The aircraft can have an aircraft engine and a cowl, the engine having an engine part disposed within the cowl, the cowl having a cowl section movable relative to a remainder of the cowl, the engine further having a gas path duct internal to the cowl with a first portion and a cooperating second portion, the second portion mounted to the cowl section, the cowl section moveable between a first position in which the first portion and the second portion are in fluid flow communication with one another and a second position in which the cowl section and the second portion are moved away from the first portion, wherein in the first position at least the second portion obstructs external access to the engine part and in the second position at least the second portion is displaced to permit external access to the engine part.
Moveable aircraft cowl and bypass section
2021-01-26
Patent
Elektronische Ressource
Englisch
Moveable Cowl Control for Increased Hypersonic Performance
British Library Conference Proceedings | 1998
|Testing aircraft cowl fasteners
Engineering Index Backfile | 1942
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