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Balance block and weight-removing balancing method for flexible rotor dynamic balance

A technology of flexible rotor and balance weight, applied in the field of rotor dynamics, can solve problems such as affecting production efficiency, unsuitable transmission shaft, cumbersome operation, etc., and achieves the effects of simple structure, high processing and installation efficiency, and convenient use.

Active Publication Date: 2019-07-02
CHINA HANGFA SOUTH IND CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The invention provides a balance block and a weight-removing balancing method for flexible rotor dynamic balance, so as to solve the cumbersome operation caused by the existing flexible rotor dynamic balance control method, which affects production efficiency and is not suitable for special processes. Technical problem with drive shaft

Method used

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  • Balance block and weight-removing balancing method for flexible rotor dynamic balance
  • Balance block and weight-removing balancing method for flexible rotor dynamic balance
  • Balance block and weight-removing balancing method for flexible rotor dynamic balance

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Embodiment Construction

[0047] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0048] refer to figure 1 and figure 2 , a preferred embodiment of the present invention provides a balance weight for flexible rotor dynamic balance, used to control the dynamic balance of the transmission shaft as a flexible rotor, the balance weight is a hollow thin-walled shaft structure as a whole, including a The connecting section 1 fixed to the transmission shaft and the deduplication section 2 used to meet the dynamic balance requirements of the transmission shaft through deduplication treatment. The deduplication section 2 includes four arc-shaped teeth 21 uniformly distributed along the circumferential direction, and two adjacent arc-shaped teeth 21 U-shaped slots 22 are formed bet...

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Abstract

The invention discloses a balance block for flexible rotor dynamic balance and a de-weight balance method. The balance block is wholly in a hollow thin-wall shaft structure, and comprises a connectionsection for fixing to a transmission shaft and a de-weight section subjected to de-weight processing to meet dynamic balance requirement of the transmission shaft. The de-weight section comprises four arc teeth uniformly distributed in the circumferential direction. A U-shaped groove is formed between two adjacent arc teeth. The arc teeth and the U-shaped grooves are uniformly and alternately distributed in the circumferential direction of the balance block. The balance block is simple in structure and convenient to use, can realize quick assembly and disassembly with the transmission shaft;after de-weight processing of the de-weight section of the balance block, the balance block can meet balance requirement of a rotor; and the balance block is suitable for a rotor shaft subjected to surface treatment, is simple to debug, and is high in processing and installation efficiency.

Description

technical field [0001] The invention relates to the field of rotor dynamics, in particular to a balance weight used for dynamic balancing of a flexible rotor. In addition, the present invention also relates to a weight-removing and balancing method using the above-mentioned balancing weight. Background technique [0002] The rotor of an aero-engine is an important part of an aero-engine. An unbalanced aero-engine rotor will cause engine vibration, generate noise, accelerate bearing wear, shorten the service life of the engine, and cause destructive accidents in severe cases. For this reason, the rotor must be balanced so that the amplitude of the mechanical vibration it generates falls within the allowable range. [0003] The new generation of aero-engines pursues high performance and high thrust-to-weight ratio, and the speed can reach more than 20,000 rpm. The requirements for dynamic balance of flexible rotors are getting higher and higher. Patent CN 105867307A disclose...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M1/02G01M1/34
CPCG01M1/02G01M1/34
Inventor 刘杰章灿李颖慧
Owner CHINA HANGFA SOUTH IND CO LTD