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A vibration reduction system and vibration reduction method for reducing the vibration of the whole aircraft engine

An aero-engine and engine technology, which is applied to engine components, machines/engines, mechanical equipment, etc., can solve the problems of vibration of the whole machine, unbalanced force of the engine rotor, and no unbalanced amount, and achieve the effect of reducing the vibration of the whole machine.

Active Publication Date: 2022-07-29
中国航发贵阳发动机设计研究所
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  • Summary
  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0003] Traditional methods to reduce engine vibration levels include improving the machining accuracy of engine parts and reducing the residual unbalance of the rotor dynamic balance, but it is still impossible to completely eliminate the unbalance, and the engine rotor will always generate unbalanced force and vibration of the whole machine

Method used

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  • A vibration reduction system and vibration reduction method for reducing the vibration of the whole aircraft engine
  • A vibration reduction system and vibration reduction method for reducing the vibration of the whole aircraft engine

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Embodiment Construction

[0017] In order to make the technical solutions of the present invention clearer, the present invention will be further described in detail. The control system of the invention includes a rotational speed sensor, a rotational speed signal acquisition unit, a vibration sensor, a vibration signal acquisition unit, a vibration controller, an excitation processing unit, a vibration excitation device, and an electronic rotor controller.

[0018] Due to the residual unbalance of the engine rotor, an unbalanced force is generated during rotation, and the unbalanced force brings about the vibration of the whole machine. The unbalance and azimuth angle of the engine rotor in the stable rotation state remain unchanged. The engine using the flexible rotor has a critical speed in the working speed range, and the vibration of the engine will increase abruptly near the critical speed, but its vibration direction is also regular. . The overall vibration level of the engine can be reduced by...

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Abstract

The invention relates to the technical field of mechanical vibration control, in particular to a vibration reduction system and a vibration reduction method for reducing the vibration of an aero-engine; the system includes a rotational speed sensor, a rotational speed signal acquisition unit, a vibration sensor, a vibration signal acquisition unit, and a vibration control unit. The engine electronic controller will analyze the vibration value and the vibration value of the current time and the next time. The azimuth angle is sent to the vibration controller; the vibration controller conducts vibration analysis and logical judgment according to the signal collected by the vibration signal acquisition unit and the signal sent by the electronic controller, and obtains the control signal required by the vibration excitation device, which is processed by the excitation processing unit. Control the vibration excitation device. The invention effectively reduces the vibration of the whole engine through intelligent adjustment.

Description

technical field [0001] The invention relates to the technical field of mechanical vibration control, in particular to a vibration reduction system and a vibration reduction method for reducing the vibration of the entire aero-engine. Background technique [0002] Aero-engines are large rotating machines with high temperature and high speed. Due to the machining error of parts and the influence of the natural frequency of the rotor itself, the rotor of the engine will generate a large unbalanced force when it rotates, and the unbalanced force will cause the whole machine to vibrate. Larger vibration will affect the life of the engine itself and the flight safety of the aircraft. The vibration value of the engine is an important parameter to monitor whether the engine state is normal. [0003] The traditional methods to reduce the vibration level of the engine include improving the machining accuracy of engine parts and reducing the residual unbalance of the rotor dynamic bala...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F01D5/10F01D21/00
CPCF01D5/10F01D21/00F01D21/003
Inventor 刘鹏飞
Owner 中国航发贵阳发动机设计研究所
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