F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 1/54 (2006.01) F02K 1/60 (2006.01)
Patent
CA 2249072
A turbine engine thrust reverser comprises a moveable component composed of two internal clamshells (12) mounted on fixed pivots (18) of the fixed structure (1) and of an annular structure (11) moveable axially constituting the outer downstream component part (13) of the nacelle and in forward thrust, the downstream part (15) of the radially outer wall of the flow duct, forming the trailing edge and covering the said clamshells (12) which constitute a part of the said radially outer flow duct wall.
Un inverseur de poussée de turboréacteur comporte une partie mobile composée de deux coquilles internes (12) montées sur des pivots fixes (18) de la structure fixe (1) et d'une structure annulaire (11) déplaçable axialement constituant la partie externe (13) aval de la nacelle et en jet direct, la partie aval (15) de la paroi radialement externe du canal de veine du flux, en formant le bord de fuite et en recouvrant lesdites coquilles (12) qui constituent une partie de ladite paroi radialement externe de veine de flux.
Metezeau Fabrice Henri Emile
Vauchel Guy Bernard
Goudreau Gage Dubuc
Hispano-Suiza Aerostructures
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