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    • 1. 发明授权
    • External portable propeller rotator
    • 外部便携式螺旋桨旋转器
    • US4131249A
    • 1978-12-26
    • US863984
    • 1977-12-23
    • Ronald S. Watson
    • Ronald S. Watson
    • B64F1/34
    • B64F1/34
    • A device for starting an aircraft engine which is capable of being started by rotating a propeller connected to the crankshaft of the engine. The device comprises an anchor for fixedly positioning on the landing surface below the propeller; this anchor can be held in place by a portion of the aircraft itself; in one case, the nose wheel and in another case, a separate extension arrangement. A holding device is provided for holding the propeller and crankshaft of the engine against rotation in a proper starting position while a rotative device is provided for placing a biasing force on the propeller for rotating it. When desired, the holding device is remotely released and the propeller is pulled through the compression stroke by the rotative device and rotated in a manner to start the engine by the rotation of the crankshaft. Each of the holding device and rotative device has a propeller tip cap for connection to the propeller, while the other ends are fixed to the anchor.
    • 一种用于启动飞行器发动机的装置,其能够通过旋转连接到发动机曲轴的螺旋桨而起动。 该装置包括用于固定地定位在螺旋桨下方的着陆表面上的锚固件; 该锚可以由飞机本身的一部分保持在适当位置; 在一种情况下,前轮,在另一种情况下,单独的延伸装置。 提供一种保持装置,用于在适当的起始位置保持发动机的螺旋桨和曲轴旋转,同时提供用于在螺旋桨上施加偏置力以使其旋转的旋转装置。 当需要时,保持装置被远程释放,螺旋桨通过旋转装置被拉动通过压缩行程,并且通过曲轴的旋转以旋转方式启动发动机。 保持装置和旋转装置中的每一个具有用于连接到螺旋桨的螺旋桨梢帽,而另一端固定到锚固件。
    • 3. 发明授权
    • Anchor device for propeller rotator
    • 螺旋桨旋转器锚固装置
    • US4296898A
    • 1981-10-27
    • US974169
    • 1978-12-21
    • Ronald S. Watson
    • Ronald S. Watson
    • B64F1/12B64F1/34B64D31/04B64F1/16
    • B64F1/34B64F1/12
    • A device for starting an aircraft engine which is capable of being started by rotating a propeller connected to the crankshaft of the engine. The device comprises an anchor device for fixedly positioning on the landing surface below the propeller; this anchor device can be held in place by a portion of the aircraft itself; in one case, the nose wheel and in another case, a separate extension arrangement. A holding device is provided for connection to the anchor device for holding the propeller and the crankshaft of the engine against rotation in a proper starting position while a rotative device is provided for connection to the anchor device for placing a biasing force on the propeller for rotating it. The anchor device has forwardly extending arms, or members, with an attaching device fixed below the propeller, the holding device and rotative device are each fixed between the propeller and the attaching device. The arms, or members, can be made adjustable to adapt to different width tires and can be foldable lengthwise and in a sidewise overlapping manner to be compact for storing.
    • 一种用于启动飞行器发动机的装置,其能够通过旋转连接到发动机曲轴的螺旋桨而起动。 该装置包括用于固定地定位在螺旋桨下方的着陆表面上的锚固装置; 该锚装置可以由飞机本身的一部分保持在适当位置; 在一种情况下,前轮,在另一种情况下,单独的延伸装置。 提供一种用于连接到锚固装置的保持装置,用于在适当的起始位置保持发动机的螺旋桨和曲轴旋转,同时提供用于连接到锚定装置的旋转装置,用于在螺旋桨上旋转偏置力 它。 锚固装置具有向前延伸的臂或构件,其​​中固定装置固定在螺旋桨下方,保持装置和旋转装置均固定在螺旋桨和附接装置之间。 臂或构件可以制成可调整以适应不同宽度的轮胎,并且可以纵向折叠并且以侧向重叠的方式可折叠成紧凑的用于存储。