ENGINE NACELLE

A nacelle for a gas turbine jet engine (10) for an aircraft includes flow disruptors (42, 46, 48, 64) to provide boundary layer turbulence when the engine is exposed to air flow that is obtuse to direction of travel of the engine.

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Bibliographische Detailangaben
Hauptverfasser:	Fulayter, Roy David, Smith III, Crawford F
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A nacelle for a gas turbine jet engine (10) for an aircraft includes flow disruptors (42, 46, 48, 64) to provide boundary layer turbulence when the engine is exposed to air flow that is obtuse to direction of travel of the engine.