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    ICING CONDITION DETECTION METHOD
    1.
    发明申请
    ICING CONDITION DETECTION METHOD 审中-公开
    ICING条件检测方法

    公开(公告)号：US20160257414A1

    公开(公告)日：2016-09-08

    申请号：US15155079

    申请日：2016-05-16

    Applicant: The Boeing Company

    Inventor： Mark Joseph Clemen, JR. ,  Jerry Lee Wert ,  George Albert Perry ,  Scott Hutchinson Gardner ,  Erik Marc Langhofer ,  Charles Steven Meis

    IPC: B64D15/22 ,  B64D15/12

    CPC classification number: B64D15/22 ,  B64D15/12 ,  B64D15/20

    Abstract: A method for detecting an icing condition using an apparatus comprising a piezoelectric material and a vibration detector. The piezoelectric material has a surface proximate to a surface of a vehicle. The piezoelectric material is configured to vibrate. The vibration detector is configured to detect a change in vibrations in the piezoelectric material that indicates a presence of an icing condition on the surface of the piezoelectric material.

    Abstract translation: 一种使用包括压电材料和振动检测器的装置检测结冰条件的方法。 压电材料具有靠近车辆表面的表面。 压电材料构造成振动。 振动检测器被配置为检测表示在压电材料的表面上存在结冰条件的压电材料的振动的变化。

    Mitigating Shock Using Plasma
    2.
    发明申请
    Mitigating Shock Using Plasma 有权

    公开(公告)号：US20170129592A1

    公开(公告)日：2017-05-11

    申请号：US14936953

    申请日：2015-11-10

    Applicant: The Boeing Company

    Inventor： Mark Joseph Clemen, JR. ,  Donald V. Drouin, JR. ,  Alan F. Stewart

    IPC: B64C21/00 ,  B64C23/00

    CPC classification number: B64C21/00 ,  B64C23/00 ,  B64C23/005 ,  B64C30/00 ,  B64C2230/12

    Abstract: A method, apparatus, and system for mitigating undesired effects of a vehicle traveling at a speed greater than a critical Mach number for the vehicle. Ultraviolet energy is generated using a plurality of ultraviolet energy sources associated with an interior structure of the vehicle that travels at the speed greater than the critical Mach number for the vehicle. The ultraviolet energy is transported from the plurality of ultraviolet energy sources past an exterior of the vehicle around a selected location of the vehicle. A plasma is created around the selected location to mitigate the undesired effects of the vehicle traveling at the speed greater than the critical Mach number for the vehicle.

    APPARATUS AND METHOD FOR GENERATING A HIGH POWER ENERGY BEAM BASED LASER
    4.
    发明申请
    APPARATUS AND METHOD FOR GENERATING A HIGH POWER ENERGY BEAM BASED LASER 审中-公开

    公开(公告)号：US20190115713A1

    公开(公告)日：2019-04-18

    申请号：US15785022

    申请日：2017-10-16

    Applicant: THE BOEING COMPANY

    Inventor： Mark Joseph Clemen, JR. ,  John R. Hull

    IPC: H01S3/032 ,  H01S3/102 ,  H01S3/0975 ,  H01S3/07

    CPC classification number: H01S3/0326 ,  H01S3/07 ,  H01S3/0959 ,  H01S3/0975 ,  H01S3/10092 ,  H01S3/102

    Abstract: A system for generating an energy beam based laser includes an apparatus for receiving an energy beam and for generating an energy beam based laser. The apparatus is configurable or controllable for tuning an output wavelength of the laser generated by the apparatus using the energy beam. The apparatus includes a first component for producing a first magnetic field oriented in a first direction and a second component for producing a second magnetic field oriented in a second direction substantially opposite to the first direction. A channel through the apparatus is defined by the first component and the second component through which the energy beam passes to generate the laser at an output of the apparatus. The apparatus is configurable or controllable for modifying at least one of the first magnetic field and the second magnetic field for tuning the output wavelength of the laser.

    APPARATUS AND METHOD FOR GENERATING A HIGH POWER ENERGY BEAM BASED LASER
    6.
    发明申请
    APPARATUS AND METHOD FOR GENERATING A HIGH POWER ENERGY BEAM BASED LASER 审中-公开

    公开(公告)号：US20200280160A1

    公开(公告)日：2020-09-03

    申请号：US16874367

    申请日：2020-05-14

    Applicant: The Boeing Company

    Inventor： Mark Joseph Clemen, JR. ,  John R. Hull

    IPC: H01S3/032 ,  H01S3/07 ,  H01S3/0975 ,  H01S3/102 ,  H01S3/0959

    Abstract: A system for generating an energy beam based laser includes an apparatus for receiving an energy beam and for generating an energy beam based laser. The apparatus is configurable or controllable for tuning an output wavelength of the laser generated by the apparatus using the energy beam. The apparatus includes a first component for producing a first magnetic field oriented in a first direction and a second component for producing a second magnetic field oriented in a second direction substantially opposite to the first direction. A channel through the apparatus is defined by the first component and the second component through which the energy beam passes to generate the laser at an output of the apparatus. The apparatus is configurable or controllable for modifying at least one of the first magnetic field and the second magnetic field for tuning the output wavelength of the laser.

    THERMAL INSULATION FOR AIRCRAFT COMPONENTS
    7.
    发明申请
    THERMAL INSULATION FOR AIRCRAFT COMPONENTS 审中-公开

    公开(公告)号：US20170240266A1

    公开(公告)日：2017-08-24

    申请号：US15590693

    申请日：2017-05-09

    Applicant: The Boeing Company

    Inventor： Mark Joseph Clemen, JR. ,  Jerry Lee Wert

    IPC: B64C1/40 ,  B64C30/00

    CPC classification number: B64C1/40 ,  B64C1/38 ,  B64C30/00 ,  H01F7/0236

    Abstract: A thermal insulation system for an aircraft is provided. The thermal insulation system includes a carrier and a container. The carrier has an interior surface including a first plurality of magnets that generate a first magnetic field, and an exterior surface that is thermally coupled to at least one high temperature component. The container is surrounded by the interior surface of the carrier, has an exterior surface including a second plurality of magnets that generate a second magnetic field oriented opposite the first magnetic field, and has an interior surface that is thermally coupled to at least one temperature sensitive component. The first magnetic field and the second magnetic field generate a gap between the carrier and the container to reduce a heat transfer from the at least one high temperature component to the at least one temperature sensitive component during operation of the aircraft.

    THERMAL INSULATION SYSTEM, AIRCRAFT, AND VEHICLE HAVING SAME
    8.
    发明申请
    THERMAL INSULATION SYSTEM, AIRCRAFT, AND VEHICLE HAVING SAME 有权

    公开(公告)号：US20170101170A1

    公开(公告)日：2017-04-13

    申请号：US14881337

    申请日：2015-10-13

    Applicant: The Boeing Company

    Inventor： Mark Joseph Clemen, JR. ,  Jerry Lee Wert

    IPC: B64C1/38 ,  H01F7/02 ,  H01F7/06 ,  B64C30/00 ,  F41H3/00

    CPC classification number: B64C1/38 ,  B64C30/00 ,  F41H3/00 ,  H01F7/0236 ,  H01F7/0273 ,  H01F7/064 ,  H02N15/00

    Abstract: A thermal insulation system for an aircraft that includes leading surfaces is provided. The thermal insulation system includes a carrier and a container. The carrier has an interior surface that includes a first plurality of magnets that generate a first magnetic field, and an exterior surface that is thermally coupled to the leading surfaces of the aircraft. The container is surrounded by the interior surface of the carrier, has an exterior surface including a second plurality of magnets that generate a second magnetic field oriented opposite the first magnetic field, and has an interior that includes electronics. The first magnetic field and the second magnetic field generate a gap between the carrier and the container to reduce a heat transfer from the leading surfaces to the electronics during operation of the aircraft.

    SYSTEMS AND METHODS FOR DETECTING LIGHT
    9.
    发明申请
    SYSTEMS AND METHODS FOR DETECTING LIGHT 有权
    用于检测光的系统和方法

    公开(公告)号：US20160266228A1

    公开(公告)日：2016-09-15

    申请号：US14643386

    申请日：2015-03-10

    Applicant: THE BOEING COMPANY

    Inventor： Mark Joseph Clemen, JR.

    IPC: G01S3/782 ,  G01J1/42

    CPC classification number: G01S3/782 ,  G01J1/0266 ,  G01J1/0414 ,  G01J1/06 ,  G01J1/4228 ,  G01J1/4257 ,  G01J2001/061 ,  G01S3/784 ,  G02B5/003 ,  G02B26/0816

    Abstract: A light detection system may include a light detecting assembly including a plurality of light detectors. Each light detector may include a substrate, a mirror coupled to the substrate, and a light-receiving tube coupled to the substrate. The light-receiving tube may include a sensor positioned at a first end, a light-transmissive opening at a second end that is opposite from the first end, and a plurality of partitions that are configured to block transmission of light energy. A central light path extends through the light-receiving tube. The system may also include a control unit in communication with the light detecting assembly. The control unit is configured to determine one or more of a direction of light emitted from a light source, a position of the light source, or an intensity of light emitted from the light source based on one or more light detection signals received from the light detecting assembly.

    Abstract translation: 光检测系统可以包括包括多个光检测器的光检测组件。 每个光检测器可以包括衬底，耦合到衬底的反射镜和耦合到衬底的光接收管。 光接收管可以包括位于第一端处的传感器，在与第一端相对的第二端处的透光开口，以及被配置为阻挡光能的传输的多个隔板。 中央光路延伸穿过光接收管。 该系统还可以包括与光检测组件通信的控制单元。 控制单元被配置为基于从光接收到的一个或多个光检测信号来确定从光源发射的光的方向，光源的位置或从光源发射的光的强度中的一个或多个 检测组件。

    RADIATION INDUCED ERROR DETECTION IN SOLID-STATE DEVICES
    10.
    发明公开
    RADIATION INDUCED ERROR DETECTION IN SOLID-STATE DEVICES 审中-公开

    公开(公告)号：US20240362112A1

    公开(公告)日：2024-10-31

    申请号：US18307743

    申请日：2023-04-26

    Applicant: The Boeing Company

    Inventor： Mark Joseph Clemen, JR. ,  Ethan Cannon ,  Manuel F. Cabanas-Holmen

    IPC: G06F11/10 ,  G11C29/12 ,  G11C29/42

    CPC classification number: G06F11/1068 ,  G06F11/106 ,  G11C29/12005 ,  G11C29/42

    Abstract: A solid-state device having a substrate that receives an ionizing radiation, logic circuits, integrity circuits, and a collection circuit. The logic circuits are operational to perform logic functions. The logic circuits are located in an area on the substrate, and are individually susceptible to a possible corruption by the ionizing radiation. Each integrity cell is initialized to a predetermined state. The integrity cells are located in the area on the substrate, arranged in a pattern neighboring the logic circuits, and individually susceptible to disrupting the predetermined state in response to the ionizing radiation. The collection circuit is located on the substrate. The collection circuit is operational to read the plurality of integrity cells, and assert a report signal that identifies the possible corruption in a subset of the logic circuits due to the ionizing radiation in response to reading an incorrect state in a neighboring one of the integrity cells.

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