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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/39093 ; 60/2261 ; 415/1212 ; 55/306|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 16 인용 특허 : 3|
In a turbojet aero-engine of the bypass type in which the compressor includes pivotally mounted blow-off valves for discharging air from the primary air flow path through the compressor to prevent surging, the compressor further includes pivoted means associated with the blow-off valves such that the pivoted means lie against the wall of the primary air flow path whenever the valves are closed or are open below a predetermined angle of opening and, when said valves are opened beyond said predetermined angle, the pivoted means are caused to project into t...
In a turboshaft bypass engine, particularly a turbojet aero-engine of the bypass type, defining a primary air flow path and a secondary air flow path, said engine including in said primary air flow path a compressor having a casing wall delimiting a part of said primary flow path, a combustion chamber in which fuel is mixed with compressed air from said compressor and burned, and a turbine driven by gases from said combustion chamber and arranged to drive said compressor, said compressor including blow-off valves disposed in said casing wall so as to be ...