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INTEGRATED PROPULSIVE SYSTEM COMPRISING A DOUBLE FLOW TURBOREACTOR ENGINE.
INTEGRATED PROPULSIVE SYSTEM COMPRISING A DOUBLE FLOW TURBOREACTOR ENGINE.
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机译:集成了双流涡轮增压发动机的专用系统。
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摘要
An integrated propulsion system with a turbojet engine, comprising a cylindrical downstream structure of a nacelle in two parts, one of which (26) is fixed and comprises a beam (20) for fixing means of attachment to the aircraft, and whose another (40) is movable between a service position and an open position facilitating maintenance.
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