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1. 发明授权

US07950606B2 Electric-based secondary power system architectures for aircraft 有权
标题翻译：用于飞机的电力二次电力系统架构
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。

2. 发明申请

US20070284480A1 ELECTRIC-BASED SECONDARY POWER SYSTEM ARCHITECTURES FOR AIRCRAFT 有权
标题翻译：电动二次电机系统架构
公开(公告)号：US20070284480A1
公开(公告)日：2007-12-13
申请号：US11693532
申请日：2007-03-29
申请人： Warren Atkey , Alan Bernier , Michael Bowman , Thomas Campbell , Jonathan Cruse , Charles Fiterman , Charles Meis , Casey Ng , Farhad Nozari , Edward Zielinski
发明人： Warren Atkey , Alan Bernier , Michael Bowman , Thomas Campbell , Jonathan Cruse , Charles Fiterman , Charles Meis , Casey Ng , Farhad Nozari , Edward Zielinski
IPC分类号： B64D41/00 , B64D15/12
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。

3. 发明申请

US20060102790A1 Electric-based secondary power system architectures for aircraft 有权
标题翻译：用于飞机的电力二次电力系统架构
公开(公告)号：US20060102790A1
公开(公告)日：2006-05-18
申请号：US11301179
申请日：2005-12-12
申请人： Warren Atkey , Alan Bernier , Michael Bowman , Thomas Campbell , Jonathan Cruse , Charles Fiterman , Charles Meis , Casey Ng , Farhad Nozari , Edward Zielinski
发明人： Warren Atkey , Alan Bernier , Michael Bowman , Thomas Campbell , Jonathan Cruse , Charles Fiterman , Charles Meis , Casey Ng , Farhad Nozari , Edward Zielinski
IPC分类号： B64D15/16
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。

4. 发明申请

US20070267540A1 ELECTRIC-BASED SECONDARY POWER SYSTEM ARCHITECTURES FOR AIRCRAFT 审中-公开
公开(公告)号：US20070267540A1
公开(公告)日：2007-11-22
申请号：US11693046
申请日：2007-03-29
申请人： Warren Atkey , Alan Bernier , Michael Bowman , Thomas Campbell , Jonathan Cruse , Charles Fiterman , Charles Meis , Casey Ng , Farhad Nozari , Edward Zielinski
发明人： Warren Atkey , Alan Bernier , Michael Bowman , Thomas Campbell , Jonathan Cruse , Charles Fiterman , Charles 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.

5. 发明申请

US20210185429A1 PRESSURE EQUALIZING EARPHONE 有权
公开(公告)号：US20210185429A1
公开(公告)日：2021-06-17
申请号：US17125603
申请日：2020-12-17
申请人： Robert Smith , Casey Ng
发明人： Robert Smith , Casey Ng
IPC分类号： H04R1/10
摘要： An earphone has a body housing a transducer that is capable of generating an acoustic signal and directing the acoustic signal to an outlet in the body, the body being positionable in, on, or near an ear of user so that the acoustic signal can be directed into the ear canal of the user. The earphone also has an ear coupling mechanism comprising a sealing mechanism with a sealing member that is adapted to contact a portion of the ear of the user to at least partially create a seal between the ear canal and the external environment and a venting mechanism capable of venting air between the ear canal and the external environment, the venting mechanism comprising an air conduit that is adapted to communicate on one end with the ear canal and at another end with the external environment so that air can flow through the conduit to equalize a pressure differential across the sealing mechanism. The air conduit is sized and shaped so as to provide an improved audio performance over an earphone without the air conduit.

6. 发明授权

US11405717B2 Pressure equalizing earphone 有权
公开(公告)号：US11405717B2
公开(公告)日：2022-08-02
申请号：US17125603
申请日：2020-12-17
申请人： Robert Smith , Casey Ng
发明人： Robert Smith , Casey Ng
IPC分类号： H04R1/10
摘要： An earphone has a body housing a transducer that is capable of generating an acoustic signal and directing the acoustic signal to an outlet in the body, the body being positionable in, on, or near an ear of user so that the acoustic signal can be directed into the ear canal of the user. The earphone also has an ear coupling mechanism comprising a sealing mechanism with a sealing member that is adapted to contact a portion of the ear of the user to at least partially create a seal between the ear canal and the external environment and a venting mechanism capable of venting air between the ear canal and the external environment, the venting mechanism comprising an air conduit that is adapted to communicate on one end with the ear canal and at another end with the external environment so that air can flow through the conduit to equalize a pressure differential across the sealing mechanism. The air conduit is sized and shaped so as to provide an improved audio performance over an earphone without the air conduit.

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