F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 3/06 (2006.01) F02K 1/09 (2006.01) F02K 1/28 (2006.01) F02K 1/30 (2006.01) F02K 1/32 (2006.01) F02K 1/34 (2006.01) F02K 1/70 (2006.01) F02K 1/72 (2006.01)
Patent
CA 2656279
The subject of the invention is a method aimed at reducing, cancelling or reversing the thrust generated by at least one air stream leaving a power plant of an aircraft by deflecting at least some of the stream liable to contribute to the thrust, characterized in that it consists in injecting a fluid termed the thrust-reversal fluid into the power plant in such a way as, through an entrainment effect, to deflect at least some of the stream liable to contribute to the thrust from inside the nacelle toward the outside of the nacelle.
L'objet de l' invention est un procédé visant a réduire, annuler ou inverser Ia poussée générée par au moins un flux d'air sortant d'un ensemble propulsif (14) d'un aéronef en déviant au moins une partie du flux (Fi) susceptible de participer à Ia poussée. Il consiste à injecter au niveau (30) de l' ensemble propulsif un fluide (F1,F2,F3) appelé fluide d' inversion de poussée pour dévier par un effet d' entraînement, depuis I'intérieur de Ia nacelle (12) en direction de l'extérieur de Ia nacelle, au moins une partie (Fi') du flux susceptible de participer à Ia poussée.
Bulin Guillaume
Oberle Patrick
Surply Thierry
Airbus France
Airbus Operations Sas
Robic
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