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Structure for ensuring concentricity of gas compressor control mechanism through rolling contact

A control mechanism and rolling contact technology, applied in the direction of machines/engines, liquid fuel engines, pumping devices for elastic fluids, etc., can solve the problems affecting the reliability of the engine control mechanism, poor follow-up of the adjustment system, and baffles wear and other problems, achieve huge economic and social benefits, reduce the frequency of replacement, and reduce the effect of long-term wear and tear

Active Publication Date: 2018-05-04
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Existing structures such as image 3 The concentricity is ensured through the sliding contact between the radial support pin and the baffle plate. During the adjustment process, the thrust required to overcome the sliding friction is relatively large, and the followability of the adjustment system is poor. Long-term use will cause the baffle plate to wear and affect the reliability of the engine control mechanism.

Method used

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  • Structure for ensuring concentricity of gas compressor control mechanism through rolling contact
  • Structure for ensuring concentricity of gas compressor control mechanism through rolling contact
  • Structure for ensuring concentricity of gas compressor control mechanism through rolling contact

Examples

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Effect test

Embodiment Construction

[0021] Such as Figure 1-2 Shown is a structure that uses rolling contact to ensure the concentricity of the compressor control mechanism, including actuating ring 1, ball 2, wear-resistant layer 3, ball seat 4 and casing 5;

[0022] The ball seat 4 is a cuboid structure;

[0023] The ball seat 4 is fixed on the casing by welding or bolting;

[0024] The ball seat 4 is provided with a ball and socket structure;

[0025] A wear-resistant layer 3 is provided in the ball-and-socket structure;

[0026] The ball 2 is placed in the ball seat 4;

[0027] The actuating ring 1 is in surface contact with the ball 2;

[0028] The actuating ring 1 and the casing 5 are arranged concentrically.

[0029] The ball 2 is spherical.

[0030] The wear-resistant layer 3 can be a ceramic layer or a non-metallic coating;

[0031] A plurality of ball seats 4 and balls 2 are evenly distributed on the casing 1 .

[0032] A structural movement method that uses rolling contact to ensure the conce...

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PUM

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Abstract

The invention discloses a structure for ensuring the concentricity of a gas compressor control mechanism through rolling contact. The structure comprises an actuating ring, a ball, an anti-abrasion layer, a ball seat and a casing. The ball seat is of a cuboid structure and is fixed to the casing through welding or bolted connecting. A ball socket is formed in the ball seat and internally providedwith the anti-abrasion layer, and the ball is stored in the ball socket. The actuating ring makes contact with the ball surface of the ball, and the actuating ring and the casing are concentrically arranged. According to the technical scheme of the structure, the thrust for friction overcoming is small, the following property of the control mechanism is good, abrasion of long-term use is small, and the reliability of an engine control mechanism is improved.

Description

technical field [0001] The invention relates to the technical field of aero-engines, in particular to a structure that adopts rolling contact to ensure the concentricity of a compressor control mechanism. Background technique [0002] In the process of adjusting the angle of the adjustable blades, the control mechanism of the aero-engine compressor needs a structure to ensure the concentricity of the actuating ring and the compressor casing. Existing structures such as image 3 The concentricity is ensured through the sliding contact between the radial support pin and the baffle plate. During the adjustment process, the thrust required to overcome the sliding friction is relatively large, and the followability of the adjustment system is poor. Long-term use will cause the baffle plate to wear and affect the reliability of the engine control mechanism. Contents of the invention [0003] In order to solve the above technical problems, the purpose of this invention is to prov...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F04D29/56
CPCF04D29/563
Inventor 王丹包宏强李春波王华王维东
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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