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公开(公告)号：US20180170190A1
公开(公告)日：2018-06-21
申请号：US15898822
申请日：2018-02-19
CPC分类号： B60L11/12 , B60L50/15 , B60L2200/10 , B64D27/24 , B64D35/02 , Y02T10/646 , Y02T10/7005 , Y02T10/7077 , Y02T50/44 , Y02T50/62
摘要： The present disclosure provides an apparatus with a prime mover coupled to a generator that is directly electrically coupled to an electric motor. A propeller or fan may be coupled to and driven by the electric motor. A bi-directional power converter may be coupled to the generator and further coupled to an energy storage device. The energy storage device may be selectively coupled to the electric motor. Methods of using the apparatus are also provided.
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公开(公告)号：US09937803B2
公开(公告)日：2018-04-10
申请号：US15145869
申请日：2016-05-04
摘要： The present disclosure provides an apparatus with a prime mover coupled to a generator that is directly electrically coupled to an electric motor. A propeller or fan may be coupled to and driven by the electric motor. A bi-directional power converter may be coupled to the generator and further coupled to an energy storage device. The energy storage device may be selectively coupled to the electric motor. Methods of using the apparatus are also provided.
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公开(公告)号：US20160325629A1
公开(公告)日：2016-11-10
申请号：US15145869
申请日：2016-05-04
摘要： The present disclosure provides an apparatus with a prime mover coupled to a generator that is directly electrically coupled to an electric motor. A propeller or fan may be coupled to and driven by the electric motor. A bi-directional power converter may be coupled to the generator and further coupled to an energy storage device. The energy storage device may be selectively coupled to the electric motor. Methods of using the apparatus are also provided.
摘要翻译： 本公开提供了一种具有耦合到直接电耦合到电动机的发电机的原动机的装置。 螺旋桨或风扇可以联接到电动机并由电动机驱动。 双向功率转换器可以耦合到发电机并进一步耦合到能量存储装置。 能量存储装置可以选择性地联接到电动机。 还提供了使用该装置的方法。
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公开(公告)号：US20160176529A1
公开(公告)日：2016-06-23
申请号：US15058924
申请日：2016-03-02
CPC分类号： B64D13/006 , B64D13/08 , B64D33/04 , B64D33/08 , B64D41/00 , B64D41/007 , B64D2013/0614 , B64D2013/0674 , F02C6/08 , F02C7/32 , H02K7/1823
摘要： One embodiment of the present disclosure is a unique airborne electrical power and thermal management system. Another embodiment is a unique aircraft. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft and electrical power and thermal management systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
摘要翻译： 本公开的一个实施例是独特的机载电力和热管理系统。 另一个实施例是独特的飞机。 其他实施例包括用于飞机和电力和热管理系统的装置，系统，装置，硬件，方法和组合。 本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。
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公开(公告)号：US09771157B2
公开(公告)日：2017-09-26
申请号：US15058924
申请日：2016-03-02
IPC分类号： B64D13/00 , B64D13/08 , F02C7/32 , B64D33/04 , B64D33/08 , B64D41/00 , H02K7/18 , F02C6/08 , B64D13/06
CPC分类号： B64D13/006 , B64D13/08 , B64D33/04 , B64D33/08 , B64D41/00 , B64D41/007 , B64D2013/0614 , B64D2013/0674 , F02C6/08 , F02C7/32 , H02K7/1823
摘要： One embodiment of the present disclosure is a unique airborne electrical power and thermal management system. Another embodiment is a unique aircraft. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft and electrical power and thermal management systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
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公开(公告)号：US10427527B2
公开(公告)日：2019-10-01
申请号：US15898822
申请日：2018-02-19
摘要： The present disclosure provides an apparatus with a prime mover coupled to a generator that is directly electrically coupled to an electric motor. A propeller or fan may be coupled to and driven by the electric motor. A bi-directional power converter may be coupled to the generator and further coupled to an energy storage device. The energy storage device may be selectively coupled to the electric motor. Methods of using the apparatus are also provided.
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7.发明申请PROPULSION, ELECTRICAL, AND THERMAL MANAGEMENT DEVICE FOR A SMALL UNMANNED AERIAL VEHICLE 审中-公开用于小型无人驾驶车辆的推进，电气和热管理装置公开(公告)号：US20150001339A1
公开(公告)日：2015-01-01
申请号：US14133155
申请日：2013-12-18
CPC分类号： B64D41/00 , B64C39/024 , B64C2201/042 , B64C2201/048 , B64C2201/165 , B64D13/06 , B64D27/02 , B64D27/10 , B64D27/24 , B64D35/00 , B64D2013/0674 , B64D2027/026 , F02C7/32 , F25B27/00 , F25B2327/00 , Y02T50/44 , Y02T50/62
摘要： An aircraft is provided with a gas turbine engine having a plurality of shafts. A first shaft provides power to an electrical generator and a propeller, while a second shaft provides power to a refrigeration system. The refrigeration system may be integrated to the propeller, like a ducted fan, or on the outer skin of the aircraft.
摘要翻译： 飞机设置有具有多个轴的燃气涡轮发动机。 第一轴为发电机和螺旋桨提供动力，而第二轴为制冷系统提供动力。 制冷系统可以集成到螺旋桨，如风扇，或飞机外皮上。
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8.发明授权公开(公告)号：US09731836B2
公开(公告)日：2017-08-15
申请号：US14133155
申请日：2013-12-18
IPC分类号： B64D41/00 , B64D35/00 , B64C39/02 , B64D13/06 , B64D27/02 , F02C7/32 , B64D27/10 , B64D27/24 , F25B27/00
CPC分类号： B64D41/00 , B64C39/024 , B64C2201/042 , B64C2201/048 , B64C2201/165 , B64D13/06 , B64D27/02 , B64D27/10 , B64D27/24 , B64D35/00 , B64D2013/0674 , B64D2027/026 , F02C7/32 , F25B27/00 , F25B2327/00 , Y02T50/44 , Y02T50/62
摘要： An aircraft is provided with a gas turbine engine having a plurality of shafts. A first shaft provides power to an electrical generator and a propeller, while a second shaft provides power to a refrigeration system. The refrigeration system may be integrated to the propeller, like a ducted fan, or on the outer skin of the aircraft.
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9.发明申请公开(公告)号：US20150151848A1
公开(公告)日：2015-06-04
申请号：US14609548
申请日：2015-01-30
CPC分类号： B64D13/006 , B64D13/08 , B64D33/04 , B64D33/08 , B64D41/00 , B64D41/007 , B64D2013/0614 , B64D2013/0674 , F02C6/08 , F02C7/32 , H02K7/1823
摘要： One embodiment of the present invention is a unique airborne electrical power and thermal management system. Another embodiment is a unique aircraft. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft and electrical power and thermal management systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
摘要翻译： 本发明的一个实施例是独特的机载电力和热管理系统。 另一个实施例是独特的飞机。 其他实施例包括用于飞机和电力和热管理系统的装置，系统，装置，硬件，方法和组合。 本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。
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公开(公告)号：US20140356135A1
公开(公告)日：2014-12-04
申请号：US14461721
申请日：2014-08-18
IPC分类号： F02C6/04
CPC分类号： F02C6/04 , F01D15/10 , F02C7/266 , F05D2220/36 , F05D2220/76 , F05D2270/304 , H02K3/28 , H02K7/1823 , H02K21/028 , H02K2213/09
摘要： An electric machine is disclosed integrated to rotate with a shaft of a gas turbine engine. In one form the electric machine is integrated with a fan of the gas turbine engine. A rotor of the electric machine can be disposed at the end of the fan blades and the stator integrated into a flow path forming surface of the gas turbine engine. In one form the windings of the electric machine can change configuration permitting some windings to be placed in parallel with one or more other windings, and then connected together in series with remaining windings, if any. The voltage of the electric machine can change as a result of a change in configuration of the windings. A moveable member can also be used to alter a magnetic field produced from the electric machine when operated such that a voltage can be changed as a result of altering the magnetic field.
摘要翻译： 公开了一种集成为与燃气涡轮发动机的轴一起旋转的电机。 在一种形式中，电机与燃气涡轮发动机的风扇集成。 电机的转子可以设置在风扇叶片的端部，并且定子整合在燃气轮机的流路形成面上。 在一种形式中，电机的绕组可以改变配置，允许一些绕组与一个或多个其他绕组平行放置，然后与剩余绕组（如果有的话）串联连接在一起。 由于绕组的配置变化，电机的电压可能会改变。 还可以使用可移动部件来改变由电机产生的磁场，以使得可以通过改变磁场来改变电压。
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