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公开(公告)号：US20170160024A1
公开(公告)日：2017-06-08
申请号：US14959717
申请日：2015-12-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Patrick Trizila , Yogendra Yogi Sheoran , Frank Lin
CPC classification number: F16K47/08 , F24F11/84 , F28F9/026 , F28F27/02 , F28F2220/00
Abstract: A flow control system in an inlet duct to a heat exchanger includes a door having a first end and a second end opposite the first end. The first end rotates about an axis and the second end moves between an open position and a closed position to respectively allow and prevent flow into the heat exchanger. The second end has a rounded configuration. A plurality of mixing elements are downstream of the door. At least one mixing element has a base portion and a distal portion, and the base portion has a base width and the distal portion has a distal width. The base width is wider that the distal width.
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公开(公告)号：US09145214B2
公开(公告)日：2015-09-29
申请号：US14063324
申请日：2013-10-25
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Murali Krishnan Payangapadan , Vunnam Kiran , Lavan Kumar Gundeti , Yogendra Yogi Sheoran , Bruce Dan Bouldin
CPC classification number: B64D33/02 , B64C1/0009 , B64D41/00 , B64D2033/0213 , Y10T137/0536
Abstract: An inlet door system includes a duct, an inlet door, and a plurality of openings. The duct is configured to extend from the auxiliary power unit (APU) to an intake opening formed in an outer surface of an aircraft. The duct includes an inlet port, an outlet port, and a duct sidewall extending between the inlet port and the outlet port. The inlet door includes an inner surface, an outer surface, and an outer peripheral edge between the inner and outer surfaces. The door is rotationally coupled to the duct, and is configured to selectively rotate between a closed position and a plurality of open positions. The openings extend through the inlet door between the inner surface and outer surface, and each opening is disposed adjacent to the outer peripheral edge.
Abstract translation: 入口门系统包括管道，入口门和多个开口。 管道构造成从辅助动力单元（APU）延伸到形成在飞行器的外表面中的进气口。 管道包括入口，出口和在入口和出口之间延伸的管道侧壁。 入口门包括内表面，外表面和内表面和外表面之间的外周边缘。 门旋转地联接到管道，并且构造成选择性地在关闭位置和多个打开位置之间旋转。 开口在内表面和外表面之间延伸穿过入口门，并且每个开口邻近外围边缘设置。
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公开(公告)号：US20150115099A1
公开(公告)日：2015-04-30
申请号：US14063324
申请日：2013-10-25
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Murali Krishnan Payangapadan , Vunnam Kiran , Lavan Kumar Gundeti , Yogendra Yogi Sheoran , Bruce Dan Bouldin
CPC classification number: B64D33/02 , B64C1/0009 , B64D41/00 , B64D2033/0213 , Y10T137/0536
Abstract: An inlet door system includes a duct, an inlet door, and a plurality of openings. The duct is configured to extend from the auxiliary power unit (APU) to an intake opening formed in an outer surface of an aircraft. The duct includes an inlet port, an outlet port, and a duct sidewall extending between the inlet port and the outlet port. The inlet door includes an inner surface, an outer surface, and an outer peripheral edge between the inner and outer surfaces. The door is rotationally coupled to the duct, and is configured to selectively rotate between a closed position and a plurality of open positions. The openings extend through the inlet door between the inner surface and outer surface, and each opening is disposed adjacent to the outer peripheral edge.
Abstract translation: 入口门系统包括管道，入口门和多个开口。 管道构造成从辅助动力单元（APU）延伸到形成在飞行器的外表面中的进气口。 管道包括入口，出口和在入口和出口之间延伸的管道侧壁。 入口门包括内表面，外表面和内表面和外表面之间的外周边缘。 门旋转地联接到管道，并且构造成选择性地在关闭位置和多个打开位置之间旋转。 开口在内表面和外表面之间延伸穿过入口门，并且每个开口邻近外围边缘设置。
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公开(公告)号：US20150040535A1
公开(公告)日：2015-02-12
申请号：US13961284
申请日：2013-08-07
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Zedic Daniel Judd , Yogendra Yogi Sheoran , Devinder N. Katariya , Eduardo Guerra
IPC: F02C7/05
CPC classification number: F02C7/05 , B64D2033/0246 , F02C7/052 , F05D2260/607 , Y02T50/675
Abstract: An inlet particle separator system for a vehicle engine includes a hub section, a shroud section, a splitter, and a hub suction flow passage. The shroud section surrounds at least a portion of the hub section and is spaced apart therefrom to define a main flow passageway that has an air inlet. The splitter is disposed downstream of the air inlet and extends into the passageway to divide the main flow passageway into a scavenge flow path and an engine flow path. The hub suction flow passage has a hub suction inlet port and a hub suction outlet port. The hub suction inlet port extends through the hub section and is in fluid communication with the air inlet. The hub suction outlet port extends through the splitter and is in fluid communication with the scavenge flow path.
Abstract translation: 用于车辆发动机的入口颗粒分离器系统包括轮毂部分，护罩部分，分离器和轮毂吸入流动通道。 护罩部分围绕轮毂部分的至少一部分并与其间隔开以限定具有空气入口的主流动通道。 分流器设置在空气入口的下游并延伸到通道中，以将主流动通道分成扫气流动路径和发动机流动路径。 轮毂吸入流路具有轮毂吸入口和轮毂吸出口。 轮毂吸入口延伸穿过轮毂部分并与进气口流体连通。 轮毂吸出口延伸穿过分流器并与清流流路流体连通。
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公开(公告)号：US20140190347A1
公开(公告)日：2014-07-10
申请号：US13734875
申请日：2013-01-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Yates Wong , Eric Blumer , Eduardo Guerra , Yogendra Yogi Sheoran , Zedic Daniel Judd
IPC: F02C7/052
CPC classification number: F02C7/052 , F01D25/002 , F05D2260/607 , Y02T50/671 , Y02T50/675
Abstract: An inlet particle separator system for a vehicle engine includes a separator assembly and a liquid injection system. The separator assembly defines an inlet flow path for receiving inlet air and includes a scavenge flow path and an engine flow path downstream of the inlet flow path. The separator assembly is configured to separate the inlet air into scavenge air and engine air such that the scavenge air is directed from the inlet flow path into the scavenge flow path and the engine air is directed from the inlet flow path into the engine flow path. The liquid injection system is coupled to the separator assembly and configured to introduce a diffused liquid into the inlet air flowing through the separator assembly.
Abstract translation: 用于车辆发动机的入口颗粒分离器系统包括分离器组件和液体喷射系统。 分离器组件限定用于接收入口空气的入口流动路径，并且包括清除流动路径和在入口流动路径下游的发动机流动路径。 分离器组件构造成将入口空气分离成清空空气和发动机空气，使得清扫空气从入口流动路径引导到清除流动路径中，并且发动机空气从入口流动路径引导到发动机流动路径中。 液体注射系统联接到分离器组件并且构造成将扩散的液体引入流过分离器组件的入口空气中。
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Patent Agency Ranking
公开(公告)号：US11261788B2
公开(公告)日：2022-03-01
申请号：US16355392
申请日：2019-03-15
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Tirumala Rao Koka , Shailesh Kumar , Karthik Narayanasamy , Yogendra Yogi Sheoran
Abstract: An inlet particle separator system for a gas turbine engine includes a separator manifold. The separator manifold includes an inlet upstream from an outlet. The inlet is to receive an incoming airflow, and the outlet is to be fluidly coupled to an inlet of the gas turbine engine. The inlet particle separator system includes at least one dry fog nozzle coupled proximate the inlet so as to face at least partially away from the inlet. The dry fog nozzle is external to the separator manifold, and the dry fog nozzle is to direct a spray of dry fog in a direction transverse to the incoming airflow to agglomerate with fine particles in the incoming airflow to form agglomerated particles. The inlet particle separator system includes a scavenging system coupled to the separator manifold downstream from the inlet, and the scavenging system removes the agglomerated particles from the separator manifold.
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公开(公告)号：US11255239B2
公开(公告)日：2022-02-22
申请号：US16215914
申请日：2018-12-11
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Yoonshik Shin , Yogendra Yogi Sheoran , Daniel Brown
Abstract: A gas turbine engine includes a combustion section that generates combustive gases that form a primary exhaust flow and an exhaust system downstream from the combustion section. The exhaust system includes an eductor system that includes a body that extends along a first axis, and a plurality of ducts spaced apart about a circumference of the body. Each of the plurality of ducts define a plurality of eductor primary flow paths that terminate in a mixing chamber. The exhaust system includes a muffler system downstream from the mixing chamber that includes a plurality of baffles that cooperate to define a tortuous path and attenuate sound generated by the gas turbine engine. The exhaust system includes a housing that surrounds the eductor system and the muffler system such that the eductor system and the muffler system are contained within the housing.
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公开(公告)号：US20200291855A1
公开(公告)日：2020-09-17
申请号：US16355392
申请日：2019-03-15
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Tirumala Rao Koka , Shailesh Kumar , Karthik Narayanasamy , Yogendra Yogi Sheoran
Abstract: An inlet particle separator system for a gas turbine engine includes a separator manifold. The separator manifold includes an inlet upstream from an outlet. The inlet is to receive an incoming airflow, and the outlet is to be fluidly coupled to an inlet of the gas turbine engine. The inlet particle separator system includes at least one dry fog nozzle coupled proximate the inlet so as to face at least partially away from the inlet. The dry fog nozzle is external to the separator manifold, and the dry fog nozzle is to direct a spray of dry fog in a direction transverse to the incoming airflow to agglomerate with fine particles in the incoming airflow to form agglomerated particles. The inlet particle separator system includes a scavenging system coupled to the separator manifold downstream from the inlet, and the scavenging system removes the agglomerated particles from the separator manifold.
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公开(公告)号：US10760487B2
公开(公告)日：2020-09-01
申请号：US16058627
申请日：2018-08-08
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Zedic Daniel Judd , Yogendra Yogi Sheoran , Jennifer Ann Reich , Todd A. Kincheloe , Yates Wong , Cristopher Frost
Abstract: An inertial inlet particle separator system for a vehicle engine is provided. A separator assembly and collector assembly are coupled to the scavenge flow path and configured to receive the scavenge air. The collector inlet has a throat defining a cumulative throat area at each position along the throat length from the first throat end to the second throat end. The collector body defines a cross-sectional area associated with each position along the throat length between the first throat end and the second throat end. The collector outlet is coupled to the collector body such that scavenge air flows into the collector inlet, through the collector body, and out through the collector outlet. At a first position between the first throat end and the second throat end, the respective cross-sectional area of the collector body is greater than or equal to the respective cumulative throat area.
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公开(公告)号：US10359242B2
公开(公告)日：2019-07-23
申请号：US14959717
申请日：2015-12-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Patrick Trizila , Yogendra Yogi Sheoran , Frank Lin
Abstract: A flow control system in an inlet duct to a heat exchanger includes a door having a first end and a second end opposite the first end. The first end rotates about an axis and the second end moves between an open position and a closed position to respectively allow and prevent flow into the heat exchanger. The second end has a rounded configuration. A plurality of mixing elements are downstream of the door. At least one mixing element has a base portion and a distal portion, and the base portion has a base width and the distal portion has a distal width. The base width is wider that the distal width.
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