Elastic annular type damping structure used for high-rotating-speed engine

An elastic ring, engine technology, applied in the direction of engine lubrication, engine components, machines/engines, etc., can solve the problems of less reliability than mechanical structure, larger vibration, etc., achieve small structure size, reduce vibration, and run reliable results

Inactive Publication Date: 2020-02-28
NO 60 RES INST OF GENERAL STAFF DEPT PLA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the reliability of the O-ring (rubber ring) is far inferior to that of the mechanical structure. The engine using the O-ring often has a fault phenomenon of sudden increase in vibration during use.

Method used

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  • Elastic annular type damping structure used for high-rotating-speed engine
  • Elastic annular type damping structure used for high-rotating-speed engine
  • Elastic annular type damping structure used for high-rotating-speed engine

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Embodiment Construction

[0020] Below in conjunction with accompanying drawing, a kind of elastic ring type shock-absorbing structure of the present invention is used for high speed engine is described in further detail:

[0021] The invention provides an elastic ring type damping structure for a high-speed engine. Reference attached figure 1 , an elastic ring damping structure for a high-speed engine comprises: an inner ring seat 1 with a bearing chamber, an elastic ring 2, two O-rings 3, and an outer ring seat 4. The elastic ring is located between the inner ring seat and the outer ring seat; the two O-rings are respectively located in the O-ring outer ring groove 11 and the O-ring inner ring groove 44 .

[0022] Reference attached figure 2 And attached Figure 4 , the inner ring seat 1 is provided with an outer ring groove 11 for placing an O-ring 3 and a first lubricating oil hole 12; the outer ring seat 4 is provided with an inner ring groove 44 for placing an O-ring and a second lubricating ...

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Abstract

The invention discloses an elastic annular type damping structure used for a high-rotating-speed engine. The structure comprises an inner ring base with a bearing chamber, an elastic ring, O rings, and an outer ring base. The two O rings are located in ring grooves of the inner ring base and the outer ring base, an outer boss of the elastic ring is in contact attaching to the outer ring base, an inner boss of the elastic ring is in contact attaching to the outer wall face of the inner ring base, the two O rings are located on the two ends of the elastic ring, and the inner ring base and the outer ring base adopt structures capable of preventing relative rotation. According to the elastic annular type damping structure used for the high-rotating-speed engine, for the high-rotating-speed engine, elastic bearing and damping mechanical structure design are achieved, bearing rigidity is reduced, damping is improved, vibration of the high-rotating-speed engine is reduced, the structure sizeis small, and reliability is high.

Description

technical field [0001] The invention relates to an elastic ring damping structure of a high-speed engine, which is used for reducing the vibration level of the high-speed engine. Background technique [0002] The operating speed of modern aero-engines is often greater than the critical speed, so it is necessary to design elastic support and damping mechanical structures to reduce support stiffness and increase damping, thereby reducing engine vibration. For conventional large aeroengines, the operating speed is generally below 50,000rpm (rpm is the unit of speed, 1rpm means 1 revolution per minute), and there is enough dimensional space for designing elastic supports. On the contrary, high-speed engines, especially aero-engines or turbochargers with speeds above 50,000rpm, have limited size and space, and O-rings (rubber rings) are usually used instead of elastic supports and damping mechanical structures to reduce engine vibration, such as AMT The company's NIKE small turb...

Claims

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Application Information

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IPC IPC(8): F02C7/06F01D25/04
CPCF01D25/04F02C7/06
Inventor钱松林陈强张俊成吴进军
OwnerNO 60 RES INST OF GENERAL STAFF DEPT PLA