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1. 发明授权

US06634596B2 Aircraft system architecture 有权
标题翻译：飞机系统架构
公开(公告)号：US06634596B2
公开(公告)日：2003-10-21
申请号：US10077277
申请日：2002-02-14
申请人： Jose Albero , Louis J. Bruno , Richard Dussault , Charles E. Lents , Wayne A. Thresher , Michael K. Sahm , Robert G. Thompson
发明人： Jose Albero , Louis J. Bruno , Richard Dussault , Charles E. Lents , Wayne A. Thresher , Michael K. Sahm , Robert G. Thompson
IPC分类号： F02K312
CPC分类号： B64D15/04 , B64D13/06 , B64D27/16 , B64D41/00 , B64D2013/0611 , B64D2013/064 , B64D2013/0644 , F02C7/32 , F05D2220/50 , Y02T50/44 , Y02T50/56 , Y02T50/671
摘要： An integrated aircraft system which comprises an aircraft frame, a nacelle cowl mounted to the aircraft frame, a primary gas turbine engine mounted within the nacelle cowl, a secondary power system incorporated within the nacelle cowl and being driven by a flow of air created by or through the engine, and an electrical power and cooling unit for supplying electrical power and cabin cooling air. The electrical power and cooling unit is pneumatically driven by engine bleed air.
摘要翻译：一种集成的飞行器系统，包括飞机机架，安装在飞行器机架上的机舱罩，安装在机舱罩内的主要燃气涡轮发动机，并入机舱罩内的二次电力系统，并被由通过发动机，以及用于提供电力和客舱冷却空气的电力和冷却单元。电力和冷却单元由发动机排放气体气动驱动。

2. 发明授权

US06845630B2 Electric power and cooling system for an aircraft 有权
标题翻译：飞机电力和冷却系统
公开(公告)号：US06845630B2
公开(公告)日：2005-01-25
申请号：US10077281
申请日：2002-02-14
申请人： Louis J. Bruno , Charles E. Lents , Michael K. Sahm , Wayne A. Thresher
发明人： Louis J. Bruno , Charles E. Lents , Michael K. Sahm , Wayne A. Thresher
IPC分类号： B64D13/06 , F25D9/00 , B64D13/02
CPC分类号： B64D13/06 , B64D2013/064 , B64D2013/0644 , Y02T50/56
摘要： The present invention relates to an electrical power and cooling system for use in an aircraft having at least one engine. The electrical power and cooling system comprises a single shaft, a power turbine mounted on the shaft for receiving fresh pressurized air from the at least one engine, a cooling turbine mounted on the shaft and receiving the fresh pressurized air from the at least one engine, a generator mounted on the shaft, and a fan mounted on the shaft for creating a flow of cooling air. The system further has a condenser for removing moisture from the air exiting the cooling turbine and a mixing chamber for mixing the cooled dry air with recirculated cabin air. The electrical power and cooling system delivers conditioned air to a cabin and/or a flight deck onboard the aircraft and electrical power to the aircraft's electrical systems.
摘要翻译：本发明涉及一种用于具有至少一个发动机的飞行器中的电力和冷却系统。电力和冷却系统包括单个轴，安装在轴上的动力涡轮机，用于接收来自至少一个发动机的新鲜加压空气;安装在轴上的冷却涡轮机，以及接收来自至少一个发动机的新鲜加压空气，安装在轴上的发电机和安装在轴上的风扇，用于产生冷却空气流。该系统还具有用于从离开冷却涡轮机的空气中除去水分的冷凝器和用于将冷却的干燥空气与再循环的机舱空气混合的混合室。电力和冷却系统向飞机上的舱室和/或飞行甲板提供调节空气，并向飞机的电气系统提供电力。

3. 发明授权

US06928832B2 Electrically driven aircraft cabin ventilation and environmental control system 有权
标题翻译：电动飞机机舱通风和环境控制系统
公开(公告)号：US06928832B2
公开(公告)日：2005-08-16
申请号：US10672651
申请日：2003-09-26
申请人： Charles E. Lents , Steven E. Squier , Wayne A. Thresher
发明人： Charles E. Lents , Steven E. Squier , Wayne A. Thresher
IPC分类号： B64D13/06 , F25B9/00 , F25D25/00 , F25D9/00
CPC分类号： B64D13/06 , B64D2013/0644 , F25B9/004 , Y02T50/56
摘要： The present invention relates to an electrically driven aircraft cabin and ventilation and environmental control system. The system includes at least one inlet for capturing ram air, an electrically driven compressor for pressurizing the ram air, and a thermal conditioning subsystem for thermally conditioning the pressurized ram air. The system further includes a subsystem for removing undesirable moisture from the thermally conditioned ram air.
摘要翻译：本发明涉及电动飞机机舱和通风和环境控制系统。该系统包括用于捕获冲压空气的至少一个入口，用于对冲压空气加压的电动压缩机和用于对加压的冲压空气进行热调节的热调节子系统。该系统还包括用于从热调节的冲压空气中除去不需要的水分的子系统。

4. 发明授权

US06681592B1 Electrically driven aircraft cabin ventilation and environmental control system 有权
标题翻译：电动飞机机舱通风和环境控制系统
公开(公告)号：US06681592B1
公开(公告)日：2004-01-27
申请号：US10076687
申请日：2002-02-14
申请人： Charles E. Lents , Steven E. Squier , Wayne A. Thresher
发明人： Charles E. Lents , Steven E. Squier , Wayne A. Thresher
IPC分类号： F25B900
CPC分类号： B64D13/06 , B64D2013/0644 , F25B9/004 , Y02T50/56
摘要： The present invention relates to an electrically driven aircraft cabin and ventilation and environmental control system. The system includes at least one inlet for capturing ram air, an electrically driven compressor for pressurizing the ram air, and a thermal conditioning subsystem for thermally conditioning the pressurized ram air. The system further includes a subsystem for removing undesirable moisture from the thermally conditioned ram air.
摘要翻译：本发明涉及电动飞机机舱和通风和环境控制系统。该系统包括用于捕获冲压空气的至少一个入口，用于对冲压空气加压的电动压缩机和用于对加压的冲压空气进行热调节的热调节子系统。该系统还包括用于从热调节的冲压空气中除去不需要的水分的子系统。

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