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    COMPOSITE PANEL WITH INTEGRATED HEATER SYSTEM AND ASSOCIATED METHODS FOR MANUFACTURING
    6.
    发明申请
    COMPOSITE PANEL WITH INTEGRATED HEATER SYSTEM AND ASSOCIATED METHODS FOR MANUFACTURING 审中-公开
    具有集成加热器系统的复合面板及相关制造方法

    公开(公告)号：US20160270153A1

    公开(公告)日：2016-09-15

    申请号：US15069800

    申请日：2016-03-14

    Applicant: The Boeing Company

    Inventor： Jeffrey L. Duce ,  Marcus K. Richardson ,  Myles E. Brown

    IPC: H05B1/02 ,  H05B3/36 ,  H05B3/54

    CPC classification number: H05B1/0238 ,  F24D13/022 ,  F24D2200/08 ,  F24D2220/2081 ,  F24H9/1872 ,  H05B1/0202 ,  H05B3/20 ,  H05B3/36 ,  H05B2203/013 ,  H05B2203/016 ,  H05B2203/017 ,  H05B2203/02 ,  Y02B30/26

    Abstract: Described herein is a composite panel that includes a first layer made from an electrically non-conductive material. The composite panel also includes a resistance heater printed onto the first layer and a capacitive sensor applied onto the first layer. The capacitive sensor is operably coupled with the resistance heater. The composite panel additionally includes a second layer adjacent the resistance heater and the capacitive sensor. The resistance heater and the capacitive sensor are positioned between the first layer and the second layer. Furthermore, the second layer is made from an electrically non-conductive material. The resistance heater is configured to generate heat at least partially in response to input sensed by the capacitive sensor.

    Abstract translation: 这里描述的是包括由不导电材料制成的第一层的复合面板。 复合面板还包括印刷在第一层上的电阻加热器和施加到第一层上的电容传感器。 电容传感器可操作地与电阻加热器耦合。 复合面板还包括邻近电阻加热器和电容传感器的第二层。 电阻加热器和电容传感器位于第一层和第二层之间。 此外，第二层由不导电材料制成。 电阻加热器被配置为响应于由电容传感器感测的输入而至少部分地产生热量。

    CONTROLLING FLOW OF DRY ICE SUBLIMATION INSIDE A GALLEY CART
    7.
    发明申请
    CONTROLLING FLOW OF DRY ICE SUBLIMATION INSIDE A GALLEY CART 有权
    控制流动的干冰下降在一个GALLEY CART

    公开(公告)号：US20150251758A1

    公开(公告)日：2015-09-10

    申请号：US14202495

    申请日：2014-03-10

    Applicant: The Boeing Company

    Inventor： Bryce A. Vandyke ,  Marcus K. Richardson ,  Chao-Hsin Lin

    IPC: B64D11/00 ,  B62B3/00

    CPC classification number: B64D11/04 ,  B62B3/004 ,  B62B3/005 ,  B64D11/0007 ,  F25D3/125 ,  F25D2600/04

    Abstract: A galley cart system employs a housing with a door coupled to the housing, the door configured to be moved between a closed position and an open position. A vent plate in the housing communicates between a first compartment and a second compartment. A valve plate adjacent the vent plate is movable from a venting position when the door is in the closed position to a blocking position when the door is in the open position thereby preventing flow communication between the first and second compartment.

    Abstract translation: 厨房车系统采用具有与壳体连接的门的壳体，门构造成在关闭位置和打开位置之间移动。 壳体中的排气板在第一隔室和第二隔室之间连通。 当门处于打开位置时，当门处于关闭位置时，邻近排气板的阀板可从通气位置移动，从而防止第一和第二隔室之间的流动连通。

    Systems and methods to produce aircraft cabin supply air
    8.
    发明授权
    Systems and methods to produce aircraft cabin supply air 有权

    公开(公告)号：US11465757B2

    公开(公告)日：2022-10-11

    申请号：US16212167

    申请日：2018-12-06

    Applicant: The Boeing Company

    Inventor： Marcus K. Richardson ,  Steve G. Mackin

    IPC: B64D13/00 ,  B64D13/08 ,  B64D13/06

    Abstract: Systems to produce cabin supply air for aircraft and related methods are described herein. An example system includes an air conditioning pack including a heat exchanger including a first flow path and a second flow path isolated from the first flow path. The second flow path is to receive cabin exhaust air from a cabin of an aircraft. The cabin exhaust air is to reduce a temperature of the cabin supply air flowing through the first flow path of the heat exchanger. The system also includes a turbine to receive the cabin supply air from the heat exchanger. The turbine is to reduce a temperature and pressure of the cabin supply air. A turbine outlet of the turbine is fluidly coupled to the cabin to provide the cabin supply air to the cabin. The system further includes a fan to direct the cabin exhaust air from the heat exchanger.

    SYSTEMS AND METHODS TO PRODUCE AIRCRAFT CABIN SUPPLY AIR
    10.
    发明申请
    SYSTEMS AND METHODS TO PRODUCE AIRCRAFT CABIN SUPPLY AIR 审中-公开

    公开(公告)号：US20200180772A1

    公开(公告)日：2020-06-11

    申请号：US16212167

    申请日：2018-12-06

    Applicant: The Boeing Company

    Inventor： Marcus K. Richardson ,  Steve G. Mackin

    IPC: B64D13/08 ,  B64D13/06

    Abstract: Systems to produce cabin supply air for aircraft and related methods are described herein. An example system includes an air conditioning pack including a heat exchanger including a first flow path and a second flow path isolated from the first flow path. The second flow path is to receive cabin exhaust air from a cabin of an aircraft. The cabin exhaust air is to reduce a temperature of the cabin supply air flowing through the first flow path of the heat exchanger. The system also includes a turbine to receive the cabin supply air from the heat exchanger. The turbine is to reduce a temperature and pressure of the cabin supply air. A turbine outlet of the turbine is fluidly coupled to the cabin to provide the cabin supply air to the cabin. The system further includes a fan to direct the cabin exhaust air from the heat exchanger.

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