F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 1/40 (2006.01) F02C 7/04 (2006.01) F02K 1/52 (2006.01)
Patent
CA 2703602
Embodiments of the invention relate to a supersonic nacelle design employing a bypass flow path internal to the nacelle and around the engine. By shaping the nacelle, embodiments of the invention may function to reduce sonic boom strength, cowl drag, and/or airframe interference drag. Embodiments of the invention may also function to improve total pressure recovery and/or total thrust of the primary flow path through the engine.
Des modes de réalisation de l'invention concernent un modèle de nacelle supersonique utilisant un canal de dérivation à l'intérieur de la nacelle et autour du moteur. Lors du façonnage de la nacelle, les modes de réalisation de l'invention peuvent permettre de réduire la résistance au bang supersonique, la traînée du carénage et/ou la traînée d'interférence de la cellule. Les modes de réalisation de l'invention peuvent également permettre d'améliorer la récupération totale de pression et/ou la poussée totale du canal primaire à travers le moteur.
Finlayson & Singlehurst
Gulfstream Aerospace Corporation
LandOfFree
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