发明授权
- 专利标题： Fast-pivot missile flight control surface
- 专利标题（中）： 快速导弹飞行控制面
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申请号： US11067038申请日： 2005-02-25
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公开(公告)号： US07325769B1公开(公告)日： 2008-02-05
- 发明人: Paul E. Harnisch , Robert E. Winkel
- 申请人： Paul E. Harnisch , Robert E. Winkel
- 申请人地址： US NJ Morristown
- 专利权人： Honeywell International, Inc.
- 当前专利权人： Honeywell International, Inc.
- 当前专利权人地址： US NJ Morristown
- 代理机构： Ingrassia, Fisher & Lorenz
- 主分类号： F42B10/64
- IPC分类号： F42B10/64
摘要：
Methods and apparatus are provided for a missile that includes a housing, a fin, and a first actuator. The housing has a slot formed therethrough. The fin is disposed within the housing proximate the slot. The first actuator is coupled to the fin and configured to selectively move the fin at least partially in and out of the housing through the slot.
公开/授权文献
- US20080029642A1 FAST-PIVOT MISSILE FLIGHT CONTROL SURFACE 公开/授权日：2008-02-07
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