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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/39092 ; 55/306 ; 415/9 ; 222/541|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 4 인용 특허 : 4|
An air intake for a gas turbine engine compressor comprises an arcuate primary duct which is in communication with the compressor of the gas turbine engine and which is provided with frangible wall portion. The frangible wall portion provides a barrier between the primary duct and a secondary duct and is so positioned and adapted as to be impacted and penetrated by a foreign body, such as a bird, which is above a predetermined weight and which has been ingested through the inlet of the primary duct. After penetrating the wall portion the foreign body pas...
An air intake for a compressor of a gas turbine engine comprising: a primary duct defined by an annular wall, said primary duct having an air inlet for receiving air and an air outlet arranged to deliver air therefrom to the compressor of the gas turbine engine, said primary duct being at least partially arcuate in cross-sectional form whereby said air outlet is offset laterally from said air inlet and air flowing through said duct follows a tortuous path, a portion of said annular wall of said primary duct being frangible and being arranged to be impact...