基本信息:
- 专利标题： SELF DEPLOYING SOLAR ARRAY
- 专利标题（中）：自我配置太阳能阵列
- 申请号：PCT/US2011/026745 申请日：2011-03-01
- 公开(公告)号：WO2011109436A1 公开(公告)日：2011-09-09
- 发明人： TAYLOR, Robert , KELLER, Philip N. , MALLICK, Kaushik , TURSE, Dana , HULSE, Michael J.
- 申请人： COMPOSITE TECHNOLOGY DEVELOPMENT, INC. , TAYLOR, Robert , KELLER, Philip N. , MALLICK, Kaushik , TURSE, Dana , HULSE, Michael J.
- 申请人地址： 2600 Campus Drive, Suite D Lafayette, Colorado 80026 US
- 专利权人： COMPOSITE TECHNOLOGY DEVELOPMENT, INC.,TAYLOR, Robert,KELLER, Philip N.,MALLICK, Kaushik,TURSE, Dana,HULSE, Michael J.
- 当前专利权人： COMPOSITE TECHNOLOGY DEVELOPMENT, INC.,TAYLOR, Robert,KELLER, Philip N.,MALLICK, Kaushik,TURSE, Dana,HULSE, Michael J.
- 当前专利权人地址： 2600 Campus Drive, Suite D Lafayette, Colorado 80026 US
- 代理机构： WEIGHT, Clark F. et al.
- 优先权： US13/036,910 20110228; US12/873,615 20100901; US61/310,205 20100303
- 主分类号： B64G1/22
- IPC分类号： B64G1/22
摘要：
A deployable structure that may include a slit-tube longeron and a flat panel coupled with the slit-tube longeron. The slit-tube longeron may include a tubular member having a slit that runs along the longitudinal length of the slit-tube longeron. The deployable structure may be configured to couple with a satellite. And the deployable structure may be configured to transform between a stowed state and a deployed state where the tubular member is substantially straight when the deployable structure is in the deployed state, and the tubular member is wrapped around the satellite when the deployable structure is in the stowed state.
摘要（中）：
可展开的结构，其可以包括狭缝管长孔和与狭缝管连接的平板。 狭缝管长龙可以包括具有沿着狭缝管长孔的纵向长度延伸的狭缝的管状构件。 可部署结构可以被配置成与卫星耦合。 并且可部署结构可以被配置为在收起状态和展开状态之间转换，其中当展开结构处于展开状态时，管状构件基本上是直的，并且当可部署结构处于展开状态时，管状构件被包裹在卫星周围 收起状态
IPC结构图谱:
| B | 作业；运输 |
| --B64 | 飞行器；航空；宇宙航行 |
| ----B64G | 宇宙航行；及其所用的飞行器或设备 |
| ------B64G1/00 | 宇宙航行的飞行器 |
| --------B64G1/22 | .宇宙航行飞行器的部件或专门适用于装入或装到宇宙航行运载工具上的设备 |