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    • 8. 发明申请
    • GAS SPRING ASSEMBLIES AND INTERNAL MISALIGNMENT MOUNTS FOR SAME
    • 气体弹簧组件和内部缺口对齐方式
    • US20160101663A1
    • 2016-04-14
    • US14888525
    • 2014-05-01
    • FIRESTONE INDUSTRIAL PRODUCTS COMPANY, LLC
    • Joshua R. Leonard
    • B60G15/12F16F9/04
    • B60G15/12B60G2202/314B60G2204/126F16F9/0472F16F9/084F16F2230/0052
    • An assembly (AS1) in accordance with the subject matter of the present disclosure can include a gas spring (200), an internally-mounted device (300) and a mounting assembly (400, 500) operatively connecting the internally-mounted device to an end member (202, 204) of the gas spring (200). The mounting assembly (400, 500) can permit at least a portion of the internally-mounted device to undergo 360 degree rotational and pivotal displacement relative the end member (202, 204) of the as spring (200). The mounting assembly (400, 500) can include a device mount (402, 502) that can be operatively secured to the internally-mounted device (300) and a retainer (404, 504) that is secured to the end member (202, 204) and operatively retains the device mount (402, 502) adjacent the end member (202, 204). The device mount (402, 502) and the retainer (404, 504) can include complimentary semi-spherical surfaces that permit the relative movement between internally-mounted device (300) and the end member (202, 204) of the gas spring (200).
    • 根据本公开的主题的组件(AS1)可以包括气弹簧(200),内部安装的装置(300)和安装组件(400,500),其将内部安装的装置可操作地连接到 气弹簧(200)的端部件(202,204)。 安装组件(400,500)可以允许内部安装的装置的至少一部分相对于弹簧(200)的端部构件(202,204)经历360度的旋转和枢转位移。 安装组件(400,500)可以包括可操作地固定到内部安装的装置(300)的装置安装件(402,502)和固定到端部构件(202)的保持器(404,504) 204)并且可操作地保持所述装置安装件(402,502)邻近所述端部构件(202,204)。 装置安装件(402,502)和保持器(404,504)可以包括互补的半球形表面,其允许内部安装的装置(300)和气体弹簧的端部构件(202,204)之间的相对运动 200)。
    • 9. 发明申请
    • ADAPTOR AND PAYLOAD LAUNCH VEHICLE
    • 适配器和载货启动车
    • US20130284857A1
    • 2013-10-31
    • US13995325
    • 2011-12-15
    • Toshihiro Tombe
    • Toshihiro Tombe
    • B64G1/64
    • B64G1/641B64G2001/228F16F15/02F16F15/04F16F15/073F16F2230/0052
    • An object is to provide an adaptor that can attenuate a vibration acting on a payload using a simple structure, and a payload launch vehicle. The adaptor (1) according to the invention controls a vibration of the payload housed in the payload launch vehicle, and is provided between the payload and a rocket portion. The adaptor (1) includes a cylinder member having a double structure including an outer cylinder (11) and an inner cylinder (12); a first elastic member (21) coupled to the outer cylinder (11) and the inner cylinder (12) at one end of the cylinder member; and a second elastic member (22) coupled to the outer cylinder and the inner cylinder at the other end of the cylinder member. The adaptor (1) is linked to the payload on the inner cylinder side or the outer cylinder side on one end side of the cylinder member, and linked to a leading end of the rocket portion on the outer cylinder side or the inner cylinder side on the other end side of the cylinder member.
    • 目的是提供一种适配器,其可以使用简单的结构和有效载荷运载火箭衰减作用在有效载荷上的振动。 根据本发明的适配器(1)控制装载在有效载荷运载火箭中的有效载荷的振动,并且设置在有效载荷和火箭部分之间。 适配器(1)包括具有包括外筒(11)和内筒(12)的双重结构的气缸构件; 在所述气缸构件的一端处联接到所述外筒(11)和所述内筒(12)的第一弹性构件(21) 以及在所述气缸构件的另一端处联接到所述外筒和所述内筒的第二弹性构件(22)。 适配器(1)与气缸构件的一端侧的内筒侧或外筒侧的有效载荷连接,与外筒侧或内筒侧的火箭部的前端连接 气缸构件的另一端侧。