Invention Grant
US08998132B2 Aerodynamic wing load distribution control 有权
气动翼载荷分布控制

Aerodynamic wing load distribution control
Abstract:
An aerodynamic wing load distribution control apparatus for increasing flight performance of an aircraft. The apparatus may include an aileron uprigger connectable to left and right ailerons of an aircraft and configured to uprig the left and the right wing ailerons of such aircraft. An operator interface communicates operator command inputs to the aileron uprigger. The aileron uprigger includes left and right actuators actuable in response to command inputs received from an operator through the operator interface and are connectable into respective left and right aileron control linkages of an aileron actuator assembly.
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