|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/76R ; 244/178 ; 244/195 ; 364/434|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 15 인용 특허 : 0|
According to the invention each of the pitch and thrust commands is a linear combination, inter alia, of the trim setting and of the speed setting, and the control provided by the aircraft joystick is pitch rate control. Protection may be provided with respect to trim, angle of incidence, and vertical load factor.
A pitch and thrust control system for an aircraft the system comprising: first airfoils for pitch control actuated from a first actuator member associated with a first transducer delivering a first electrical signal representative of the trim setting: at least one engine controlled from a second actuator member associated with a second transducer delivering a second electrical signal representative of a speed setting for said aircraft; a plurality of second airfoils capable of taking up different determined positions as a function of each stage of flight...