发明名称 |
SYSTEM, APPARATUS AND METHOD FOR LONG ENDURANCE VERTICAL TAKEOFF AND LANDING VEHICLE |
摘要 |
A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends.
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申请公布号 |
US2013206921(A1) |
申请公布日期 |
2013.08.15 |
申请号 |
US201213397569 |
申请日期 |
2012.02.15 |
申请人 |
PADUANO JAMES DONALD;DAHLSTRAND PAUL NILS;WISSLER JOHN BROOKE;AURORA FLIGHT SCIENCES CORPORATION |
发明人 |
PADUANO JAMES DONALD;DAHLSTRAND PAUL NILS;WISSLER JOHN BROOKE |
分类号 |
B64C29/00 |
主分类号 |
B64C29/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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