公开(公告)号：US3735942A

公开(公告)日：1973-05-29

申请号：US3735942D

申请日：1971-03-04

申请人： CENTRE NAT ETD SPATIALES

发明人： PALZ W

IPC分类号： B64G1/22 ,  B64G1/44 ,  H01L15/02

CPC分类号： B64G1/222 ,  B64G1/443 ,  H02S30/20 ,  Y10S136/292

摘要： A solar generator has flexible panels adapted to be deployed by means of extensible frame means. The flexible active material of each panel is so arranged and the extensible frames so operated that the development of the panel takes place not only in the longitudinal direction away from the base, but also in the transverse direction. The panels are adapted for use on satellites or other space vehicles.

摘要翻译： 太阳能发电机具有适于通过可伸缩的框架装置部署的柔性板。 每个面板的柔性活性材料如此布置，并且可伸展框架的操作使得面板的发展不仅在远离基座的纵向方向上而且在横向上发生。 这些面板适用于卫星或其他太空飞行器。

公开(公告)号：US3715600A

公开(公告)日：1973-02-06

申请号：US3715600D

申请日：1971-11-22

申请人： NASA

发明人： FLETCHER J ,  WEINGART J ,  YASUI R

IPC分类号： B64G1/44 ,  B64G1/64 ,  H01L31/042 ,  B64G9/00 ,  F03G7/02

CPC分类号： B64G1/645 ,  B64G1/443 ,  H01L31/042 ,  Y02E10/50 ,  Y10S136/292

摘要： A solar cell stack, for use in a spacecraft or the like, is disclosed. In the stack only the top solar cell panel is exposed to solar energy to provide electrical power. Except the top panel each panel is covered from exposure to damaging bombarding particles by the preceding panels in the stack toward the stack top. When the exposed top panel''s performance is degraded, due to bombardment by particles or other unexpected failure, the top panel is ejected, thereby exposing the underlying panel in the stack, which not becomes the power supplying panels. Each panel in the stack is successively exposed when the panel above it is ejected.

摘要翻译： 公开了一种用于航天器等的太阳能电池堆。 在堆叠中，仅顶部太阳能电池板暴露于太阳能以提供电力。 除了上面板之外，每个面板都覆盖着由堆叠中的前面的面板向堆叠顶部暴露于有害的轰击颗粒。 当暴露的顶板的性能降低时，由于颗粒的轰击或其他意想不到的故障，顶板被弹出，从而将下面的面板暴露在堆叠中，而不是供电板。 当其上方的面板弹出时，堆叠中的每个面板依次露出。

公开(公告)号：US3690080A

公开(公告)日：1972-09-12

申请号：US3690080D

申请日：1970-09-21

申请人： TRW INC

发明人： DILLARD PAUL A

IPC分类号： B64G1/22 ,  B64G1/44

CPC分类号： B64G1/443 ,  B64G1/222 ,  H02S30/20 ,  Y10S136/292 ,  Y10S343/02

摘要： A deployable panel for a spacecraft deployable solar array and other deployable structures. The panel has a number of panel sections hinged edge-to-edge for folding to a stowage configuration wherein the sections are disposed in confronting face-to-face relation and extension to a flat unfolded configuration wherein the panel sections are disposed in coplanar relation. Fixed to selected edges of the panels are sheets which are held flat between the panel sections in the folded configuration of the panel and curl into tubular beams for deploying the panel to unfolded configuration and/or rigidizing the panel when the latter is extended to unfolded configuration. In a solar array the sheets provide protection covers for the solar cells when the solar panel is folded. A deployable panel structure embodying the panel.

摘要翻译： 用于航天器可部署太阳能阵列和其他可部署结构的可部署面板。 面板具有多个铰接到边缘到边缘的面板部分，用于折叠到一个装载结构，其中这些部分面对着面对关系设置并延伸到平坦的展开构造，其中面板部分设置成共面关系。 固定到面板的选定边缘的是在面板的折叠构造中的平板部分之间平坦地保持的片材，并且卷曲成管状梁，用于将面板展开为展开构型和/或当面板延伸到展开构型时使其刚性化 。 在太阳能阵列中，当太阳能电池板折叠时，该片材提供太阳能电池的保护盖。 实施面板的可部署面板结构。

公开(公告)号：US3635425A

公开(公告)日：1972-01-18

申请号：US3635425D

申请日：1969-10-01

申请人： US NAVY

发明人： SWET CHARLES J

IPC分类号： B64G1/22 ,  B64G1/34 ,  B64G1/44 ,  B64G1/00

CPC分类号： B64G1/222 ,  B64G1/34 ,  B64G1/443 ,  Y10S136/292

摘要： A method for deployment of a solar cell array, conduction of generated power from the array to the satellite, and utilization of the array and deployment means as an aid for the gravitygradient stabilization of the satellite. The method envisions telescoping sections of a solar cell array being extended in orbit by an erectable mast and boom assembly. Power is carried from the array through electrically conductive booms and twin conducting masts, thereby eliminating the need for electrical wiring and associated wiring guides and connectors. The extended solar array also assists in stabilizing the satellite by providing necessary gravity-gradient restoring moments. Multiple function of equipment increases the wattage to weight ratio of the array.

摘要翻译： 用于部署太阳能电池阵列的方法，将阵列的发电功率传导到卫星，以及利用阵列和展开装置来辅助卫星的重力梯度稳定。 该方法设想太阳能电池阵列的伸缩部分通过可竖立的桅杆和吊杆组件在轨道中延伸。 电力通过导电吊杆和双导电桅杆从阵列传送，从而不需要电气布线和相关的导线引导件和连接器。 扩展的太阳能阵列还通过提供必要的重力梯度恢复力矩来帮助稳定卫星。 设备的多功能增加了阵列的瓦数与重量比。

公开(公告)号：US3559919A

公开(公告)日：1971-02-02

申请号：US3559919D

申请日：1968-06-05

申请人： BOLKOW GMBH

发明人： SASS HANS ECKHARD

IPC分类号： B64G1/00 ,  B64G1/10 ,  B64G1/26 ,  B64G1/44 ,  H01Q1/28 ,  H04B7/185

CPC分类号： H04B7/185 ,  B64G1/007 ,  B64G1/1007 ,  B64G1/26 ,  B64G1/44 ,  H01Q1/288 ,  Y10S136/292

摘要： An active communications satellite which is stabilized as to attitude and to orbit includes at least one directional antenna rigidly mounted on a body portion. The antenna part of the generated surface of the body of the satellite in the operating condition is oriented toward earth. The other parts of the surface of the body are penetrated by control engines and their connecting parts which serve to control the attitude and orbit stabilization of the satellite. Some of the control engines are enclosed in the operative condition of the satellite by at least two unfoldable solar battery areas which are mounted on pivot arm members to permit them to be swung outwardly when the satellite is in space. A fly wheel is carried by the body for the attitude stabilization of the satellite and it rotates about the axis of symmetry parallel to the antenna plane. The satellite is advantageously constructed such that the apogee motor, the fly wheel, the electronic equipment and the fuel tanks are disposed so that they will be rotationally symmetric to the axis of symmetry of the satellite.

公开(公告)号：US3532299A

公开(公告)日：1970-10-06

申请号：US3532299D

申请日：1968-02-05

申请人： TRW INC

发明人： WILLIAMSON CLYDE E ,  BAKER DONALD R

IPC分类号： B64G1/22 ,  B64G1/44 ,  B64G1/30

CPC分类号： B64G1/222 ,  B64G1/443 ,  Y10S136/292

公开(公告)号：US3459391A

公开(公告)日：1969-08-05

申请号：US3459391D

申请日：1964-02-13

申请人： NASA

发明人： HAYNOS JOSEPH G

IPC分类号： B64G1/22 ,  B64G1/44 ,  F24J2/52 ,  H01L25/03 ,  H01L31/042 ,  B64C39/02 ,  H01V1/30 ,  H02N11/00

CPC分类号： H01L25/03 ,  B64G1/222 ,  B64G1/443 ,  F24J2/5266 ,  H01L27/142 ,  H01L31/0508 ,  H01L2924/0002 ,  H02S30/20 ,  Y02E10/47 ,  Y02E10/50 ,  Y10S136/292 ,  H01L2924/00

摘要： 1,033,681. Mounting solar cells. NATIONAL AERONAUTICS & SPACE ADMINISTRATION. Jan. 1, 1965 [Feb. 13, 1964], No. 37/65. Heading H1K. A plurality of solar cells are joined mechanically and electrically by an expanded metal strip which is attached to the solar cells by a conductive adhesive. The term " expanded metal " is defined as a very thin sheet of metal which has cuts made therein and has then been pulled out transversely to the cuts to give a mesh. In a specific embodiment, Fig. 3, PN silicon devices 12 have their P-type region 13 connected to the N-type region 14 by an expanded metal strip 16 by way of tin-lead solder 19 and 20 and a thin layer of bonding material 17 and 18, e.g. Cu, Ni, Ag or Pt. The matrix 11 so formed is secured to an aluminium honeycomb 22 by a flexible adhesive 23, e.g. room temperature vulcanizing silicone rubber. In another embodiment, the matrix 11 is joined by silicone rubber to a glass fibre backing, and is incorporated in rolled form in a space satellite. In operation the rolled matrix is unrolled by telescopic arms and held rigidly in an extended position.

公开(公告)号：US3416319A

公开(公告)日：1968-12-17

申请号：US83515159

申请日：1959-08-20

申请人： ALBERT M. RUBENSTEIN

发明人： RUBENSTEIN ALBERT M

IPC分类号： B64G1/40 ,  B64G1/44 ,  F03H1/00

CPC分类号： F03H1/00 ,  B64G1/405 ,  B64G1/44

公开(公告)号：US3412955A

公开(公告)日：1968-11-26

申请号：US58860066

申请日：1966-10-21

申请人： BOLKOW GMBH

发明人： FRIEDRICH VILBIG

IPC分类号： B64G1/10 ,  B64G1/24 ,  B64G1/28 ,  B64G1/32 ,  B64G1/36 ,  B64G1/44 ,  B64G1/64

CPC分类号： B64G1/10 ,  B64G1/24 ,  B64G1/281 ,  B64G1/32 ,  B64G1/36 ,  B64G1/443 ,  B64G1/64 ,  Y10S136/292

公开(公告)号：US3379394A

公开(公告)日：1968-04-23

申请号：US40695064

申请日：1964-10-27

申请人： NAVY USA

发明人： BIALY KAROL J

IPC分类号： B64G1/44 ,  G02B6/04 ,  H01L31/00

CPC分类号： F24J2/067 ,  B64G1/446 ,  H01L31/00 ,  Y02E10/40 ,  Y10S136/292