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    • 4. 发明授权
    • Satellite solar generator structure comprising bracing elements between panels
    • 卫星太阳能发电机结构包括面板之间的支撑元件
    • US06909042B2
    • 2005-06-21
    • US10472865
    • 2002-03-25
    • Freddy GeyerDaniel Viale
    • Freddy GeyerDaniel Viale
    • B64G1/22B64G1/44H01L31/045H01L31/052
    • B64G1/443B64G1/222H02S30/20Y10S136/292
    • The satellite solar generator structure comprises a plurality of solar panels (PR, PS) each having a plane surface, the panels being disposed in superposition in said structure (ST), the structure including at least one rod (TI) holding said panels (PR, PS) pressed against one another, two successive panels being in contact via bearing points (AL) disposed at the peripheries of the panels. In this structure, spacers (CA) are distributed over the surfaces of the panels (PR, PS) and are disposed between pairs of successive panels in order to improve contact between two successive panels so that the structure presents better mechanical strength during the satellite launch stage. With this arrangement, a fraction of the forces is taken up by the spacers instead of being taken up by the panels, thus making it possible to optimize the solar generator, for example by reducing the weight of the panels constituting it.
    • 卫星太阳能发电机结构包括多个太阳能电池板(PR,PS),每个太阳能电池板具有一个平面,该板被叠置在所述结构(ST)中,所述结构包括至少一个保持所述面板(PR)的杆(TI) ,PS)彼此压靠,两个连续的面板通过设置在面板周边的轴承点(AL)而接触。 在这种结构中,间隔物(CA)分布在面板(PR,PS)的表面上并且设置在成对的连续面板之间,以改善两个连续面板之间的接触,使得结构在卫星发射期间呈现更好的机械强度 阶段。 通过这种布置,力的一小部分被间隔物吸收,而不是被面板吸收,从而使得可以例如通过减小构成它的面板的重量来优化太阳能发电机。
    • 5. 发明授权
    • System for extending or retracting two members and cam-locking the
members in the extended position
    • 用于延伸或缩回两个构件并将构件凸轮锁定在延伸位置的系统
    • US5699698A
    • 1997-12-23
    • US605061
    • 1996-03-05
    • Freddy Geyer
    • Freddy Geyer
    • B64G1/22B64G1/44B64G1/64G05G1/04
    • B64G1/44B64G1/22B64G1/222B64G1/64B64G1/645Y10T403/589Y10T403/591Y10T74/2063Y10T74/2101
    • A system for extending or retracting two rotationally interconnected members and locking or releasing the members in the extended position. The system includes a locking cam (4) on a shaft (5) combined with the first member (2) and connected to a drive (9). The cam is engageable with a bearing surface (8) on the second member. The drive (9) is preferably a power drive rotating the two members about their pivot axis and includes a motor (9A) with a rotational axis (17) parallel to the rotational axes (10, 11) of the cam and the shaft, the rotational axis coinciding with the pivot axis of the two members; a transmission (18) linking the motor to the shaft; and a radial linkage (19) rotating with the motor and capable of rotating the second member about the pivot axis.
    • PCT No.PCT / FR95 / 00967 Sec。 371日期:1996年3月5日 102(e)1996年3月5日PCT PCT 1995年7月19日PCT公布。 公开号WO96 / 02418 日期1996年2月1日用于延伸或缩回两个旋转互连的构件并将构件锁定或释放在延伸位置的系统。 该系统包括在与第一构件(2)组合并连接到驱动器(9)的轴(5)上的锁定凸轮(4)。 凸轮可与第二构件上的支承表面(8)接合。 驱动器(9)优选地是使两个构件围绕其枢转轴线旋转的动力驱动器,并且包括具有与凸轮和轴的旋转轴线(10,11)平行的旋转轴线(17)的马达(9A), 旋转轴线与两个构件的枢转轴线重合; 将马达与轴连接的变速器(18) 以及与所述马达一起旋转并且能够绕所述枢转轴线旋转所述第二构件的径向联动装置(19)。
    • 8. 发明授权
    • Articulated device for space vehicles, especially for temporarily
sealing the aperture of space optical instruments
    • 用于太空车辆的铰接装置,特别是临时密封空间光学仪器的孔
    • US5384661A
    • 1995-01-24
    • US835967
    • 1992-02-20
    • Freddy GeyerDominique Giraud
    • Freddy GeyerDominique Giraud
    • B64D47/08B64G1/66G02B23/16G02B5/00G02B26/02G02B23/00
    • G01J1/04B64D47/08B64G1/66G01J1/0403G01J1/044G02B26/02G02B27/0006
    • An articulated device for space vehicles, for example, for temporarily sealing the aperture of a space optical instrument. The device includes a fixed support element for mounting on the vehicle and an auxiliary element such as a temporary sealing flap mounted to pivot with respect to the fixed support element around a hinge axis between a first configuration (e.g. wherein the aperture is sealed) and a second configuration. The auxiliary element is attached, by a frangible controlled-break component for making temporary connections, to a hinge shaft whose rotation between the first and second configuration is controlled by an actuator. A torsional resilient return device is secured to the auxiliary element and to the shaft while resiliently biasing the auxiliary element to rotate it around the shaft in a predetermined direction. The shaft is substantially loosely engaged in journal bearings which are rigidly fastened to the auxiliary element.
    • PCT No.PCT / FR91 / 00494 Sec。 371日期1992年2月20日 102(e)日期1992年2月20日PCT提交1991年6月20日PCT公布。 出版物WO91 / 19645 日期为1991年12月26日。空间车辆的关节式装置,例如用于临时密封空间光学仪器的孔。 该装置包括用于安装在车辆上的固定支撑元件和辅助元件,例如安装成围绕铰链轴线相对于固定支撑元件在第一构造(例如,其中孔被密封)和第一构造之间枢转的临时密封翼片 第二配置。 辅助元件通过用于进行临时连接的易碎控制断开部件连接到铰链轴,其中第一和第二构造之间的旋转由致动器控制。 扭转弹性返回装置固定到辅助元件和轴上,同时弹性地偏置辅助元件以使它围绕轴沿预定方向旋转。 轴基本上松动地接合在刚性地紧固到辅助元件上的轴颈轴承中。
    • 9. 发明授权
    • Cam locking system
    • CAM锁定系统
    • US5108216A
    • 1992-04-28
    • US580112
    • 1990-09-10
    • Freddy GeyerJean-Pierre ScheffterGerard Vezain
    • Freddy GeyerJean-Pierre ScheffterGerard Vezain
    • B64G1/64B64G1/66E05C3/12F16B2/18
    • E05C3/124B64G1/645B64G1/66Y10S403/08Y10T24/44368Y10T292/225Y10T403/608Y10T403/76Y10T74/2101
    • A locking system is disclosed comprising two elements connected mechanically together so as not to be able to move apart, as well as a cam mounted for rotation on the first of said elements and having a contact surface pressing against a bearing face carried by the second of said elements.According to the invention, said contact surface of said cam has at least approximately a profile in the form of a logarithmic spiral, whereas said bearing face is flat and said cam may rotate about a hub on the axis of which is located the origin of said logarithmic spiral, said hub being mounted for rotation on said first element about an off-centered axis of rotation opposite said contact surface of said cam. Resilient means are provided for rotating said cam in a first direction such that said contact surface moves towards said bearing face.
    • 公开了一种锁定系统,其包括机械地连接在一起以便不能移动的两个元件,以及安装成用于在所述元件中的第一个上旋转的凸轮,并且具有压靠由第二个元件承载的支承面的接触表面 说要素 根据本发明,所述凸轮的所述接触表面具有至少大致为对数螺旋形的轮廓,而所述支承面是平坦的,并且所述凸轮可以围绕轴线旋转,所述轮毂的轴线位于所述毂 对数螺旋,所述轮毂安装成围绕与所述凸轮的所述接触表面相对的偏心轴线旋转在所述第一元件上。 提供弹性装置用于沿第一方向旋转所述凸轮,使得所述接触表面向所述支承面移动。