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 |