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公开(公告)号：US07950606B2
公开(公告)日：2011-05-31
申请号：US11693532
申请日：2007-03-29
申请人： Warren A. Atkey , Alan T. Bernier , Michael D. Bowman , Thomas A. Campbell , Jonathan M. Cruse , Charles J. Fiterman , Charles S. Meis , Casey Ng , Farhad Nozari , Edward Zielinski
发明人： Warren A. Atkey , Alan T. Bernier , Michael D. Bowman , Thomas A. Campbell , Jonathan M. Cruse , Charles J. Fiterman , Charles S. Meis , Casey Ng , Farhad Nozari , Edward Zielinski
IPC分类号： B64D41/00
CPC分类号： B64D13/08 , B64D13/06 , B64D41/00 , B64D2013/0611 , B64D2013/064 , B64D2013/0644 , B64D2041/005 , B64D2221/00 , Y02T50/44 , Y02T50/53 , Y02T50/56 , Y02T90/36
摘要： Methods and systems for providing secondary power to aircraft systems. In one embodiment, an aircraft system architecture for providing power to an environmental control system includes an electric generator operably coupled to a jet engine. The jet engine can be configured to provide propulsive thrust to the aircraft, and the electric generator can be configured to receive shaft power from the jet engine. The environmental control system can be configured to provide outside air to a passenger cabin of the aircraft in the absence of bleed air from the jet engine.
摘要翻译： 为飞机系统提供次级电源的方法和系统。 在一个实施例中，用于向环境控制系统提供动力的飞机系统架构包括可操作地联接到喷气发动机的发电机。 喷气发动机可以被配置成向飞行器提供推进推力，并且发电机可被配置成从喷气发动机接收轴功率。 环境控制系统可以被配置为在没有来自喷气发动机的排放空气的情况下向飞行器的客舱提供外部空气。
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公开(公告)号：US07207521B2
公开(公告)日：2007-04-24
申请号：US11301179
申请日：2005-12-12
申请人： Warren A. Atkey , Alan T. Bernier , Michael D. Bowman , Thomas A. Campbell , Jonathan M. Cruse , Charles J. Fiterman , Charles S. Meis , Casey Y. K. Ng , Farhad Nozari , Edward Zielinski
发明人： Warren A. Atkey , Alan T. Bernier , Michael D. Bowman , Thomas A. Campbell , Jonathan M. Cruse , Charles J. Fiterman , Charles S. Meis , Casey Y. K. Ng , Farhad Nozari , Edward Zielinski
IPC分类号： B64D41/00
CPC分类号： B64D13/08 , B64D13/06 , B64D41/00 , B64D2013/0611 , B64D2013/064 , B64D2013/0644 , B64D2041/005 , B64D2221/00 , Y02T50/44 , Y02T50/53 , Y02T50/56 , Y02T90/36
摘要： Methods and systems for providing secondary power to aircraft systems. In one embodiment, an aircraft system architecture for providing power to an environmental control system includes an electric generator operably coupled to a jet engine. The jet engine can be configured to provide propulsive thrust to the aircraft, and the electric generator can be configured to receive shaft power from the jet engine. The environmental control system can be configured to provide outside air to a passenger cabin of the aircraft in the absence of bleed air from the jet engine.
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公开(公告)号：US07210653B2
公开(公告)日：2007-05-01
申请号：US10691440
申请日：2003-10-21
申请人： Warren A. Atkey , Alan T. Bernier , Michael D. Bowman , Thomas A. Campbell , Jonathan M. Cruse , Charles J. Fiterman , Charles S. Meis , Casey Y. K. Ng , Farhad Nozari , Edward Zielinski
发明人： Warren A. Atkey , Alan T. Bernier , Michael D. Bowman , Thomas A. Campbell , Jonathan M. Cruse , Charles J. Fiterman , Charles S. Meis , Casey Y. K. Ng , Farhad Nozari , Edward Zielinski
IPC分类号： B64D41/00
CPC分类号： B64D13/08 , B64D13/06 , B64D41/00 , B64D2013/0611 , B64D2013/064 , B64D2013/0644 , B64D2041/005 , B64D2221/00 , Y02T50/44 , Y02T50/53 , Y02T50/56 , Y02T90/36
摘要： Methods and systems for providing secondary power to aircraft systems. In one embodiment, an aircraft system architecture for providing power to an environmental control system includes an electric generator operably coupled to a jet engine. The jet engine can be configured to provide propulsive thrust to the aircraft, and the electric generator can be configured to receive shaft power from the jet engine. The environmental control system can be configured to provide outside air to a passenger cabin of the aircraft in the absence of bleed air from the jet engine.
摘要翻译： 为飞机系统提供次级电源的方法和系统。 在一个实施例中，用于向环境控制系统提供动力的飞机系统架构包括可操作地联接到喷气发动机的发电机。 喷气发动机可以被配置成向飞行器提供推进推力，并且发电机可被配置成从喷气发动机接收轴功率。 环境控制系统可以被配置为在没有来自喷气发动机的排放空气的情况下向飞行器的客舱提供外部空气。
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公开(公告)号：US09914543B2
公开(公告)日：2018-03-13
申请号：US14964365
申请日：2015-12-09
CPC分类号： B64D15/22 , B64D15/166 , B64D15/20
摘要： A method includes receiving a plurality of temperature measurements from temperature sensors of an aircraft. The method includes determining whether a first count of one or more first temperature metrics that are within a temperature range is greater than a first threshold. The one or more temperature metrics are derived from the plurality of temperature measurements. The method includes initiating generating an icing output signal when the first count is greater than or equal to the first threshold.
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公开(公告)号：US20170166314A1
公开(公告)日：2017-06-15
申请号：US14964365
申请日：2015-12-09
CPC分类号： B64D15/22 , B64D15/166 , B64D15/20
摘要： A method includes receiving a plurality of temperature measurements from temperature sensors of an aircraft. The method includes determining whether a first count of one or more first temperature metrics that are within a temperature range is greater than a first threshold. The one or more temperature metrics are derived from the plurality of temperature measurements. The method includes initiating generating an icing output signal when the first count is greater than or equal to the first threshold.
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