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SYSTEM AND METHOD FOR ALLEVIATING STRUCTURAL LOADS ON A PIVOTING MAIN LANDING GEAR OF AN AIRCRAFT IN A PIVOT TURN MANEUVER
SYSTEM AND METHOD FOR ALLEVIATING STRUCTURAL LOADS ON A PIVOTING MAIN LANDING GEAR OF AN AIRCRAFT IN A PIVOT TURN MANEUVER
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机译:用于缓解在枢轴转动机动的飞机的枢转主着陆齿轮上的结构载荷的系统和方法
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摘要
There is provided a pivot turn load alleviation (PTLA) brake system for alleviating structural loads on a pivoting main landing gear of an aircraft in a pivot turn maneuver. The PTLA brake system includes a brake control system operatively coupled to at least two main landing gear, each having two or more wheels. The PTLA brake system further includes a PTLA brake inhibit subsystem coupled to the brake control system. The subsystem inhibits braking of one or more of the two or more wheels of the pivoting main landing gear, in the pivot turn maneuver, so that at least one wheel of the two or more wheels is in an unbraked state, and a remaining number of the two or more wheels are in a braked state. The PTLA brake system alleviates structural loads, and reduces wear on the at least one wheel that is in the unbraked state.
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