首页> 外国专利> TILTING PLATFORM FOR SIMULATION OF AIRCRAFT ATTITUDES DURING GROUND TESTING OF AIRCRAFT FUEL SYSTEM

TILTING PLATFORM FOR SIMULATION OF AIRCRAFT ATTITUDES DURING GROUND TESTING OF AIRCRAFT FUEL SYSTEM

机译:飞机燃油系统地面测试过程中用于模拟飞机姿态的倾斜平台

摘要

Aircraft Fuel Systems are designed to ensure uninterrupted fuel supply to the engine throughout the flight envelope including reheat/combat and in accordance with retevant MIL specifications. Ground Testing of Aircraft Fuel System requ res simulation of various aircraft attitudes in two axes, namely pitch and roll. Ground Testing also incorporates failure simulations at different attitudes. The Tilting Platform simulates various pitch and roll angles. The platform is tilted by using a 5HP, 3 phase, 1430 RPM Electrical Motor. A gear train connects the motor shaft to the tilting platform. Gear train reduces the speed of the drve to around 1 RPM and provides sufficient torque to tilt the fuel system installed on the platform to any attitude from 0o to 360�. Electromechanic al locking facility is provided in the motor so that in the absence of electrical power, the platform can stay in the set attitude.
机译:飞机燃油系统的设计可确保整个飞行包线(包括再加热/战斗)并根据MIL的相关规定,不间断地为发动机提供燃油。飞机燃油系统的地面测试需要在两个轴(即俯仰和横滚)上模拟各种飞机姿态。地面测试还结合了不同态度下的故障模拟。倾斜平台可模拟各种俯仰和横滚角。通过使用5HP三相1430 RPM电动机倾斜平台。齿轮系将电动机轴连接到倾斜平台。齿轮系将钻机的速度降低至大约1 RPM,并提供足够的扭矩以将安装在平台上的燃油系统倾斜至0o至360°的任何姿态。电机中设有机电锁定装置,因此在没有电源的情况下,平台可以保持在设定姿势。

著录项

  • 公开/公告号IN2014CH05726A

    专利类型

  • 公开/公告日2016-07-01

    原文格式PDF

  • 申请/专利权人

    申请/专利号IN5726/CHE/2014

  • 发明设计人 DR T R RAJANNA;R RAJKUMAR;

    申请日2014-11-14

  • 分类号

  • 国家 IN

  • 入库时间 2022-08-21 14:25:31

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