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    MULTI-PART AIR DATA PROBE ASSEMBLY TO FACILITATE RAPID REPLACEMENT
    11.
    发明申请
    MULTI-PART AIR DATA PROBE ASSEMBLY TO FACILITATE RAPID REPLACEMENT 有权

    公开(公告)号：US20170108360A1

    公开(公告)日：2017-04-20

    申请号：US14884733

    申请日：2015-10-15

    Applicant: Honeywell International Inc.

    Inventor： Yates Wong ,  Grant A. Gordon ,  Richard Bonvouloir ,  Patrick Flynn

    IPC: G01D11/30

    CPC classification number: G01D11/30 ,  G01P5/165 ,  G01P13/025

    Abstract: A multi-part air data probe sensor assembly facilitating rapid replacement is provided. In one embodiment, an air data probe sensor assembly comprises a mount plate interface including at least one mount plate electrical connector configured to mate with electrical lines of an aircraft and at least one mount plate pneumatic connector configured to mate with pneumatic tubes of an aircraft; and a detachable sensor body having at least one sensor electrical connector that is coupled with the at least one mount plate electrical connector and at least one sensor pneumatic connector that is coupled with the at least one mount plate pneumatic connector; and a mechanical seal provided between the mount plate interface and the detachable sensor body, wherein the mechanical seal is composed of a moisture blocking material.

    Liquid injection inlet particle separator systems and methods
    12.
    发明授权
    Liquid injection inlet particle separator systems and methods 有权
    液体注入口颗粒分离器系统和方法

    公开(公告)号：US09206740B2

    公开(公告)日：2015-12-08

    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 ,  F01D25/00

    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。

    Probe tip for air data probe
    14.
    发明授权
    Probe tip for air data probe 有权

    公开(公告)号：US10605637B2

    公开(公告)日：2020-03-31

    申请号：US15858633

    申请日：2017-12-29

    Applicant: Honeywell International Inc.

    Inventor： Grant A. Gordon ,  Yates Wong

    IPC: B23K31/02 ,  G01F1/46 ,  G01P5/165 ,  B23K1/00 ,  G01F15/10

    Abstract: A probe assembly includes a heat source; and a probe tip configured to enhance conduction of heat provided by the heat source into a front end tip of the probe. The probe tip includes: a first region having high thermal conductivity in at least a z-direction, wherein the z-direction is parallel to an axis along which the probe tip is extended; and at least one additional region having thermal characteristics different from the first region.

    PORTED SHROUD SYSTEM FOR TURBOPROP INLETS
    15.
    发明申请
    PORTED SHROUD SYSTEM FOR TURBOPROP INLETS 审中-公开

    公开(公告)号：US20200088097A1

    公开(公告)日：2020-03-19

    申请号：US16132954

    申请日：2018-09-17

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Bruce Dan Bouldin ,  Derek Anthony Rice ,  Michael Todd Barton ,  Raymond Mccage ,  Yates Wong ,  Kevin Sing

    IPC: F02C7/057 ,  F02C3/06 ,  B64D33/02 ,  F02C9/18

    Abstract: A system for delivering a flow stream of a gas to a compressor. A shroud extends from an inlet to the compressor and defines a main inlet passage configured to direct the flow stream from the inlet to the compressor. A communication plenum is separated from the main inlet passage. A port system includes first and second port subsystems that each provide an opening between the main inlet passage and the communication plenum. The first port subsystem is disposed further from the compressor than the second port subsystem. The port system is configured so that a portion of the gas enters or exits the compressor through the second port subsystem, depending on operating conditions of the compressor.

    PROBE TIP FOR AIR DATA PROBE
    18.
    发明申请
    PROBE TIP FOR AIR DATA PROBE 审中-公开

    公开(公告)号：US20180143049A1

    公开(公告)日：2018-05-24

    申请号：US15858633

    申请日：2017-12-29

    Applicant: Honeywell International Inc.

    Inventor： Grant A. Gordon ,  Yates Wong

    IPC: G01F1/46 ,  G01P5/165 ,  G01F15/10

    CPC classification number: G01F1/46 ,  G01F15/10 ,  G01P5/165

    Abstract: A probe assembly includes a heat source; and a probe tip configured to enhance conduction of heat provided by the heat source into a front end tip of the probe. The probe tip includes: a first region having high thermal conductivity in at least a z-direction, wherein the z-direction is parallel to an axis along which the probe tip is extended; and at least one additional region having thermal characteristics different from the first region.

    INLET PARTICLE SEPARATOR SYSTEMS AND METHODS
    20.
    发明申请
    INLET PARTICLE SEPARATOR SYSTEMS AND METHODS 审中-公开
    入射颗粒分离系统和方法

    公开(公告)号：US20160312698A1

    公开(公告)日：2016-10-27

    申请号：US15092820

    申请日：2016-04-07

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Zedic Daniel Judd ,  Yogendra Yogi Sheoran ,  Jennifer Ann Reich ,  Todd A. Kincheloe ,  Yates Wong ,  Cristopher Frost

    IPC: F02C7/052 ,  B01D45/04

    CPC classification number: F02C7/052 ,  B01D45/04 ,  B01D45/08 ,  B01D45/12 ,  B01D45/16 ,  B01D50/002 ,  F02C7/05 ,  F02C7/055 ,  F05D2260/607 ,  Y10T137/0536

    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.

    Abstract translation: 提供了一种用于车辆发动机的惯性入口颗粒分离器系统。 分离器组件和收集器组件联接到清扫流动路径并且构造成接收扫气。 收集器入口具有在从第一喉端到第二喉端的喉部长度的每个位置处限定累积喉部区域的喉部。 收集器主体限定与沿着第一喉部端部和第二喉部端部之间的喉部长度的每个位置相关联的横截面面积。 收集器出口连接到收集器主体，使得清除空气通过收集器主体流入收集器入口，并通过收集器出口流出。 在第一喉部端部和第二喉部端部之间的第一位置处，集热体的相应横截面积大于或等于相应的累积喉部面积。

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