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Calibrator for calibration of adjusting mechanism and calibration method of adjusting mechanism

A technology of adjusting mechanism and calibration instrument, which is applied in the direction of control/adjustment system, instrument, computer control, etc., can solve the problem of high cost, achieve the effects of reducing manufacturing and use costs, avoiding out-of-tolerance calibration results, and shortening assembly time

Active Publication Date: 2021-12-07
AECC AVIATION POWER CO LTD
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  • Claims
  • Application Information

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Problems solved by technology

[0004] The purpose of the present invention is to overcome the disadvantages of the high cost of the calibration test of the adjustment mechanism of the aeroengine high-pressure compressor in the above-mentioned prior art, and to provide a calibration instrument for calibration of the adjustment mechanism and a calibration method for the adjustment mechanism

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  • Calibrator for calibration of adjusting mechanism and calibration method of adjusting mechanism
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  • Calibrator for calibration of adjusting mechanism and calibration method of adjusting mechanism

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Embodiment Construction

[0023] In order to enable those skilled in the art to better understand the solutions of the present invention, the following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only It is an embodiment of a part of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts shall fall within the protection scope of the present invention.

[0024] It should be noted that the terms "first" and "second" in the description and claims of the present invention and the above drawings are used to distinguish similar objects, but not necessarily used to describe a specific sequence or sequence. It is to be understood that the data so used are interchangeable under appropriate ...

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Abstract

The invention belongs to the field of aero-engines, and discloses a calibration instrument for calibration of an adjusting mechanism and a calibration method of the adjusting mechanism, and the calibration instrument comprises an upper computer, a processor, an electro-hydraulic servo valve driving module, an electromagnetic valve driving module and an LVDT control module; the upper computer obtains and sends a control instruction, the processor generates an electro-hydraulic servo valve control signal and an electromagnetic valve control signal according to the control instruction, the electro-hydraulic servo valve driving module generates an electro-hydraulic servo valve driving signal according to the electro-hydraulic servo valve control signal, and the electromagnetic valve driving module generates an electromagnetic valve driving signal according to the electromagnetic valve control signal; the LVDT control module generates an excitation signal, sends the excitation signal, receives the excitation signal and sends collected data sent by a linear displacement sensor of the adjusting mechanism to the processor and the upper computer; and the upper computer calibrates the adjusting mechanism according to the collected data. The working performance of the adjusting mechanism can be detected in advance, reworking and secondary assembly of the adjusting mechanism caused by out-of-tolerance calibration results during complete machine assembly are avoided, the production cycle is shortened, and the cost is reduced.

Description

technical field [0001] The invention belongs to the field of aero-engines, and relates to a calibration instrument for calibration of an adjustment mechanism and a calibration method for the adjustment mechanism. Background technique [0002] The adjustment mechanism of the high-pressure compressor of the aero-engine needs to be calibrated before use. At present, the calibration test of the high-pressure compressor adjustment mechanism of the aero-engine is generally carried out under the assembly condition of the core machine / complete machine of the aero-engine, and the debugging equipment usually adopts the engine controller . [0003] However, this method has the following disadvantages: the calibration test of the high-pressure compressor adjustment mechanism is carried out under the assembly condition of the core engine / whole machine. It will inevitably affect the assembly cycle of the engine; after the assembly of the adjustment mechanism components is completed, the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B19/042
CPCG05B19/0423G05B2219/24215Y02P90/02
Inventor 李静闫庆安庞昕郗育钊王满贤雷飞刘丽慧张昊哲
Owner AECC AVIATION POWER CO LTD
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