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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||364/43101 ; 60/702 ; 244/76R ; 244/194|
|발명자 / 주소|
|인용정보||피인용 횟수 : 11 인용 특허 : 3|
An apparatus and method for compensating for asymmetrically produced total engine thrust caused by an engine failure in a multiengine aircraft. The presence of asymmetric total thrust is detected by monitoring aircraft performance parameters, including engine manifold pressures, airspeed, roll angle and yaw. When an engine failure resulting in the production of asymmetric thrust is detected at air speeds below a minimum controllable air speed for the aircraft, and during large aircraft bank angles, the power output from an operating engine is reduced to ...
An apparatus for limiting adverse yaw caused by asymmetrically produced total thrust in a multiengine aircraft, comprising: asymmetrical thrust detector means including engine power measurement means for measuring engine power outputs from each engine and for generating signals indicative of the corresponding thrust developed thereby; aircraft attitude detector means for detecting aircraft attitude and producing a signal responsive thereto; and control means responsive to said signals from said asymmetric thrust detector means and said aircraft attitude ...