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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/2262 ; ; 60/262 ; ; 60/232 ; 244/110 ; B|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 83 인용 특허 : 0|
A thrust reverser is provided for both modulating and reversing bypass flow discharged from a fan through a bypass duct of a turbofan gas turbine engine. The reverser includes an aft cowl joined to a forward cowl and having an aft end surrounding a core engine to define a discharge fan nozzle of minimum flow throat area. The aft cowl is axially translatable relative to the forward cowl from a first position fully retracted against the forward cowl, to a second position partially extended from the forward cowl, and to a third position fully extended from ...
A thrust reverser for modulating and reversing bypass flow discharged from a fan through a bypass duct defined between a core engine and a fan nacelle comprising: an aft cowl of said nacelle joined to a forward cowl thereof and having an aft end defining with a core cowl surrounding said core engine a discharge fan nozzle of minimum flow throat area at an aft end of said bypass duct; a plurality of cascade turning vanes disposed between said aft and forward cowls; means for axially translating said aft cowl relative to said forward cowl from a first posi...