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Bearing support device for aero-engine

An aero-engine and bearing support technology, which is applied to the rigid brackets, shafts and bearings, bearing components of bearing components, etc., can solve problems such as hidden dangers, ineffective shock absorption, and vulnerable shafts of the engine, and reduce the impact force. Effect

Active Publication Date: 2019-07-12
刘和来
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] In modern industrial production and daily life, bearings can be seen everywhere, and as a fixing device for bearings, bearing supports have been widely used. Although the structure of the invention patent is simple, it cannot effectively absorb shocks, so the engine shaft is vulnerable during aviation, which not only brings inconvenience to people's travel, but also brings safety hazards

Method used

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  • Bearing support device for aero-engine
  • Bearing support device for aero-engine
  • Bearing support device for aero-engine

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Embodiment Construction

[0021] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0022] see Figure 1-5 , The present invention provides a technical solution: a bearing support device for an aero-engine, comprising a bearing 1, the bearing 1 comprises an inner ring body 101, the inner ring body 101 sandwiches the balls 103, and the outer wall of the inner ring body 101 is installed with ten The ball 103, the outer ring body 102 is installed on the outside of the inner ring body 101, and the ball 103 is connected w...

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Abstract

The invention discloses a bearing supporting device applied to an aero-engine. The bearing supporting device comprises a bearing; the bearing comprises an inner ring body; a plurality of balls are installed at the outer wall of the inner ring body; a clamping plate is installed in an inner chamber of a clamping slot; an inserting rod is installed at the upper surface of the clamping plate; the topend of the inserting rod is connected with a second upright post; and a second spring is installed at the bottom of the clamping plate and is connected with the inner wall of the clamping slot. According to the bearing supporting device applied to the aero-engine, a first clamping ring and a second clamping ring are used for clamping the bearing at the middle; a nut is tightened and the clampingplate is pressed tightly in a way of twisting a bolt so that the bearing can be clamped by the first clamping ring and the second clamping ring; when shock occurs, the first spring supports the secondupright post so that the shock is alleviated, and the clamping plate is used for limiting the relative positions of a first upright post and the second upright post; and the second spring positionedat the bottom of the clamping plate can also be used for reducing an impact force when shock occurs, so the safety of people is guaranteed.

Description

technical field [0001] The invention relates to the technical field of bearings, in particular to a bearing support device for an aero-engine. Background technique [0002] In modern industrial production and daily life, bearings can be seen everywhere, and as a fixing device for bearings, bearing supports have been widely used, such as the invention patent application number CN 203130990U, including transmission shafts, bearings, bearing supports Although the structure of the invention patent is simple, it cannot effectively absorb shock, which makes the rotating shaft of the engine vulnerable during the aviation process, which not only brings inconvenience to people's travel but also brings security risks. SUMMARY OF THE INVENTION [0003] The purpose of the present invention is to provide a bearing support device for an aero-engine to solve the above-mentioned problems in the background art. [0004] In order to achieve the above purpose, the present invention provides...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16C35/06F16F15/08
CPCF16C35/06F16F15/08
Inventor 刘和来
Owner 刘和来
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