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Device allowing engine component to rotate to be assembled

An engine and component technology, applied in the field of aero-engine assembly, can solve the problems of discoloration of dishes, inability to rotate, and large diameter of the round table, and achieve the effect of reducing labor intensity and improving work efficiency

Inactive Publication Date: 2018-05-04
AECC SICHUAN GAS TURBINE RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Just imagine, many people eat around a round table. The round table has a large diameter (like an engine part) and cannot be rotated. People need to walk around the table to eat, and even the most delicious dishes will be eclipsed by it.

Method used

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  • Device allowing engine component to rotate to be assembled
  • Device allowing engine component to rotate to be assembled
  • Device allowing engine component to rotate to be assembled

Examples

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Embodiment Construction

[0020] The present invention will be described in further detail below in conjunction with the accompanying drawings of the description, please refer to Figure 1~2 .

[0021] figure 1 Shown is a structural diagram of a device capable of rotatably assembling engine parts according to the present invention. The device includes an extension ring 1, a thrust bearing 2, a stop pin 3, a rotating disc 4, a pressing device 5, a platform main body 6, and casters 7. Wherein, the rotating disk 4 is connected through the pressing device 5 and the thrust bearing 2, and the workpiece to be assembled is placed on the upper surface of the rotating disk 4 to realize the rotating function. When the rotating disk 4 rotates to a certain angle and needs to stop reliably, the stop pin 3 is inserted into the pin hole to ensure that the rotating disk 4 does not rotate any more. The platform main body 6 bears the gravity of the workpiece. The extension ring 1 is used to meet the assembly requirem...

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PUM

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Abstract

The invention belongs to the technical field of aviation engine assembly, and particularly relates to a device allowing an engine component to rotate to be assembled. The device comprises an anti-thrust bearing 2, a braking pin 3, a rotating disc 4, a compression device 5, a platform main body 6 and trundles 7. The rotating disc 4 is connected with the anti-thrust bearing 2 through the compressiondevice 5, and the rotating function of the rotating disc 4 is achieved. When the rotating disc 4 rotates to a certain angle and needs to stay reliably, the braking pin 3 is inserted into a pin hole in the edge of the rotating disc 4, and thus it is ensured that the rotating disc 4 does not rotate any longer. The platform main body 6 bears the gravity of a workpiece. An extending ring 1 is used for meeting the assembly requirements of workpieces of different diameter sizes, and rotates with the rotating disc 4 together in the working process. The trundles 7 are used for achieving the moving function of a platform, have a braking function by itself and are used for ensuring reliable braking of the platform. Unnecessary workloads of tangential displacement generated between operation personnel and assemblies are omitted, the labor intensity is relieved, and the working efficiency is improved.

Description

technical field [0001] The invention belongs to the technical field of aero-engine assembly, and in particular relates to a device capable of rotatably assembling engine parts. Background technique [0002] The status of air supremacy is increasing day by day in modern warfare, which requires fighters to perform difficult combat missions around the clock under harsh weather conditions. The aero engine is the "heart" of the aircraft and the source of aircraft power. It is known as the jewel on the top of the industrial crown. To reliably guarantee the maneuverability and combat readiness of fighter jets, aero engines with high thrust-to-weight ratio and high reliability bear the brunt. As an important link in the engine manufacturing cycle, aero-engine assembly is the post-process of engine manufacturing and an independent production stage. [0003] The aero-engine belongs to the turbine, and most of its parts are evenly distributed in the circumferential direction. Such a...

Claims

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Application Information

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IPC IPC(8): B23P21/00B25H1/02
CPCB23P21/006B25H1/02
Inventor 徐广庆徐铭泽白彦张格若张纲董磊磊
Owner AECC SICHUAN GAS TURBINE RES INST
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