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Arm design to support airplane turbojet engine nacelle, airplane turbojet engine nacelle incorporating one arm, propulsion assembly.
Arm design to support airplane turbojet engine nacelle, airplane turbojet engine nacelle incorporating one arm, propulsion assembly.
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机译:机臂设计可支撑飞机涡轮喷气发动机机舱,飞机涡轮喷气发动机机舱包含一个臂,推进组件。
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摘要
This strut (9), designed to support an aircraft turbojet engine, has, on the one hand, a connecting part (11) for connection between the casing (1) of the fan (3) or the casing of the gas generator (5) of the said turbojet engine and a wing of the said aircraft and, on the other hand, a Y-shaped box-section part (19), secured to the said connecting part (11) and designed to form the upper part of the inner fixed structure of the said nacelle.
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