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A kind of decomposition method of double tightness chuck

A chuck and tightness technology, which is applied to the supporting components of blades, machines/engines, and leakage prevention, etc., can solve the problems that double tightness chucks cannot be disassembled, and achieve the effect of eliminating friction and interference and stabilizing the decomposition process

Active Publication Date: 2021-09-28
AECC AVIATION POWER CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide a disassembly method of a double-tightness chuck, which solves the defect that the existing double-tightness chuck cannot be disassembled

Method used

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  • A kind of decomposition method of double tightness chuck
  • A kind of decomposition method of double tightness chuck
  • A kind of decomposition method of double tightness chuck

Examples

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Embodiment Construction

[0051] Below in conjunction with accompanying drawing, the present invention is described in detail.

[0052] Such as figure 1 , figure 2 As shown, a disassembly device for a double-tightness chuck provided by the present invention includes a lifting mechanism 1, a body 2, a rotating mechanism 3, an outer ring lifting mechanism 4, a backing plate 5, a gripping mechanism 6 and an auxiliary gripping mechanism 7, wherein , the backing plate 5 is placed under the outer ring lifting mechanism 4, and the turbine disk to be separated is placed in the cavity between the backing plate 5 and the outer ring lifting mechanism 4; the grasping mechanism 6 and the auxiliary grasping mechanism 7 are installed outside In the central hole of the ring lifting mechanism 4, the body 2 is installed on the upper surface of the outer ring lifting mechanism 4, and the body 2 is also connected with the lifting mechanism 1.

[0053] specifically:

[0054] Such as image 3 As shown, the lifting mech...

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Abstract

A disassembly device and method for a double-tightness chuck provided by the present invention includes a lifting mechanism, a body, a rotating mechanism, an outer ring lifting mechanism, a backing plate and a gripping mechanism, wherein the body is arranged below the lifting mechanism, and the gripping mechanism is placed It is under the body, and the three are fixedly connected; the outer ring lifting mechanism is set on one end of the grasping mechanism and connected to the body, and the other end of the grasping mechanism is in contact with the chuck in the double-tightness chuck to be separated; the backing plate is placed Below the lifting mechanism of the outer ring, the turbine disk in the double-tightness chuck to be separated is placed in the cavity between the backing plate and the lifting mechanism of the outer ring, and fixed on the backing plate; the rotating mechanism is set on the lifting mechanism of the outer ring The upper surface of the upper surface; the present invention uses the decomposing hydraulic device to make the chuck pre-deformed, and decomposes the synchronous double-tight over-positioning chuck step by step, eliminating the friction and interference between the parts during the relative motion of the decomposition, and the decomposing process is stable and accurate , Reliable, no bump damage.

Description

technical field [0001] The invention belongs to the technical field of aero-engine assembly, and in particular relates to a method for disassembling a double-tightness chuck. Background technique [0002] In recent years, the chuck (i.e. the integrated structure of the front sealing plate of the turbine rotor and the baffle) has been widely used in domestic advanced aero-engine research products. It is not only the axial positioning baffle of the turbine blade but also the Rotating non-contact gas sealing device, this structure simplifies the turbine components, reduces the number of parts, weight and improves the cooling effect of the disc, which has significant advantages in improving the performance of aircraft engines. [0003] From the analysis of the assembly structure of the chuck and the turbine disk, the chuck and the turbine disk are connected in a "pressure cooker cover" type, and the axial fit tightness is 1.07-1.31mm (that is, the amount of deformation of the ch...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F01D5/30F01D11/04F01D25/00
CPCF01D5/30F01D11/04F01D25/00
Inventor 王满贤孟繁翎吕军刚郗育钊杨翠玲王幸张绍军齐玮凤
Owner AECC AVIATION POWER CO LTD
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