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公开(公告)号:US09963792B2
公开(公告)日:2018-05-08
申请号:US14969429
申请日:2015-12-15
Applicant: Hamilton Sundstrand Corporation
Inventor: Jonathan Rheaume
CPC classification number: C25B9/10 , B01D53/326 , B64D13/06 , B64D37/32 , B64D2013/0677 , C25B1/00 , C25B1/10 , C25B9/18 , C25B13/04 , Y02E60/366 , Y02T50/56
Abstract: An inert gas generating system includes an air source configured to provide an air stream that comprises at least one of ram air, external air, conditioned air, or compressed air. An electrochemical gas separator is configured to receive the air stream and to produce an oxygen-depleted air stream. A contained volume is configured to receive the oxygen-depleted air stream.
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公开(公告)号:US20180111696A1
公开(公告)日:2018-04-26
申请号:US15299811
申请日:2016-10-21
Applicant: Hamilton Sundstrand Corporation
Inventor: Stephen E. Tongue , Jonathan Rheaume , Haralambos Cordatos
Abstract: A purge system includes an airflow source to provide an airflow, and a fuel tank, including: a tank volume including a tank ullage, at least one inlet, wherein the at least one inlet is in fluid communication with the tank ullage and the airflow source to provide the airflow as an inbound airflow to the tank ullage, and at least one outlet, wherein the at least one outlet is in fluid communication with the tank ullage and an overboard location outside the aircraft to direct the inbound airflow as an outbound airflow from the tank ullage to the overboard location.
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公开(公告)号:US20180050300A1
公开(公告)日:2018-02-22
申请号:US15238287
申请日:2016-08-16
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor: Jonathan Rheaume , Brian St. Rock , Charles E. Lents
CPC classification number: B01D53/326 , A62C3/08 , A62C99/0018 , B01D53/265 , B01D53/30 , B01D2259/4575 , B64D13/02 , B64D13/06 , B64D37/32 , C25B9/18 , F24F3/1405 , Y02T50/44 , Y02T50/54 , Y02T50/56 , Y02T90/44
Abstract: An on-board aircraft dried inert gas system includes a source inert gas containing water, an air cycle or vapor cycle cooling system, and a heat exchanger condenser. The heat exchanger condenser has a heat absorption side in thermal communication with the air cycle or vapor cycle cooling system. The heat exchanger condenser has a heat rejection side that receives the inert gas containing water and outputs dried inert gas.
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公开(公告)号:US20170331131A1
公开(公告)日:2017-11-16
申请号:US15151132
申请日:2016-05-10
Applicant: Hamilton Sundstrand Corporation
Inventor: Jonathan Rheaume
IPC: H01M8/04746 , H01M8/04082 , H01M8/1231 , H01M8/04858
CPC classification number: H01M8/04753 , A62C3/08 , A62C99/0018 , B64D37/32 , B64D2045/009 , H01M8/04201 , H01M8/04761 , H01M8/04865 , H01M8/1231 , H01M2250/20 , Y02T90/32
Abstract: An onboard electrochemical system of an electrochemical cell including a cathode and an anode separated by an electrolyte separator is selectively operated in either of two modes. In a first mode of operation, water or air is directed to the anode, electric power is provided to the anode and cathode to provide a voltage difference between the anode and the cathode, and nitrogen-enriched air is directed from the cathode to an aircraft fuel tank or aircraft fire suppression system. In a second mode of operation, fuel is directed to the anode, electric power is directed from the anode and cathode to one or more aircraft electric power-consuming systems or components, and nitrogen-enriched air is directed from the cathode to a fuel tank or fire suppression system.
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公开(公告)号:US20170267377A1
公开(公告)日:2017-09-21
申请号:US15460966
申请日:2017-03-16
Applicant: Hamilton Sundstrand Corporation
Inventor: Jonathan Rheaume , Stephen E. Tongue , Thomas P. Filburn
IPC: B64F1/22
Abstract: A taxi tug includes a chassis, a motive power source, and an auxiliary power services system. The chassis has at least one drive wheel. The motive power source is operatively connected to the at least one drive wheel. The auxiliary power services system is disposed on the chassis and is configured to provide at least one of electric power, pneumatic power, and low pressure conditioned air to an aircraft.
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公开(公告)号:US20170167037A1
公开(公告)日:2017-06-15
申请号:US14969429
申请日:2015-12-15
Applicant: Hamilton Sundstrand Corporation
Inventor: Jonathan Rheaume
CPC classification number: C25B9/10 , B01D53/326 , B64D13/06 , B64D37/32 , B64D2013/0677 , C25B1/00 , C25B1/10 , C25B9/18 , C25B13/04 , Y02E60/366 , Y02T50/56
Abstract: An inert gas generating system includes an air source configured to provide an air stream that comprises at least one of ram air, external air, conditioned air, or compressed air. An electrochemical gas separator is configured to receive the air stream and to produce an oxygen-depleted air stream. A contained volume is configured to receive the oxygen-depleted air stream.
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公开(公告)号:US11872424B2
公开(公告)日:2024-01-16
申请号:US16593834
申请日:2019-10-04
Applicant: Hamilton Sundstrand Corporation
Inventor: Jonathan Rheaume , Peter A T Cocks
CPC classification number: A62C3/08 , B01D53/326 , B01D69/08 , B01D2257/104 , B01D2313/243 , B64D2037/325 , B64D2045/009
Abstract: A system and method fare disclosed for inerting a protected space. Process water is delivered to an anode of an electrochemical cell where a portion of the process water is electrolyzed to form protons and oxygen. The protons are transferred across the separator to the cathode, and process water is directed through a process water fluid flow path including a first side of a membrane. Gas is transferred to a second side of the membrane to form a de-gassed process water on the first side of the membrane, and the de-gassed process water is recycled to the anode. Air is delivered to the cathode and oxygen is reduced at the cathode to generate oxygen-depleted air. The oxygen-depleted air is directed from the cathode of the electrochemical cell along an inerting gas flow path to the protected space.
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公开(公告)号:US11713132B2
公开(公告)日:2023-08-01
申请号:US16593681
申请日:2019-10-04
Applicant: Hamilton Sundstrand Corporation
Inventor: Jonathan Rheaume , Kimberly Saviers
CPC classification number: B64D37/32 , B01D53/326 , B01D53/8671 , B64D27/12 , B01D2257/104 , B64D13/06 , B64D2013/0618
Abstract: A system and method for inerting a fuel tank is disclosed. A fluid including non-condensable gas is directed from a vapor space in the fuel tank to a suction port of an ejector, and a motive fluid is directed to a motive fluid port of the ejector. The motive fluid and the non-condensable gas fluid are combined in the ejector and are directed from an outlet port of the ejector to the fuel tank. An inert gas is provided to the ejector motive fluid port, or to the second flow path, or to the first flow path.
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79.
公开(公告)号:US11648509B2
公开(公告)日:2023-05-16
申请号:US16593703
申请日:2019-10-04
Applicant: Hamilton Sundstrand Corporation
Inventor: Jonathan Rheaume
CPC classification number: B01D53/326 , B01D19/0063 , B64D37/32 , C25B1/04 , C25B9/73 , C25B15/02 , C25B15/08 , A62C3/08
Abstract: A system and method for inerting a protected space is disclosed. Process water is delivered to an anode of an electrochemical cell comprising the anode and a cathode separated by a separator comprising a proton transfer medium. A portion of the process water is electrolyzed at the anode to form protons and oxygen, and the protons are transferred across the separator to the cathode. Process water is directed through a process water fluid flow path including a gas outlet and a gas discharge valve in operative fluid communication with the gas outlet. Air is delivered to the cathode and oxygen is reduced at the cathode to generate oxygen-depleted air, and the oxygen-depleted air is directed from the cathode of the electrochemical cell along an inerting gas flow path to the protected space.
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公开(公告)号:US11498691B2
公开(公告)日:2022-11-15
申请号:US16374937
申请日:2019-04-04
Applicant: Hamilton Sundstrand Corporation
Inventor: Matthew Pess , Jonathan Rheaume , John S. Murphy , Peter AT Cocks
Abstract: Redundant electrochemical systems and methods for vehicles are described. The systems include a first electrochemical device located at a first position on the vehicle wherein the first electrochemical device is configured to generate at least one of inert gas, oxygen, and electrical power and a second electrochemical device located at a second position on the vehicle wherein the second electrochemical device is configured to generate at least one of inert gas, oxygen, and electrical power. The first electrochemical device is configured to operate in a first mode during normal operation of the vehicle and a second mode when the second electrochemical device fails, wherein in the second mode, the first electrochemical device provides the at least one of inert gas, oxygen, and electrical power for at least one vehicle critical system of the vehicle.
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