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民用飞机机翼区域液压系统闪电防护设计研究 被引量:1

Research of Hydraulic System Lightning Protection in Civil Aircraft Wing
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摘要 民用飞机液压系统作为机翼燃油箱区域内布置的主要系统之一,其相关的闪电防护设计对机翼燃油箱防爆有着重要作用。本文结合液压系统布置原则,运用EMA3D仿真软件对机翼燃油箱内液压导管电流、电压进行仿真,重点研究了液压导管的搭接对闪电防护的影响。 Due to be one of the main systems disposed in wing fuel tank, hydraulic system lightning protection design is very important to aircraft fuel tank protection. Based on hydraulic system layout and software EMA3D, the lightning currents and voltages on hydraulic pipes inside of the fuel tank are simulated, and the bond of hydraulic pipes impact on lightning protection is the focus in this paper.
出处 《科技视界》 2017年第4期307-307,237,共2页 Science & Technology Vision
关键词 机翼 液压系统 闪电防护 搭接 Wing Hydraulic System Lightning Protection Bond
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  • 1SAE ARP4752 Design and Installation of Commercial TransportAircraft Hydraulics Systems
  • 2AC 20-128A Design Considerations for Minimizing HazardsCaused By Uncontained Turbine Engine and Auxiliary Power UnitRotor Failure.
  • 3FAA-2014-1027. Transport Airplane Fuel Tank and System Lightning Protection[S]. Dee 18, 2014.
  • 4AC 25. 981- IC. Fuel Tank Ignition Source Prevention Guidelines [S]. Sep 19, 2008.
  • 5SAE ARP5416. Aircraft lightning test methods [S]. Mar 2005.
  • 6ANM- 112-08-002. Policy on Issuance of Special Condi- tions and Exemptions Related to Lightning Protection of Fuel Tank Structure[S]. May 26, 2009.
  • 7PS-ANM-25. 981-02. Policy on Issuance of Special Condi- tions and Exemptions Related to Lightning Protection of Fuel Tank Structure and Systems[S]. Jun 24, 2014.
  • 8SAE AE-2 Lightning Committee. Policy Guidance for Fuel Tank Structural Lightning Protection[S]. July 5, 2011.
  • 9AC 25. 981-2A. Fuel Tank Flammability Reduction Means [S]. Sep 19, 2008.
  • 10DOT/FAA/AR-05/8. Fuel Tank Flammability Assessment Method User's Manual[S]. May 2008.

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