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A Low Vibration Diaphragm Coupling

A diaphragm and coupling technology, which is applied in the direction of couplings, elastic couplings, mechanical equipment, etc., can solve the problem of severe vibration of the coupling, affecting the stability and safety of the rotor system, diaphragm coupling Problems such as large vibration amplitude

Active Publication Date: 2020-10-27
XI AN JIAOTONG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the high rotational speed of the aero-engine, the rotational speed in the test often exceeds the critical rotational speed of the thin-walled sleeve, resulting in severe vibration of the coupling during the critical process, seriously affecting the stability and safety of the rotor system
In order to solve the problem of excessive vibration of the diaphragm coupling during high-speed operation, the present invention proposes a low-vibration diaphragm coupling applied to high-speed and high-power conditions

Method used

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  • A Low Vibration Diaphragm Coupling

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Embodiment Construction

[0024] The present invention will be described in further detail below in conjunction with the accompanying drawings:

[0025] Such as figure 1 As shown, the present invention provides a low-vibration diaphragm coupling applied to high-speed and high-power conditions, including a half coupling 1, a metal diaphragm 3, a spline sleeve 16, a laminate 10, and a positioning metal Diaphragm sleeve 12, thin-walled sleeve 5, O-shaped rubber ring damper or O-shaped wire damper 14, first to third discs 6-8, mandrel 9 and support plate 15.

[0026] figure 1 In order to apply low vibration, high speed and high power diaphragm couplings in large rotating rotors, the two half couplings 1 are connected to the rotor at one end and the motor at the other end. Small misalignment is allowed during the installation of the two shafts and can transmit larger Torque.

[0027] The metal diaphragm 3 is installed on the splined sleeve 16, and the metal diaphragm sleeve 12 is positioned axially to prevent t...

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Abstract

The invention relates to a low vibration diaphragm coupling used in high speed and high power working conditions. The low vibration diaphragm coupling includes semi-couplings, a thin-wall sleeve and so on. Supporting plates, sleeves with splines and the semi-couplings are symmetrically arranged on both ends of the thin-wall sleeve, and the supporting plates, the sleeves with splines and the semi-couplings are successively connected, wherein a core shaft is arranged on the central axis of the thin-wall sleeve, the two ends of the core shaft are correspondingly connected to the centers of the supporting plates on both ends of the thin-wall sleeve, a plurality of disks are installed on the core shaft at intervals, and dampers are arranged between the disks and the inner wall of the thin-wallsleeve; and the thin-wall sleeve, the supporting plates and the sleeves with splines are fastened by bolts, metal diaphragms are arranged on the other ends of the sleeves with splines in a sleeving mode in the circumferential direction, and the outer sides of the metal diaphragms are connected to the corresponding semi-couplings through laminates. The low vibration diaphragm coupling used in the high speed and high power working conditions has high application value for rotor connection design of rotating machinery such as a steam turbine, a turbine, a compressor and an aero-engine. The low vibration diaphragm coupling used in the high speed and high power working conditions has good functions of vibration suppression and vibration reduction, the critical vibration amplitude of the thin-wall sleeve in the diaphragm coupling can be significantly reduced, and the stability of the coupling is improved.

Description

Technical field [0001] The invention belongs to the field of coupling design, and specifically relates to a low-vibration diaphragm coupling applied to high-speed and high-power working conditions. Background technique [0002] Before leaving the factory for the high and low pressure rotors of aeroengines, the critical speed, unbalanced response and stability of the rotor must be tested under the conditions of high speed and high power. The electric motor is used as the power source during the experiment. A coupling is used to connect the aero engine and the electric motor. However, because the coupling has a certain rigidity, the connection with the measured rotor will add extra rigidity to the rotor, which affects the dynamic characteristics of the rotor system. In order to improve the accuracy of the test, the coupling used in the aero engine test has the following requirements: 1. The dynamic and static properties of the rotor system itself cannot be changed; 2. It can trans...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16D3/56
CPCF16D3/56
Inventor 裴世源洪军李超王文超郑文斌徐华
Owner XI AN JIAOTONG UNIV
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