首页> 外国专利> METHOD AND SYSTEM FOR DETERMINING THE LONGITUDINAL POSITION OF THE CENTRE OF GRAVITY OF AN AIRCRAFT EQUIPPED WITH AN ADJUSTABLE HORIZONTAL TAIL UNIT AND APPLICATION TO THE MONITORING OF SAID CENTRE OF GRAVITY IN THE NEIGHBOURHOOD OF THE AIRCRAFT AERODYNAMIC CENTRE

METHOD AND SYSTEM FOR DETERMINING THE LONGITUDINAL POSITION OF THE CENTRE OF GRAVITY OF AN AIRCRAFT EQUIPPED WITH AN ADJUSTABLE HORIZONTAL TAIL UNIT AND APPLICATION TO THE MONITORING OF SAID CENTRE OF GRAVITY IN THE NEIGHBOURHOOD OF THE AIRCRAFT AERODYNAMIC CENTRE

机译:确定装有可调水平尾翼的飞机重力中心的纵向位置的方法和系统,并将其用于监测航空气动中心近邻的重力重力中心

摘要

abbreviated descriptionmethod and system for the determination of thelongitudinal position of the centre of gravity of the aircraft.adjustable engine fitted with a horizontal tailplane.the invention is remarkable in that, at a point ofthe flight for which the aircraft is in equilibrium with itselevator engineering extensionthe horizontal tailplane and with adjustable centregravity is located in the vicinity of the focus of the aircraft.we calculate the position of the center of gravity from:the position of the home of the aircraft; the measurethe horizontal tailplane was an adjustable.the first function of the engines of the aircraftand the mach number, and a second function of themach number.
机译:简短说明确定的方法和系统飞机重心的纵向位置。可调发动机,配备水平尾翼。本发明的显着之处在于飞机与其飞行处于平衡状态的飞行电梯工程扩展水平尾翼,中心可调重力位于飞机焦点附近。我们根据以下公式计算重心的位置:飞机原点的位置;的措施水平尾翼是可调的。飞机发动机的第一功能和马赫数,以及第二个功能马赫数。

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