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公开(公告)号：US20190039738A1
公开(公告)日：2019-02-07
申请号：US15824650
申请日：2017-11-28
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Charles Lo
Abstract: A pressurization system includes a first compressor that receives a ram air, a fan air, or engine air; a first turbine that is on a common shaft with the first compressor and wherein the first turbine receives an engine air; a main heat exchanger downstream of the first compressor and the first turbine; an internal environment suitable for human occupants and downstream of the main heat exchanger; a second turbine downstream of the internal environment; the second turbine may be on the common shaft with the first compressor and first turbine; or a generator downstream of the second turbine; a motor downstream of the generator; and wherein the motor drives the first compressor.
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公开(公告)号：US09932940B2
公开(公告)日：2018-04-03
申请号：US14673066
申请日：2015-03-30
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Charles Lo
IPC: F02M31/20 , F02C7/18 , F02C7/224 , F23R3/28 , F02C7/14 , F02C7/22 , F23R3/00 , F23D11/24 , F23D11/44
CPC classification number: F02M31/20 , F02C7/14 , F02C7/185 , F02C7/222 , F02C7/224 , F05D2240/128 , F05D2250/15 , F05D2250/70 , F23D11/24 , F23D11/44 , F23D2206/10 , F23R3/005 , F23R3/28 , F23R3/283 , Y02T10/126 , Y02T50/675
Abstract: A fuel cooled cooling air heat exchanger includes a fuel injector and an airflow body. The fuel injector has a fuel flow passage formed therein that includes a fuel inlet port and a fuel outlet port. The airflow body is coupled to and surrounds at least a portion of the fuel injector. The airflow body has an inner surface that is spaced apart from the fuel injector to define an airflow passage between the airflow body and the fuel injector, and the airflow passage includes an air inlet port and an air outlet port.
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Patent Agency Ranking
公开(公告)号：US09897054B2
公开(公告)日：2018-02-20
申请号：US14597938
申请日：2015-01-15
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Charles Lo , Dan Laboda
Abstract: A fuel flow control system includes a centrifugal pump, a gas inlet valve, and a control. The centrifugal pump has a fuel inlet, a gas inlet, and an outlet. The gas inlet valve is disposed upstream of the gas inlet and is responsive to valve position commands to move between a closed position, in which inert gas is prevented from flowing into the gas inlet, and a plurality of open positions, in which inert gas may flow into the gas inlet. The control is coupled to the gas inlet valve and is configured to supply the valve position commands to the gas inlet valve to command the gas inlet valve to selectively move to the closed position, such that the centrifugal pump is configured to operate as a fuel pump, or any open position, such that the centrifugal pump is configured to operate as a fuel-gas mixer.
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公开(公告)号：US09834315B2
公开(公告)日：2017-12-05
申请号：US14570152
申请日：2014-12-15
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Charles Lo , Eric Blumer , Dan Laboda , Alexander Bershitsky
CPC classification number: B64D37/34 , B01D19/0005 , B01D19/0047 , B01D19/0057 , B01D19/0068 , B01D35/02 , B01D46/00
Abstract: An aircraft fuel deoxygenation system includes a boost pump, a contactor-separator, and a centrifuge-separator pump. The boost pump is adapted to receive fuel from a fuel source and inert gas from an inert gas source, and is configured to mix the fuel and inert gas and supply a fuel/gas mixture. The contactor-separator is coupled to receive the fuel/gas mixture and is configured to remove oxygen from the fuel and thereby generate and supply deoxygenated fuel with entrained purge gas and separated purge gas. The centrifuge-separator pump is coupled to receive the deoxygenated fuel with entrained purge gas and is configured to separate and remove the entrained purge gas from the deoxygenated fuel and supply the deoxygenated fuel and additional purge gas.
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公开(公告)号：US09656187B2
公开(公告)日：2017-05-23
申请号：US14539279
申请日：2014-11-12
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Charles Lo , Dan Laboda
IPC: B01D19/00
CPC classification number: B01D19/0057
Abstract: A fuel deoxygenation system contactor-separator includes a fuel-gas mixture inlet section, a fuel outlet section, a gas outlet, a spiral contactor-separator, and a valve element. The fuel-gas mixture inlet section has a fuel-gas mixture inlet port. The fuel outlet section has a fuel outlet port. The gas outlet section has a gas outlet port. The spiral contactor-separator conduit has an inner wall and an outer wall that defines a spiral contactor-separator flow passage. The spiral contactor-separator conduit is coupled to, and is in fluid communication with, the fuel-gas mixture inlet section, the fuel outlet section, and the gas outlet section. The valve element is disposed between the fuel outlet port and the gas outlet port and is movable between a first position and a second position.
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公开(公告)号：US09630708B2
公开(公告)日：2017-04-25
申请号：US14839065
申请日：2015-08-28
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Charles Lo , Allan Steves
CPC classification number: B64C25/405 , B60T1/10 , B60T8/1703 , B60T10/04 , B60T2270/60 , B60W30/18127 , B64C25/42 , F16D57/06 , Y02T50/823
Abstract: An aircraft landing gear wheel-drive system includes a first wheel drive unit for driving a first landing gear wheel of the aircraft and a second wheel drive unit for driving a second landing gear wheel of the aircraft. The first wheel drive unit has a first range of torque to speed (T/S) ratios. The second wheel drive unit has a second range of T/S ratios. The first range of T/S ratios is greater than the second range of T/S ratios.
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公开(公告)号：US20150314229A1
公开(公告)日：2015-11-05
申请号：US14310531
申请日：2014-06-20
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Russell W. Johnson , Peter M. Michalakos , Eric Blumer , Alexander Bershitsky , Charles Lo
IPC: B01D53/047 , B01J19/24 , B01D53/22
CPC classification number: B01D53/047 , B01D19/0005 , B01D19/0026 , B01D53/225 , B01D53/229 , B01D53/864 , B01D2053/221 , B01D2256/10 , B01D2257/104 , B01D2257/702 , B01D2258/06
Abstract: An aircraft fuel deoxygenation and tank inerting system includes an inert gas source, a fuel deoxygenation system, and an air/fuel heat exchanger. The inert gas source is configured to supply inert gas having an oxygen concentration of less than 3%. The fuel deoxygenation system is adapted to receive fuel from a fuel source and the inert gas from the inert gas source. The fuel deoxygenation system is configured to remove oxygen from the fuel and thereby generate and supply deoxygenated fuel and oxygen-rich purge gas. The air/fuel heat exchanger is adapted to receive compressed air from a compressed air source and the deoxygenated fuel from the fuel deoxygenation system. The air/fuel heat exchanger is configured to transfer heat from the compressed air to the deoxygenated fuel, to thereby supply cooled compressed air and heated deoxygenated fuel.
Abstract translation: 飞机燃料脱氧和罐惰化系统包括惰性气体源，燃料脱氧系统和空气/燃料热交换器。 惰性气体源被配置为提供氧浓度小于3％的惰性气体。 燃料脱氧系统适于从燃料源接收燃料和来自惰性气体源的惰性气体。 燃料脱氧系统被配置为从燃料中除去氧气，从而产生和供应脱氧燃料和富氧吹扫气体。 空气/燃料热交换器适于接收来自压缩空气源的压缩空气和来自燃料脱氧系统的脱氧燃料。 空气/燃料热交换器被配置为将热量从压缩空气传递到脱氧燃料，从而供应冷却的压缩空气和加热的脱氧燃料。
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