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公开(公告)号：US09181934B2
公开(公告)日：2015-11-10
申请号：US13683688
申请日：2012-11-21
申请人： The Boeing Company
发明人： John F. Stickelmaier , John Ziavras , Julie Marie Perkins , Kurt B. Kreiner , Glenn N. Caplin , Brian K. Smith , Peter S. Lauenstein
CPC分类号： F03H1/0043 , B64G1/405 , B64G1/42 , B64G1/428 , F03H1/0018 , H01H19/50 , H01H19/64
摘要： A gridded ion propulsion system comprising two power controllers, four ion thrusters, and two switch assemblies. One switch assembly is connected to the two power controllers and to two of the four ion thrusters. The other switch assembly is connected to the two power controllers and to the other two ion thrusters. Each switch assembly has first and second switching states which can be selected to enable either power controller to supply power to any one of the four ion thrusters. Each switch assembly comprises a respective movable body and a respective multiplicity of switches which change state in unison when the movable body changes position. For example, the movable body may be a rotatable hollow shaft driven by a stepper motor.
摘要翻译： 包括两个功率控制器，四个离子推进器和两个开关组件的网格离子推进系统。 一个开关组件连接到两个功率控制器和四个离子推进器中的两个。 另一个开关组件连接到两个电源控制器和另外两个离子推进器。 每个开关组件具有第一和第二开关状态，其可以被选择以使得功率控制器能够向四个离子推进器中的任何一个供电。 每个开关组件包括相应的可移动体和相应的多个开关，其在可移动体改变位置时一致地改变状态。 例如，可动体可以是由步进电动机驱动的可旋转中空轴。
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公开(公告)号：US09834324B2
公开(公告)日：2017-12-05
申请号：US14533934
申请日：2014-11-05
申请人： The Boeing Company
CPC分类号： B64G1/007 , B64G1/405 , B64G1/428 , F03H1/0018
摘要： Described herein is a thrust system for a vehicle that includes at least three electrical power controllers, at least four electrical switches each configured to receive electrical power from at least one of the at least three electrical power controllers, and at least three thrusters each configured to receive electrical power from at least one of the at least three electrical switches. The at least four electrical switches are operable to switch a supply of electrical power from any of the at least three electrical power controllers to any one of the at least three thrusters.
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公开(公告)号：US09469420B2
公开(公告)日：2016-10-18
申请号：US14258954
申请日：2014-04-22
申请人： The Boeing Company
发明人： John F. Stickelmaier , Dean A. Chin
CPC分类号： B64G1/405 , F03H1/0018 , H01H1/40 , H01H19/10 , H01H19/50 , H01H19/54 , H01H19/56 , H01H19/64 , H01H2009/0088
摘要： Described herein is a shaft assembly for a rotary switch that includes a shaft made from an electrically non-conductive material. The shaft includes at least one circumferential groove that has a generally T-shaped cross-section. The shaft assembly also includes at least one conductive ring segment made from an electrically conductive material positioned within the circumferential groove. The conductive ring segment has a generally T-shaped cross-section. Additionally, the shaft assembly includes a bonding adhesive that is positioned between the circumferential groove and the conductive ring segment.
摘要翻译： 这里描述的是用于旋转开关的轴组件，其包括由非导电材料制成的轴。 轴包括至少一个具有大致T形横截面的圆周凹槽。 轴组件还包括由定位在周向槽内的导电材料制成的至少一个导电环段。 导电环段具有大致T形的横截面。 此外，轴组件包括定位在周向槽和导电环段之间的粘结粘合剂。
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公开(公告)号：US20180057189A1
公开(公告)日：2018-03-01
申请号：US15803417
申请日：2017-11-03
申请人： The Boeing Company
摘要： Described herein is a thrust system for a vehicle that includes at least three electrical power controllers, at least four electrical switches each configured to receive electrical power from at least one of the at least three electrical power controllers, and at least three thrusters each configured to receive electrical power from at least one of the at least three electrical switches. The at least four electrical switches are operable to switch a supply of electrical power from any of the at least three electrical power controllers to any one of the at least three thrusters.
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公开(公告)号：US09038364B2
公开(公告)日：2015-05-26
申请号：US13655138
申请日：2012-10-18
申请人： The Boeing Company
CPC分类号： F03H1/0043 , B64G1/405
摘要： Thruster grid clear circuits and methods to clear thruster grids are disclosed. An example apparatus includes a low voltage grid clear circuit to apply first energy to a grid at a first voltage, and a high voltage grid clear circuit to detect a failure of the applied energy to clear a short circuit condition of the grid and to apply second energy to the grid at a second voltage higher than the first voltage.
摘要翻译： 公开了推进器网格清除电路和清除推进器网格的方法。 示例性装置包括：用于在第一电压下将第一能量施加到电网的低压电网清除电路;以及高电压电网清除电路，用于检测所施加的能量的故障以清除电网的短路状况并施加第二电压 在比第一电压高的第二电压下向电网施加能量。
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公开(公告)号：US20140137537A1
公开(公告)日：2014-05-22
申请号：US13683688
申请日：2012-11-21
申请人： THE BOEING COMPANY
发明人： John F. Stickelmaier , John Ziavras , Julie Marie Perkins , Kurt B. Kreiner , Glenn N. Caplin , Brian K. Smith , Peter S. Lauenstein
IPC分类号： F03H1/00
CPC分类号： F03H1/0043 , B64G1/405 , B64G1/42 , B64G1/428 , F03H1/0018 , H01H19/50 , H01H19/64
摘要： A gridded ion propulsion system comprising two power controllers, four ion thrusters, and two switch assemblies. One switch assembly is connected to the two power controllers and to two of the four ion thrusters. The other switch assembly is connected to the two power controllers and to the other two ion thrusters. Each switch assembly has first and second switching states which can be selected to enable either power controller to supply power to any one of the four ion thrusters. Each switch assembly comprises a respective movable body and a respective multiplicity of switches which change state in unison when the movable body changes position. For example, the movable body may be a rotatable hollow shaft driven by a stepper motor.
摘要翻译： 包括两个功率控制器，四个离子推进器和两个开关组件的网格离子推进系统。 一个开关组件连接到两个功率控制器和四个离子推进器中的两个。 另一个开关组件连接到两个电源控制器和另外两个离子推进器。 每个开关组件具有第一和第二开关状态，其可以被选择以使得功率控制器能够向四个离子推进器中的任何一个供电。 每个开关组件包括相应的可移动体和相应的多个开关，其在可移动体改变位置时一致地改变状态。 例如，可动体可以是由步进电动机驱动的可旋转中空轴。
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7.发明申请THRUSTER GRID CLEAR CIRCUITS AND METHODS TO CLEAR THRUSTER GRIDS 有权THRUSTER GRID CLEAR CIRCUITS和清除THRUSTER GRIDS的方法公开(公告)号：US20150226189A1
公开(公告)日：2015-08-13
申请号：US14693482
申请日：2015-04-22
申请人： The Boeing Company
IPC分类号： F03H1/00
CPC分类号： F03H1/0043 , B64G1/405
摘要： Thruster grid clear circuits and methods to clear thruster grids are disclosed. An example apparatus includes a low voltage grid clear circuit to apply first energy to a grid at a first voltage, and a high voltage grid clear circuit to detect a failure of the applied energy to clear a short circuit condition of the grid and to apply second energy to the grid at a second voltage higher than the first voltage.
摘要翻译： 公开了推进器网格清除电路和清除推进器网格的方法。 示例性装置包括：用于在第一电压下将第一能量施加到电网的低压电网清除电路;以及高电压电网清除电路，用于检测所施加的能量的故障以清除电网的短路状况并施加第二电压 在比第一电压高的第二电压下向电网施加能量。
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公开(公告)号：US09086060B1
公开(公告)日：2015-07-21
申请号：US13664635
申请日：2012-10-31
申请人： The Boeing Company
CPC分类号： F03H1/0018 , B64G1/405 , B64G1/428 , G01R31/3278 , H01R29/00
摘要： A relay telemetry system enables an ion propulsion system to self-test the critical relay configuration prior to supplying high-voltage power to any thruster. This test detects whether any critical relay has failed to switch properly or is in the wrong configuration. In the test mode, an onboard computer initiates the application of a low-voltage test voltage (nominally 15 V) to the high-voltage circuits (when the high voltage is off) by a stimulus circuit. Sensing circuits detect the inputs and outputs of the system connections in response to this stimulus. If the test voltage appears on an input or output where it is not expected, then a relay fault has occurred and will be detectable in telemetry sent back to the onboard computer.
摘要翻译： 继电器遥测系统使得离子推进系统能够在向任何推进器供应高压电力之前对关键继电器配置进行自检。 此测试检测任何关键继电器是否正确切换或配置错误。 在测试模式下，机载计算机通过激励电路向高电压电路（当高电压关闭时）启动低电压测试电压（标称值为15 V）的应用。 感测电路响应于该刺激来检测系统连接的输入和输出。 如果测试电压出现在不期望的输入或输出上，则发生继电器故障，并且可以在发回到机载计算机的遥测中检测到。
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公开(公告)号：US10829247B2
公开(公告)日：2020-11-10
申请号：US15803417
申请日：2017-11-03
申请人： The Boeing Company
摘要： Described herein is a thrust system for a vehicle that includes at least three electrical power controllers, at least four electrical switches each configured to receive electrical power from at least one of the at least three electrical power controllers, and at least three thrusters each configured to receive electrical power from at least one of the at least three electrical switches. The at least four electrical switches are operable to switch a supply of electrical power from any of the at least three electrical power controllers to any one of the at least three thrusters.
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公开(公告)号：US09989041B2
公开(公告)日：2018-06-05
申请号：US14693482
申请日：2015-04-22
申请人： The Boeing Company
CPC分类号： F03H1/0043 , B64G1/405
摘要： Thruster grid clear circuits and methods to clear thruster grids are disclosed. An example apparatus includes a low voltage grid clear circuit to apply first energy to a grid at a first voltage, and a high voltage grid clear circuit to detect a failure of the applied energy to clear a short circuit condition of the grid and to apply second energy to the grid at a second voltage higher than the first voltage.
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