B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/10 (2006.01) B64D 33/02 (2006.01) B64D 33/04 (2006.01) F02K 3/00 (2006.01) F02K 3/02 (2006.01) F02K 3/075 (2006.01) F02K 3/12 (2006.01)
Patent
CA 2389529
A variable cycle propulsion system for a supersonic airplane, the system comprising at least one engine (1) having at least one compressor and capable of generating thrust for supersonic flight speeds, and at least one auxiliary propulsion assembly (12) separate from said engine, and capable of generating additional thrust for takeoff, landing, and subsonic cruising speeds, at least one pipe (20) connecting the engine (1) to the auxiliary propulsion assembly (12) to convey thereto compressed air produced by the compressor so as to enable the auxiliary propulsion assembly to generate additional thrust for takeoff, landing, and subsonic cruising flight, there being at least one valve enabling the pipe to be closed off for supersonic cruising flight.
Dispositif de propulsion à cycle variable pour avion supersonique comprenant au moins un propulseur (1) ayant au moins un compresseur et capable de générer une poussée pour les vitesses de vol supersonique, au moins un ensemble propulsif auxiliaire (12), distinct du propulseur, capable de générer un complément de poussée pour le décollage, l'atterrissage et les vitesses de vol subsonique, au moins une conduite (20) reliant le propulseur (1) à l'ensemble propulsif auxiliaire (12) pour acheminer à ce dernier de l'air comprimé produit par le compresseur afin que l'ensemble propulsif auxiliaire génère un complément de poussée pour le décollage, l'atterrissage et le vol en croisière subsonique, et au moins une vanne permettant d'obturer la conduite pour le vol en croisière supersonique.
Franchet Michel
Laugier Yann
Loisy Jean
Goudreau Gage Dubuc
Snecma
Snecma Moteurs
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