CA2789329C - Systeme d'echappement guide a rotor basculant
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Systeme d'echappement guide a rotor basculant
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Publication number
CA2789329C
CA2789329CCA 2789329CA2789329ACA2789329CCA 2789329 CCA2789329 CCA 2789329CCA 2789329 CA2789329 CA 2789329CA 2789329 ACA2789329 ACA 2789329ACA 2789329 CCA2789329 CCA 2789329C
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CA
Canada
Prior art keywords
exhaust
nacelle
exhaust system
exhaust duct
primary
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Bell Helicopter Textron Inc
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Bell Helicopter Textron Inc
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Publication date
Application filed by Bell Helicopter Textron IncfiledCriticalBell Helicopter Textron Inc
Publication of CA2789329A1publicationCriticalpatent/CA2789329A1/fr
Application grantedgrantedCritical
Publication of CA2789329CpublicationCriticalpatent/CA2789329C/fr
Le système déchappement se situe sur chaque nacelle dun aéronef à rotor basculant. Le système déchappement comprend une buse de vecteur qui effectue une rotation sélective par rapport à chaque nacelle afin datteindre certains objectifs de rendement. La buse de vecteur peut être orientée pour offrir un rendement de vol maximal, réduire la signature infrarouge ou encore réduire ou empêcher tout chauffage au sol.
CA 27893292011-09-202012-09-06Systeme d'echappement guide a rotor basculant
ActiveCA2789329C
(fr)