发明申请
- 专利标题： SPLITTER PLATE FOR HYBRID AIRSHIP CONTROL
- 专利标题（中）： 混合飞行控制分机板
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申请号： PCT/CA2010/000631申请日： 2010-04-23
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公开(公告)号： WO2010121384A1公开(公告)日： 2010-10-28
- 发明人: DELAURIER, James D.
- 申请人： SOLARSHIP , DELAURIER, James D.
- 申请人地址： Suite 226 366 Adelaide Street East Toronto , Ontario M5A 3X9 CA
- 专利权人： SOLARSHIP,DELAURIER, James D.
- 当前专利权人： SOLARSHIP,DELAURIER, James D.
- 当前专利权人地址： Suite 226 366 Adelaide Street East Toronto , Ontario M5A 3X9 CA
- 代理机构： POWELL, Matthew, D. et al.
- 优先权： US12/429,542 20090424
- 主分类号： B64B1/02
- IPC分类号： B64B1/02 ; B64C13/50 ; B64C31/00
摘要：
A hybrid airship comprises a non-rigid body having a delta-wing shape and an airfoil cross-section. The body is shaped for generating aerodynamic lift during forward flight, and contains a gas for generating buoyancy lift. At least one splitter plate is pivotally connected along a trailing edge of the body. The splitter plate is configured to be controllably pivoted for controlling the airship.
