Study of Aircraft Wing Flap Hydraulic System Dynamics Under Damages Due to Operating an Aircraft

Andrzej Gronczewski; Józef B?achnio

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Study of Aircraft Wing Flap Hydraulic System Dynamics Under Damages Due to Operating an Aircraft

机译：飞机运行造成损害的飞机机翼襟翼液压系统动力学研究

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The paper indicates the main reasons for faulty operation of aeroplane wing flap hydraulic systems. A mathematical model of the wing flap dynamics has been presented, allowing an analysis of a simulation study taking into account damages due to usual wear and tear during operating of a plane.

机译：本文指出了飞机机翼襟翼液压系统故障的主要原因。提出了机翼襟翼动力学的数学模型，可以对仿真研究进行分析，同时考虑由于飞机运行过程中通常的磨损造成的损坏。

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来源
《Journal of KONBiN》 |2008年第3期|共页
作者
Andrzej Gronczewski; Józef B?achnio;
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3. The use of throttled variable displacement hydraulic motors in aircraft landing flap control systems [J] . O. Biedermann, G. Greerling Olhydraulik und Pneumatik: Zeitschrift fur Fluidtechnik·Aktorik, Steuerelektronik und Sensorik . 2001,第1期

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5. An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft. [D] . Perrino, Michael. 2014

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6. A report – recommended standards for UK fixed wing medical air transport systems and for patient management during transfer by fixed wing aircraft [O] . A Bristow, N J Toff 1992

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7. Study of Aircraft Wing Flap Hydraulic System Dynamics Under Damages Due to Operating an Aircraft [O] . Józef Błachnio, Andrzej Gronczewski 2008

机译：造成飞机损坏下飞机翼片液压系统动力学的研究

Study of Aircraft Wing Flap Hydraulic System Dynamics Under Damages Due to Operating an Aircraft

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