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    • 6. 发明公开
    • SHIFT LOCK ASSEMBLY
    • 换档锁定总成
    • EP2627965A1
    • 2013-08-21
    • EP11749671.1
    • 2011-08-18
    • Woodward HRT, Inc.
    • SWEER, Grant
    • F42B10/64
    • F42B10/64
    • A shift lock assembly includes a drive member carried by a drive shaft and configured to rotatably couple to a drive motor and a shift mechanism disposed between the drive member and a ground plate, the shift mechanism configured to move between a first position and a second position relative to the drive member and the ground plate. When disposed in the first position, the shift mechanism is configured to couple the drive shaft to the ground plate and decouple the drive shaft from the drive member to allow rotation of the drive member relative to the drive shaft. When disposed in the second position, the shift mechanism is configured to couple the drive shaft to the drive member and decouple the drive shaft from the ground plate to allow rotation of the drive shaft in response to rotation of the drive member.
    • 换档锁定组件包括驱动构件,该驱动构件由驱动轴承载并构造成可旋转地联接到驱动马达和设置在驱动构件和接地板之间的换档机构,换档机构构造成在第一位置和第二位置之间移动 相对于驱动构件和接地板。 当布置在第一位置时,换档机构构造成将驱动轴联接到接地板并且将驱动轴与驱动构件分离以允许驱动构件相对于驱动轴旋转。 当布置在第二位置时,换档机构构造成将驱动轴联接到驱动构件并且将驱动轴与接地板分离以允许驱动轴响应于驱动构件的旋转而旋转。
    • 7. 发明公开
    • Multi-stage fin deployment assembly
    • Mehrstufige Flosseneinsatzanordnung
    • EP2416104A2
    • 2012-02-08
    • EP11004470.8
    • 2011-06-01
    • Woodward HRT, Inc.
    • Palani, Kumaraguru PoonamalliBurt, Raymond Lee
    • F42B10/14
    • F42B10/14Y10T16/5385
    • A multi-stage fin deployment assembly (26) includes a rotary actuator (30) configured to release a first spring-loaded stage (32) that, when deployed, releases a second spring-loaded stage (34) to deploy a set of deployable member (24) or fins. By chaining these spring-loaded stages (32,34) together, a relatively small input force, as provided by the rotary actuator (30), causes the second spring-loaded stage (34) to generate a relatively large output force on the fins (24). This multistage force magnification makes it possible for the deployment assembly (26) to utilize smaller actuators (30) that require less power and take up less space, compared to conventional locking mechanisms.
    • 多级翅片展开组件(26)包括旋转致动器(30),其被配置为释放第一弹簧加载台(32),所述第一弹簧加载台(32)在展开时释放第二弹簧加载台(34)以部署一组可部署 成员(24)或鳍。 通过将这些弹簧加载级(32,34)链接在一起,由旋转致动器(30)提供的相对较小的输入力使得第二弹簧加载级(34)在翅片上产生相对较大的输出力 (24)。 与常规的锁定机构相比,这种多级力放大使得部署组件(26)能够利用较小的致动器(30),其需要更少的功率并占据更少的空间。