|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-013/38 B64C-009/02 B64C-013/24 B64C-013/40|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 5|
An aircraft, a control surface arrangement, and a method of assembling an aircraft are disclosed herein. In an exemplary embodiment, the aircraft includes, but is not limited to, an airframe, a control surface, and a rotary actuator. The rotary actuator rotatably mounts the control surface to the airframe. The rotary actuator supports the control surface on the airframe and is configured to rotate the control surface with respect to the airframe when the rotary actuator is actuated. The rotary actuator is further configured to deliver torque to the contr...
1. An aircraft comprising: an airframe;a control surface; anda plurality of rotary actuators cooperating to rotatably mount the control surface to the airframe, the plurality of rotary actuators being directly mounted to the airframe and supporting the control surface on the airframe and configured to rotate the control surface with respect to the airframe when the plurality of rotary actuators is actuated, the plurality of rotary actuators further configured to be coupled to the control surface at a longitudinally intermediate position along an output s...