39/02B21D43/003
Inventor 陈静何露曾智
Owner AECC AERO SCI & TECH CO LTD