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Control system for controlling collective and cyclic pitch of rotor blades of a multi-blade rotor in a rotary-wing aircraft
Control system for controlling collective and cyclic pitch of rotor blades of a multi-blade rotor in a rotary-wing aircraft
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机译：用于控制旋翼飞机中多翼旋翼的旋翼桨叶集体和周期性桨距的控制系统
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摘要
The invention is related to a control system for controlling collective and cyclic pitch of rotor blades of a multi-blade rotor 1a in a rotary-wing aircraft, the control system comprising a swash plate assembly with at least one non-rotating plate and at least one rotating plate that is mounted rotatably to the at least one non-rotating plate, the at least one rotating plate and the at least one non-rotating plate being mounted to a non-rotating sliding sleeve, wherein a spherical bearing is provided on the non-rotating sliding sleeve, wherein at least one non-rotating stop arm is provided for non-rotatably connecting the at least one non-rotating plate to the non-rotating sliding sleeve.
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机译：本发明涉及一种用于控制旋翼飞机中的多叶片转子 1 a 的转子叶片的共同桨距和周期桨距的控制系统，该控制系统包括一种旋转斜盘组件，其具有至少一个非旋转板和至少一个旋转板，所述旋转板可旋转地安装到所述至少一个非旋转板，所述至少一个旋转板和所述至少一个非旋转板安装到一种不旋转的滑动套筒，其中，在所述不旋转的滑动套筒上设置有球形轴承，其中，设置有至少一个不旋转的止动臂，用于将所述至少一个不旋转的板不可旋转地连接至所述不旋转的板。滑动套。
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