Passive aerodynamic sonic boom suppression for supersonic...

Details Passive aerodynamic sonic boom suppression for supersonic... Passive aerodynamic sonic boom suppression for supersonic...

B - Operations, Transporting

64

C

B64C 30/00 (2006.01) B64C 23/04 (2006.01)

Patent

CA 2398528

Sonic boom suppression apparatus for an aircraft (100) including a nose portion (102) having convex upper surfaces and a flat underside, slotted portions on the fuselage (106) or wings (104) of the aircraft, shock cancellation surfaces incorporated in the engine portion (108) of the aircraft, and area/lift distribution tailoring, all of which are preferably used concomitantly.

La présente invention concerne un appareil de suppression de bang supersonique pour un avion (100) comportant un nez (102) à surfaces supérieures convexes et à face inférieure plate, des parties fendues sur le fuselage (106) ou les ailes (104) de l'avion, des surfaces d'absorption de chocs présentes dans la partie moteur (108) de l'avion, et un répartiteur de portance, le tout utilisé de préférence simultanément.

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