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Airplane spoiler power control assembly testing device

A technology for power control and component testing, applied in the field of aerospace components, can solve problems such as inseparability, high maintenance costs, and functional limitations.

Inactive Publication Date: 2012-05-30
成都富凯飞机工程服务有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The Aircraft Spoiler Power Control Unit (PCU) is an electro-hydraulic servo-actuated component. After the repair work is completed, the entire component needs to be tested for function, although most of the tests are for its mechanical properties, such as travel, internal leakage , withstand voltage, hysteresis and other tests, but these tests require the input of various control electrical signals, and demodulate the feedback signal of the sensor of the component. These tests are inseparable from the special test equipment that is matched with the component. , the existing test equipment is the equipment provided by the PCU manufacturer. This equipment is expensive and not sold externally. It is only provided to major airline customers as incidental equipment and is only used for their internal maintenance, or it is only provided to the manufacturer. Self-established maintenance units, ordinary maintenance companies may not be able to obtain this equipment because it may cause competition in the industry. At the same time, this equipment is a special equipment with limited functions. Different types of test equipment need to be purchased for different types of components. For domestic maintenance companies It is said that the cost is too high to afford; current aircraft spoiler power control components generally have a relatively uniform test socket for testing

Method used

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  • Airplane spoiler power control assembly testing device
  • Airplane spoiler power control assembly testing device
  • Airplane spoiler power control assembly testing device

Examples

Experimental program
Comparison scheme
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Embodiment

[0042] The power supply module in this example includes the first AC power input terminal, the second AC power input terminal, the power switch S11, the fuse F, the first analog-to-digital conversion module, the second analog-to-digital conversion module, the first output terminal of the power supply, the second power supply The second output terminal, the third output terminal of the power supply, the fourth output terminal of the power supply and the transformer. The power supply parameter display module includes an AC voltmeter, an AC ammeter, a DC voltmeter, a single-pole double-throw switch-S1 and a ground wire. The demodulation gain circuit includes a gain Circuit 1, gain circuit 2, single-pole double-throw switch 2 S2 and demodulation circuit, the output amplifier circuit includes single-pole triple-throw switch S3, switch 1 S4, switch 2 S5, current amplifier circuit 1 and current amplifier circuit 2, and the control module includes sliding Rheostat R21, single pole doub...

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PUM

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Abstract

The invention relates to testing technology of aviation components. The invention provides an airplane spoiler power control assembly testing device for solving the problem that the conventional airplane spoiler power control assembly testing equipment has limited function. The invention adopts the technical scheme that: the airplane spoiler power control assembly testing device consists of a power supply module, a power supply parameter display module, a demodulation gain circuit, an input comparison circuit, an output amplifying circuit, an input / output interface, an outer socket and a control module. The device has low cost and is suitable for testing an airplane spoiler power control assembly.

Description

technical field [0001] The invention relates to the technology of aviation components, in particular to the testing technology of aviation components. Background technique [0002] The Aircraft Spoiler Power Control Unit (PCU) is an electro-hydraulic servo-actuated component. After the repair work is completed, the entire component needs to be tested for function, although most of the tests are for its mechanical properties, such as travel, internal leakage , withstand voltage, hysteresis and other tests, but these tests require the input of various control electrical signals, and demodulate the feedback signal of the sensor of the component. These tests are inseparable from the special test equipment that is matched with the component. , the existing test equipment is the equipment provided by the PCU manufacturer. This equipment is expensive and not sold externally. It is only provided to major airline customers as incidental equipment and is only used for their internal m...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B23/02
Inventor 蒋晓阳刘韬
Owner 成都富凯飞机工程服务有限公司