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公开(公告)号：US08967531B2
公开(公告)日：2015-03-03
申请号：US13432842
申请日：2012-03-28
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： A unique airborne electrical power and thermal management system and a unique aircraft having a unique airborne electrical power and thermal management system are provided. The electrical power and thermal management system includes a turbine, which may power loads, for example but not limited to, a generator and a refrigerant compressor. The turbine may be in fluid communication with a gas turbine engine bleed air source to extract power from bleed air for powering the loads. A combustor may be fluidly disposed between the bleed air source and the turbine. The turbine may be part of a gas turbine engine distinct from a propulsion gas turbine engine. In one aspect, at least a portion of the electrical power and thermal management system may be disposed within an aircraft external pod. The pod may be configured to appear similar to a conventional external fuel tank pod employed by the aircraft.
摘要翻译： 提供独特的机载电力和热管理系统和独特的飞机，具有独特的机载电力和热管理系统。 电力和热管理系统包括涡轮机，其可以为例如但不限于发电机和制冷剂压缩机的负载供电。 涡轮机可以与燃气涡轮发动机排气源流体连通，以从放气中提取动力以为负载供电。 燃烧器可以流体地设置在排放空气源和涡轮机之间。 涡轮机可以是不同于推进燃气涡轮发动机的燃气涡轮发动机的一部分。 在一个方面，电力和热管理系统的至少一部分可以设置在飞行器外部舱内。 荚可以被配置为看起来类似于飞机使用的常规外部燃料箱舱。
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公开(公告)号：US08814081B2
公开(公告)日：2014-08-26
申请号：US12978916
申请日：2010-12-27
申请人： Steve Gagne , John R. Arvin
发明人： Steve Gagne , John R. Arvin
IPC分类号： B64D41/00
摘要： One embodiment of the present invention is a unique aircraft. Another embodiment is a unique external pod for an aircraft. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft and external pods for aircraft. 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飞机。 另一个实施例是用于飞机的独特外部荚。 其他实施例包括用于飞行器的飞行器和外部荚的装置，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：US09534537B2
公开(公告)日：2017-01-03
申请号：US13432590
申请日：2012-03-28
CPC分类号： F02C7/141 , F01D15/08 , F01D15/10 , F02C3/04 , F02C6/08 , F02C6/20 , F02C7/12 , F02C7/16 , F02C7/32 , F05D2220/323 , F05D2220/50 , F05D2220/76 , F05D2240/35 , F05D2260/207 , F25B23/00 , F25B2400/24 , F41H13/005 , F41H13/0068 , H02K7/1823 , Y02T50/675
摘要： A system is disclosed one form of which is an aircraft that includes a pod capable of housing a work providing device. The pod can also include a thermal conditioning system and a power generation device that can be powered from the work providing device. The pod can provide thermal conditioning services and power services to a payload aboard the aircraft. In one non-limiting form the payload is a directed energy member that can be cooled using the thermal conditioning system and powered using the power generation device.
摘要翻译： 公开了一种系统，其一种形式是包括能够容纳工作提供装置的荚的飞机。 吊舱还可以包括热调节系统和可以从工作提供装置供电的发电装置。 荚可以为飞机上的有效载荷提供热调节服务和电力服务。 在一个非限制性形式中，有效载荷是能够使用热调节系统进行冷却并使用发电装置供电的定向能量构件。
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公开(公告)号：US20120248242A1
公开(公告)日：2012-10-04
申请号：US13432842
申请日：2012-03-28
IPC分类号： B64D41/00
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：US20120160957A1
公开(公告)日：2012-06-28
申请号：US12978916
申请日：2010-12-27
申请人： Steve Gagne , John R. Arvin
发明人： Steve Gagne , John R. Arvin
摘要： One embodiment of the present invention is a unique aircraft. Another embodiment is a unique external pod for an aircraft. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft and external pods for aircraft. 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飞机。 另一个实施例是用于飞机的独特外部荚。 其他实施例包括用于飞行器的飞行器和外部荚的装置，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：US20120247117A1
公开(公告)日：2012-10-04
申请号：US13432590
申请日：2012-03-28
CPC分类号： F02C7/141 , F01D15/08 , F01D15/10 , F02C3/04 , F02C6/08 , F02C6/20 , F02C7/12 , F02C7/16 , F02C7/32 , F05D2220/323 , F05D2220/50 , F05D2220/76 , F05D2240/35 , F05D2260/207 , F25B23/00 , F25B2400/24 , F41H13/005 , F41H13/0068 , H02K7/1823 , Y02T50/675
摘要： A system is disclosed one form of which is an aircraft that includes a pod capable of housing a work providing device. The pod can also include a thermal conditioning system and a power generation device that can be powered from the work providing device. The pod can provide thermal conditioning services and power services to a payload aboard the aircraft. In one non-limiting form the payload is a directed energy member that can be cooled using the thermal conditioning system and powered using the power generation device.
摘要翻译： 公开了一种系统，其一种形式是包括能够容纳工作提供装置的荚的飞机。 吊舱还可以包括热调节系统和可以从工作提供装置供电的发电装置。 荚可以为飞机上的有效载荷提供热调节服务和电力服务。 在一个非限制性形式中，有效载荷是能够使用热调节系统进行冷却并使用发电装置供电的定向能量构件。
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公开(公告)号：US3977186A
公开(公告)日：1976-08-31
申请号：US598674
申请日：1975-07-24
申请人： John R. Arvin , Albert J. Verdouw
发明人： John R. Arvin , Albert J. Verdouw
CPC分类号： F23M5/085 , F23C7/02 , F23R3/10 , Y02T50/675
摘要： A combustion liner for a gas turbine combustion apparatus or the like has a head wall and a side wall extending downstream to an outlet for combustion products. A reaction zone is contained within the upstream end of the side wall and a dilution zone downstream. A barrier ring extends inwardly from the side wall to provide a constricted path between the zones. Combustion air is admitted from a cluster of nozzles in the head wall and a ring of nozzles extending forwardly from the side wall. Each nozzle in the head wall is axially aligned with one of the nozzles in the side wall so that air jets entering into the combustion zone through each such pair of nozzles impinge to create a high degree of turbulence. Fuel is jetted against a spatter plate in each nozzle in the head wall so that the fuel is atomized and entrained by the air flowing through the head wall air nozzle.
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