Title:
エレボン制御システム
Document Type and Number:
Japanese Patent JP5886201
Kind Code:
B2
Abstract:
A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100,400,1000,1500) configured to control pitch, roll, and/or yaw via airfoils (141,142,1345,1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621,622). Embodiments include one or more rudder elements (1045,1046,1145,1146,1245,1345,1346,1445,1446,1545,1546) which may be rotatably attached and actuated by an effector member (1049,1149,1249,1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements.
Inventors:
Mirages, Carlos Thomas
Plum, Nick
Tao, Shu Tony
Olson, Nathan
Plum, Nick
Tao, Shu Tony
Olson, Nathan
Application Number:
JP2012528910A
Publication Date:
March 16, 2016
Filing Date:
September 09, 2010
Export Citation:
Assignee:
AEROVIRONMENT,INC.
International Classes:
B64C3/56; B64C9/02; B64C13/28; B64C39/02; F15B15/00
Domestic Patent References:
| JP1028096A | ||||
| JP9026300A | ||||
| JP7089492A |
Foreign References:
| US20050218260 | ||||
| US3223361 | ||||
| US20090072085 | ||||
| US5271579 |
Attorney, Agent or Firm:
Patent business corporation Kita Aoyama International