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Improvements in or relating to means for providing 'feel' in power-operated flying control systems for aircraft

机译:飞机动力操纵飞行控制系统中提供“感觉”的装置的改进或与之有关的改进

摘要

742,383. Controlling aircraft. BOULTON PAUL AIRCRAFT, Ltd. Oct. 9, 1952 [Oct. 10, 1951], No. 23593/51. Class 4. Means for providing " feel " in poweroperated flying control systems for aircraft include means for opposing the displacement of the control column in a direction to give lateral control, by a force controlled by a Machmeter on the aircraft so that the opposing force increases with increase in Mach number. The pilot's control column 1 is movable about axes a-a, e-e to operate links A and E connected respectively to servo mechanisms for operating the ailerons and elevators. Connected also to the column 1 are rods 2a, 2e, the free ends of which carry pins engaging in slots 7a, 7e in levers 3a, 3e respectively secured to torsion bars 4a, 4e. The pins on the ends of the rods 2a, 2e are secured to actuators 8a, 8e, the actuator 8e being controlled by a transmitter 9 driven by a rod 10 connected to the dynamic pressure capsule 11 of a Machmeter, and the actuator 8s being operated by a transmitter 12 into which is fed a signal derived from the divider and converter 13 of the Machmeter 15. Trimmer actuators 5a, 5e are connected to levers secured to the ends of the torque tubes 4a, 4e remote from the levers 3a, 3e.
机译:742,383。控制飞机。 BOULTON PAUL AIRCRAFT,Ltd. 1952年10月9日[Oct. 1951年10月],第23593/51号。第4类。在飞机的动力飞行控制系统中提供“感觉”的装置包括用于通过飞行器上的测速仪控制的力来抵抗控制柱在进行侧向控制的方向上的位移的装置,从而使相反的力增加随着马赫数的增加。飞行员的控制柱1可绕轴a-a,e-e移动,以操作分别连接到用于操纵副翼和电梯的伺服机构的连杆A和E。杆2a,2e也连接到柱1,杆2a,2e的自由端带有销,该销接合在分别固定到扭杆4a,4e的杠杆3a,3e中的狭槽7a,7e中。杆2a,2e的端部上的销钉固定到致动器8a,8e,致动器8e由变送器9控制,该变送器由连接到转速表的动压胶囊11的杆10驱动,致动器8s被操作。微调致动器5a,5e连接到固定在扭矩管4a,4e的远离杠杆3a,3e的端部的杠杆上,通过发射机12将来自转速表15的除法器和转换器13的信号馈入其中。

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