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INVENTION OF IMPROVED FUEL FILLER CAP ASSY PT NO MEFC-431-284-000 FOR HAWK MILITARY AIRCRAFT
INVENTION OF IMPROVED FUEL FILLER CAP ASSY PT NO MEFC-431-284-000 FOR HAWK MILITARY AIRCRAFT
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机译:改进的用于鹰式军用飞机的加油口盖总成(专利号MEFC-431-284-000)的发明
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摘要
The Fuel Filler cap assy is used on Hawk Fuselage Fuel Tank.The Fuel Filler Cap Assy consists of Filler Cap housing, Cover Plate, Handle, shaft. Plain pin, Nut, Spring, Plain washer, x0 Rings, Wire locking tab and Split pin made Aerospace grade material. The locking of the Fuel Filler cap shall be accomplished by rotating the handle in a clockwise direction on adaptor and pressing down the handle to flush down the filler cap housing. The fuel filler cap Assy is designed & developed to withstand a rated fuel pressure of 50 PSI. The specifications were prepared in accordance with the requirement of Hawk military Aircraft. The Fuel Filler Cap Assy was designed & developed by M/s Hindustan Aeronautics Ltd,and manufactured in coordination with M/s Micron Engineers, Bangalore. The indigenous Fuel Filler Cap Assy had undergone all the stringent qualification testing as recommended by the certification agencies and met all the- laid down specification and qualification requirements. The LRU is having better leak proof capability and has been cleared by Regional Centre for Airworthiness, CEMILAC for using on Hawk military aircraft.
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机译:加油口盖总成用于Hawk机身油箱。加油口盖总成由加油口盖壳体,盖板,手柄,轴组成。普通销,螺母,弹簧,普通垫圈,x0环,钢丝锁片和开口销制成航空级材料。加油口盖的锁定应通过在适配器上顺时针旋转手柄并向下压手柄以冲洗加油口盖壳体来完成。加油口盖Assy的设计和开发能够承受50 PSI的额定燃油压力。规格是根据Hawk军用飞机的要求准备的。加油口盖总成由M / s Hindustan Aeronautics Ltd设计和开发,并与班加罗尔M / s Micron工程师共同制造。本地的加油口盖总成经过了认证机构的推荐的所有严格的资格测试,并符合所有制定的规格和资格要求。 LRU具有更好的防泄漏能力,并已由CEMILAC区域适航中心批准在鹰式军用飞机上使用。
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