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1. 发明申请

US20100243817A1 SPACECRAFT HEAT DISSIPATION SYSTEM 有权
标题翻译：空调散热系统
公开(公告)号：US20100243817A1
公开(公告)日：2010-09-30
申请号：US12730457
申请日：2010-03-24
申请人： Douglas V. McKinnon , Timothy P. Moran
发明人： Douglas V. McKinnon , Timothy P. Moran
IPC分类号： B64G1/58
CPC分类号： B64G1/50 , B64G1/503 , B64G1/506 , F28D15/0275
摘要： A spacecraft is provided. The spacecraft comprises a plurality of heat generating electrical components. A first thermal radiator panel and a second thermal radiator panel are provided on the spacecraft, each panel being thermally coupled to the heat generating electrical components. Heat pipes are also provided. At least one first heat pipe is externally attached to the first thermal radiator panel and at least one second heat pipe is externally attached to the second thermal radiator panel. The at least one first heat pipe is thermally coupled to the at least one second heat pipe.
摘要翻译：提供了一种航天器。航天器包括多个发热电气部件。第一散热器面板和第二散热器面板设置在航天器上，每个面板热耦合到发热电气组件。还提供热管。至少一个第一热管外部附接到第一散热器板，并且至少一个第二热管外部附接到第二散热器板。所述至少一个第一热管热耦合到所述至少一个第二热管。

2. 发明授权

US07513462B1 Satellite equipment mounting panel 有权
标题翻译：卫星设备安装面板
公开(公告)号：US07513462B1
公开(公告)日：2009-04-07
申请号：US11147354
申请日：2005-06-08
申请人： Douglas V. McKinnon , David J. Hentosh
发明人： Douglas V. McKinnon , David J. Hentosh
IPC分类号： B64G1/44
CPC分类号： B64G1/1007 , B64G1/402 , B64G1/44 , B64G1/503 , B64G1/506 , B64G1/66
摘要： A satellite payload structure includes one side that includes at least two equipment mounting panels. Each of the equipment mounting panels are oriented substantially parallel to each other such that when the satellite is deployed, each of the equipment mounting panels are substantially parallel to a vector pointing from the deployed location of the satellite to a point on the earth's surface. The point on the earth's surface is located vertically beneath the satellite such that the vector is substantially normal to the earth's surface.
摘要翻译：卫星有效载荷结构包括包括至少两个设备安装面板的一侧。每个设备安装面板基本上彼此平行地定向，使得当卫星被部署时，每个设备安装面板基本上平行于从卫星的展开位置指向地球表面上的点的矢量。地球表面上的点位于卫星的垂直方向，使得矢量基本上垂直于地球表面。

3. 发明授权

US07874520B2 Satellite with deployable, articulatable thermal radiators 有权
标题翻译：卫星具有可部署，可铰接的散热器
公开(公告)号：US07874520B2
公开(公告)日：2011-01-25
申请号：US11385586
申请日：2006-03-21
申请人： Douglas V. McKinnon , David M. Brown , David J. Hentosh
发明人： Douglas V. McKinnon , David M. Brown , David J. Hentosh
IPC分类号： B64G1/50 , B64G1/52
CPC分类号： B64G1/222 , B64G1/503
摘要： A satellite (50) is disclosed having at least one deployable thermal radiator (64). Once deployed, this thermal radiator (64) may be repositioned. In one embodiment, the deployed thermal radiator (64) may be moved about a first axis (74), about a second axis (76), or both to move the deployed thermal radiator (64) from one deployed position to another deployed position.
摘要翻译：公开了一种具有至少一个可展开散热器（64）的卫星（50）。一旦部署，该热散热器（64）可以重新定位。在一个实施例中，部署的热辐射器（64）可围绕第一轴线（74）绕第二轴线（76）或两者移动，以将部署的散热器（64）从一个展开位置移动到另一展开位置。

4. 发明授权

US06825807B1 Preventing interference due to misaligned ground terminals 失效
标题翻译：防止由于接地端子不对准引起的干扰
公开(公告)号：US06825807B1
公开(公告)日：2004-11-30
申请号：US10374316
申请日：2003-02-25
申请人： Douglas V. McKinnon
发明人： Douglas V. McKinnon
IPC分类号： H01Q300
CPC分类号： H01Q1/1257 , H04B7/18517 , H04B7/19
摘要： Embodiments of the present invention are directed to a method and an apparatus for preventing interference of geosynchronous satellites due to ground stations with misaligned antennas. In one embodiment, a two-way satellite ground terminal is configured to communicate with a geosynchronous target satellite which transmits a target satellite signal. The ground terminal comprises an antenna which is configured to receive the target satellite signal from the geosynchronous target satellite only if the antenna is oriented toward the geosynchronous target satellite. A transmitter is configured to transmit signals from the ground terminal via the antenna A signal detector is operatively coupled with the antenna and with the transmitter. The signal detector is configured to enable the transmitter to transmit signals from the ground terminal to the target satellite via the antenna only upon detecting the target satellite signal received by the antenna from the geosynchronous target satellite at a signal level above a preset threshold level.
摘要翻译：本发明的实施例涉及一种用于防止由于具有未对准天线的地面站引起的地球同步卫星的干扰的方法和装置。在一个实施例中，双向卫星接地终端被配置为与发射目标卫星信号的地球同步目标卫星通信。接地端子包括天线，其被配置为仅当天线朝向地球同步目标卫星时才从地球同步目标卫星接收目标卫星信号。发射器被配置为经由天线从接地端子传输信号。信号检测器可操作地与天线和发射器耦合。所述信号检测器被配置成使得所述发射机仅在所述天线从所述地球同步目标卫星在高于预设阈值水平的信号电平上检测到的目标卫星信号时，经由所述天线将信号从所述接地终端发射到所述目标卫星。

5. 发明授权

US08820684B2 Spacecraft heat dissipation system 有权
标题翻译：航天器散热系统
公开(公告)号：US08820684B2
公开(公告)日：2014-09-02
申请号：US12730457
申请日：2010-03-24
申请人： Douglas V. McKinnon , Timothy P. Moran
发明人： Douglas V. McKinnon , Timothy P. Moran
IPC分类号： B64G1/52 , B64G1/50
CPC分类号： B64G1/50 , B64G1/503 , B64G1/506 , F28D15/0275
摘要： A spacecraft is provided. The spacecraft comprises a plurality of heat generating electrical components. A first thermal radiator panel and a second thermal radiator panel are provided on the spacecraft, each panel being thermally coupled to the heat generating electrical components. Heat pipes are also provided. At least one first heat pipe is externally attached to the first thermal radiator panel and at least one second heat pipe is externally attached to the second thermal radiator panel. The at least one first heat pipe is thermally coupled to the at least one second heat pipe.
摘要翻译：提供了一种航天器。航天器包括多个发热电气部件。第一散热器面板和第二散热器面板设置在航天器上，每个面板热耦合到发热电气组件。还提供热管。至少一个第一热管外部附接到第一散热器板，并且至少一个第二热管外部附接到第二散热器板。所述至少一个第一热管热耦合到所述至少一个第二热管。

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