FIELD: engines and pumps.
SUBSTANCE: turbojet nacelle thrust reverser comprises outer cowl and front frame. Outer cowl can displace between thrust reverser close position and thrust reverser position Said cowl can be opened to servicing position whereat it is swivelled and turned by appropriate guides related to moving cowl and arranged at pylon whereto nacelle is secured. Front frame can be mounted downstream of turbojet blower case and retained by flow deflector. Said front frame is articulated at its one section with blower case to translate along the guide after its detachment from said case. One part of flow deflector can be detached from front frame to translate there along independently.
EFFECT: simplified servicing.
12 cl, 6 dwg
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