发明名称 Rotary actuated high lift gapped aileron
摘要 A rotary actuated high lift gapped aileron system and method are presented. A high lift gapped aileron couples to an airfoil at a hinge line and changes a camber of the airfoil. A rotary actuator coupled to the high lift gapped aileron produces a rotary motion of the high lift gapped aileron in response to an actuation command. A droop panel positioned over the hinge line enhances lift of the high lift gapped aileron. A cove lip door positioned under the hinge line provides an airflow over the high lift gapped aileron. A deployment linkage mechanism coupled to the high lift gapped aileron positions the droop panel and the cove lip door in response to the rotary motion.
申请公布号 US9108715(B2) 申请公布日期 2015.08.18
申请号 US201213482537 申请日期 2012.05.29
申请人 THE BOEING COMPANY 发明人 Kordel Jan A.;Sakurai Seiya
分类号 B64C3/50;B64C1/10 主分类号 B64C3/50
代理机构 Ameh IP 代理人 Ameh IP ;Toosi Elahe;Campbell Lowell
主权项 1. A rotary actuated high lift gapped aileron system, comprising: a high lift gapped aileron coupled to an airfoil at a hinge line; a rotary actuator coupled to the high lift gapped aileron at the hinge line, the rotary actuator operable to produce a rotary motion to rotate the high lift gapped aileron about the hinge line in response to an actuation command; a droop panel positioned over the hinge line; a cove lip door positioned under the hinge line; and a deployment linkage mechanism coupled to the high lift gapped aileron and operable to position the droop panel and the cove lip door in response to the rotary motion.
地址 Chicago IL US