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公开(公告)号：US20170101190A1
公开(公告)日：2017-04-13
申请号：US14878650
申请日：2015-10-08
Applicant: Honeywell International Inc.
Inventor： Morris Anderson , Grant A. Gordon , Yates Wong , Richard Bonvouloir
Abstract: An air data probe comprises an elongated body structure having a proximal end and a distal end, with the elongated body structure including an outer surface and an opposing inner surface that defines an interior channel. A probe tip is located at the distal end of the elongated body structure, with the probe tip including an outer surface and an inner surface that are contiguous with the outer an inner surfaces of the elongated body structure. The probe tip has an opening in communication with the interior channel that allows outside air to pass from the probe tip into the interior channel. An electrical heater cable is coupled to the elongated body structure and the probe tip. The electrical heater cable comprises a compact double layer helix portion coupled to the elongated body structure or the probe tip, or coupled to both the elongated body structure and the probe tip.
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公开(公告)号：US20170074167A1
公开(公告)日：2017-03-16
申请号：US14850300
申请日：2015-09-10
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Shawn Alstad , Robert Romano , Morris Anderson , Robert Hoover
IPC: F02C7/18
CPC classification number: F02C7/185 , F02C6/08 , F02C7/18 , F02K3/115 , Y02T50/675
Abstract: A precooler system having a symmetrical precooler core that is optimized to be integrally mounted to the turbofan engine, regardless of the turbofan engine size, is provided. The provided precooler system optimizes available space between a turbofan engine and the nacelle, and does not substantially increase weight and cost. The provided precooler system may be flexibly implemented as either a right handed precooler system or a left handed precooler system.
Abstract translation: 提供了具有对称预冷器芯的预冷器系统，其被优化成整体地安装到涡轮风扇发动机，而不管涡轮风扇发动机的尺寸。 所提供的预冷器系统优化涡轮风扇发动机和机舱之间的可用空间，并且基本上不增加重量和成本。 所提供的预冷器系统可以灵活地实现为右手预冷器系统或左手预冷器系统。
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公开(公告)号：US11105691B2
公开(公告)日：2021-08-31
申请号：US15941520
申请日：2018-03-30
Applicant: Honeywell International Inc.
Inventor： Grant Gordon , Nicholas A. Everson , Morris Anderson , Merle L Sand
Abstract: A total air temperature (TAT) probe having a self-regulating heating system is provided. A TAT probe housing includes at least one heating cavity that is located proximate to a tip of the TAT probe. A heating element is received within the at least one heating cavity. The heating element is composed from a flexible material with a very high positive temperature coefficient (PTC) that provides non-linear resistance with temperature with generally relatively low electrical resistances at temperatures below freezing and relatively high electrical resistances above freezing. A power source is coupled to the heating element. The very high PTC material of the heating element causes less power to be drawn by the heating element from the power source at higher temperatures above freezing than the power drawn by the heating element from the power source at lower temperatures below freezing to maintain a desired temperature of the TAT probe.
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公开(公告)号：US11002222B2
公开(公告)日：2021-05-11
申请号：US15927578
申请日：2018-03-21
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Justin C. Mickelsen , Morris Anderson
Abstract: A thrust reverser system for a gas turbine engine includes at least one hinge coupled to the thrust reverser system so as to be adjacent to at least one opening defined in the thrust reverser system. The thrust reverser system includes at least one body coupled to the at least one hinge. The at least one body has a first body end and an opposing second body end. The body pivotally coupled to the hinge such that a portion of the body is positionable within the at least one opening and the body includes at least one counterweight at the first body end or the second body end. The body is positioned within the at least one opening based on an operating condition of the gas turbine engine.
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公开(公告)号：US10648426B2
公开(公告)日：2020-05-12
申请号：US14995396
申请日：2016-01-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Danis Burton Smith , Mark Knowles , Shawn Alstad , Robert Romano , John Taylor Pearson , Morris Anderson , David Robinson
Abstract: A thrust reverser system comprising a single row vane assembly is provided. The provided thrust reverser system is capable of meeting performance requirements for turbine engines with reduced weight and cost.
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Patent Agency Ranking
公开(公告)号：US20190301949A1
公开(公告)日：2019-10-03
申请号：US15941520
申请日：2018-03-30
Applicant: Honeywell International Inc.
Inventor： Grant Gordon , Nicholas A. Everson , Morris Anderson , Merle L Sand
Abstract: A total air temperature (TAT) probe having a self-regulating heating system is provided. A TAT probe housing includes at least one heating cavity that is located proximate to a tip of the TAT probe. A heating element is received within the at least one heating cavity. The heating element is composed from a flexible material with a very high positive temperature coefficient (PTC) that provides non-linear resistance with temperature with generally relatively low electrical resistances at temperatures below freezing and relatively high electrical resistances above freezing. A power source is coupled to the heating element. The very high PTC material of the heating element causes less power to be drawn by the heating element from the power source at higher temperatures above freezing than the power drawn by the heating element from the power source at lower temperatures below freezing to maintain a desired temperature of the TAT probe.
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公开(公告)号：US20170259926A1
公开(公告)日：2017-09-14
申请号：US15064748
申请日：2016-03-09
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Morris Anderson , Shawn Alstad
IPC: B64D15/04
CPC classification number: B64D15/04 , B64D2033/0233 , F02C6/06 , F02C7/047
Abstract: An anti-icing system is provided for an inlet lip annularly extending about a nacelle of an aircraft engine assembly. The anti-icing system includes an interior wall structure at least partially forming an annular anti-icing chamber with the inlet lip and an annular shield with a first end coupled to the interior wall structure and a second end extending into the annular anti-icing chamber. The annular shield divides the annular anti-icing chamber into first and second chamber portions fluidly coupled together by a passage formed between the second end and the internal surface of the inlet lip. The anti-icing system further includes a nozzle at an inwardly radial position relative to the first end of the annular shield such that the heated air exits the nozzle into the first chamber portion in which the annular shield blocks direct impingement on the internal surface of the inlet lip.
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公开(公告)号：US09664542B2
公开(公告)日：2017-05-30
申请号：US14830943
申请日：2015-08-20
Applicant: Honeywell International Inc.
Inventor： Grant A. Gordon , Yates Wong , Richard Bonvouloir , Patrick Flynn , Morris Anderson , Allen Brown
CPC classification number: G01F1/46 , B05D3/007 , B05D2202/00 , B05D2350/30 , B05D2451/00 , G01P5/165
Abstract: Systems and methods for additive manufacturing for air data probes are provided. In at least one embodiment a probe comprises a support structure comprising one or more ports for receiving one or more fluids, the support structure comprising an endoskeleton mandrel having an opening for receiving a fluid; and a heating cable encircling an external surface of the endoskeleton mandrel. The probe also comprises an additive coating fused to the external surface of the endoskeleton mandrel and an external surface of the heating cable; and an internal assembly inside the support structure for carrying pressures from the one or more ports to one or more instruments that respond to the one or more fluids to provide a measurement.
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公开(公告)号：US20170052046A1
公开(公告)日：2017-02-23
申请号：US14830943
申请日：2015-08-20
Applicant: Honeywell International Inc.
Inventor： Grant A. Gordon , Yates Wong , Richard Bonvouloir , Patrick Flynn , Morris Anderson , Allen Brown
CPC classification number: G01F1/46 , B05D3/007 , B05D2202/00 , B05D2350/30 , B05D2451/00 , G01P5/165
Abstract: Systems and methods for additive manufacturing for air data probes are provided. In at least one embodiment a probe comprises a support structure comprising one or more ports for receiving one or more fluids, the support structure comprising an endoskeleton mandrel having an opening for receiving a fluid; and a heating cable encircling an external surface of the endoskeleton mandrel. The probe also comprises an additive coating fused to the external surface of the endoskeleton mandrel and an external surface of the heating cable; and an internal assembly inside the support structure for carrying pressures from the one or more ports to one or more instruments that respond to the one or more fluids to provide a measurement.
Abstract translation: 提供了用于空气数据探头的添加剂制造的系统和方法。 在至少一个实施例中，探针包括支撑结构，该支撑结构包括用于接收一种或多种流体的一个或多个端口，所述支撑结构包括具有用于接收流体的开口的内骨架心轴; 以及围绕内骨架心轴的外表面的加热电缆。 探针还包括熔合到内骨架心轴的外表面和加热电缆的外表面的添加剂涂层; 以及在所述支撑结构内部的内部组件，用于承载来自所述一个或多个端口的压力到响应所述一种或多种流体以提供测量的一个或多个仪器。
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公开(公告)号：US11649056B2
公开(公告)日：2023-05-16
申请号：US16904295
申请日：2020-06-17
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Morris Anderson , Peter Anthony
IPC: G01K7/00 , B64D15/04 , G01K13/02 , G01L19/00 , G01K13/024
CPC classification number: B64D15/04 , G01K7/00 , G01K13/02 , G01L19/0092 , G01K13/024
Abstract: A thermally isolated sensor associated with a gas turbine engine includes a sensor probe configured to measure a temperature of a fluid associated with the gas turbine engine, and a base to be coupled to the gas turbine engine. The thermally isolated sensor includes a leading projection coupled to the base that extends into the fluid. The leading projection is configured to be heated by a heat source associated with the gas turbine engine. The thermally isolated sensor includes a trailing projection coupled to the base that extends into the fluid. The trailing projection is downstream from the leading projection. The trailing projection includes an inlet, and the sensor probe is disposed within the inlet and thermally isolated from the leading projection.
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