中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

27 records (took 0.018 seconds)

    Cabin outflow air energy optimized cabin pressurizing system
    1.
    发明授权
    Cabin outflow air energy optimized cabin pressurizing system 有权

    公开(公告)号：US11661197B2

    公开(公告)日：2023-05-30

    申请号：US16949438

    申请日：2020-10-29

    Applicant: Honeywell International Inc.

    Inventor： Charles Lo

    IPC: B64D13/02 ,  B64D13/06

    CPC classification number: B64D13/02 ,  B64D13/06 ,  B64D2013/0611 ,  B64D2013/0618 ,  B64D2013/0644 ,  B64D2013/0648 ,  B64D2013/0688

    Abstract: A pressurization system includes a first compressor that receives a ram air, a fan air, or engine air; a first turbine that is on a common shaft with the first compressor and wherein the first turbine receives an engine air; a main heat exchanger downstream of the first compressor and the first turbine; an internal environment suitable for human occupants and downstream of the main heat exchanger; a second turbine downstream of the internal environment; the second turbine may be on the common shaft with the first compressor and first turbine; or a generator downstream of the second turbine; a motor downstream of the generator; and wherein the motor drives the first compressor.

    HYDROCARBON PYROLYSIS SUBSTRATES AND SYSTEMS
    2.
    发明申请
    HYDROCARBON PYROLYSIS SUBSTRATES AND SYSTEMS 有权

    公开(公告)号：US20250033011A1

    公开(公告)日：2025-01-30

    申请号：US18361431

    申请日：2023-07-28

    Applicant: Honeywell International Inc.

    Inventor： Mark Triezenberg ,  Amanda Childers ,  Abigail Parsons ,  Charles Lo

    IPC: B01J4/00 ,  B01J6/00

    Abstract: A fibrous substrate for depositing carbon generated from pyrolysis of a hydrocarbon may include at least one roll defining a plurality of rolled deposition surfaces configured to receive carbon generated from the pyrolysis. The fibrous substrate may further include at least one spacer between and spacing at least one pair of opposed deposition surfaces of the plurality of rolled deposition surfaces. A system for generating hydrogen gas may include a pyrolysis reactor configured to generate the hydrogen gas from a hydrocarbon through pyrolysis. The system may further include the fibrous substrate. A method for forming the fibrous substrate may include positioning the at least one spacer on a surface of a fibrous mat, and rolling the fibrous mat into the at least one roll.

    IN-LINE CENTRIFUGE-SEPARATOR PUMP
    4.
    发明申请
    IN-LINE CENTRIFUGE-SEPARATOR PUMP 有权
    在线离心分离泵

    公开(公告)号：US20170056789A1

    公开(公告)日：2017-03-02

    申请号：US14686165

    申请日：2015-04-14

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Charles Lo

    IPC: B01D19/00 ,  B64D37/32 ,  F04D29/043 ,  B64D37/34 ,  F04D7/02 ,  F04D29/24

    CPC classification number: B01D19/0057 ,  B01D19/0005 ,  B01D45/14 ,  B64D37/32 ,  B64D37/34 ,  F04D7/02

    Abstract: An in-line centrifuge-separator pump includes a shaft, a shroud, and a plurality of spaced-apart corrugated, and concentrically disposed separator structures. The shaft is adapted to receive a drive torque and is configured, upon receipt thereof, to rotate. The shroud is spaced apart from and is coupled to the shaft to be rotated thereby. The separator structures are at least partially disposed within the shroud and are coupled to both the shroud and the shaft to simultaneously rotate therewith. Each separator structure has a plurality of perforations formed therein.

    Abstract translation: 在线离心分离器泵包括轴，护罩和多个间隔开的波纹和同心设置的分离器结构。 轴适于接收驱动扭矩，并在其接收时被配置为旋转。 护罩与轴间隔开并联接到轴上以便旋转。 分离器结构至少部分地设置在护罩内并且联接到护罩和轴两者以同时与其一起旋转。 每个分离器结构在其中形成有多个穿孔。

    AIRCRAFT FUEL DEOXYGENATION SYSTEM
    5.
    发明申请
    AIRCRAFT FUEL DEOXYGENATION SYSTEM 有权
    飞机燃料消除系统

    公开(公告)号：US20160167802A1

    公开(公告)日：2016-06-16

    申请号：US14570152

    申请日：2014-12-15

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Charles Lo ,  Eric Blumer ,  Dan Laboda ,  Alexander Bershitsky

    IPC: B64D37/34 ,  B01D35/02 ,  B01D46/00 ,  B01D19/00

    CPC classification number: B64D37/34 ,  B01D19/0005 ,  B01D19/0047 ,  B01D19/0057 ,  B01D19/0068 ,  B01D35/02 ,  B01D46/00

    Abstract: An aircraft fuel deoxygenation system includes a boost pump, a contactor-separator, and a centrifuge-separator pump. The boost pump is adapted to receive fuel from a fuel source and inert gas from an inert gas source, and is configured to mix the fuel and inert gas and supply a fuel/gas mixture. The contactor-separator is coupled to receive the fuel/gas mixture and is configured to remove oxygen from the fuel and thereby generate and supply deoxygenated fuel with entrained purge gas and separated purge gas. The centrifuge-separator pump is coupled to receive the deoxygenated fuel with entrained purge gas and is configured to separate and remove the entrained purge gas from the deoxygenated fuel and supply the deoxygenated fuel and additional purge gas.

    Abstract translation: 飞机燃料脱氧系统包括增压泵，接触器分离器和离心分离泵。 增压泵适于从燃料源接收燃料和来自惰性气体源的惰性气体，并且被配置为混合燃料和惰性气体并提供燃料/气体混合物。 接触器分离器联接以接收燃料/气体混合物，并且被配置为从燃料中除去氧气，从而产生并提供带有夹带的净化气体和分离的净化气体的脱氧燃料。 离心分离器泵耦合以接收带有夹带的净化气体的脱氧燃料，并且构造成分离并除去来自脱氧燃料的夹带的净化气体，并提供脱氧燃料和另外的净化气体。

    Low loss passive optical hub for use in the plastic optical fiber networks
    6.
    发明授权
    Low loss passive optical hub for use in the plastic optical fiber networks 有权
    用于塑料光纤网络的低损耗无源光学集线器

    公开(公告)号：US09164241B2

    公开(公告)日：2015-10-20

    申请号：US13945545

    申请日：2013-07-18

    Applicant: Honeywell International Inc.

    Inventor： Charles Lo

    IPC: G02B6/287 ,  G02B6/28 ,  B29L11/00

    CPC classification number: G02B6/287 ,  B29L2011/0075 ,  G02B6/2856 ,  Y10T156/1052

    Abstract: A node for a low loss passive optical hub is provided. The low loss passive optical hub includes a 1:N-split fiber and a plastic-optical fiber. The 1:N-split fiber has a fused-fractional end and N second-fractional ends. The 1:N-split fiber is formed from N sub-fibers. The N sub-fibers each have a first-fractional end and a second-fractional end. The N first-fractional ends are fused to form the fused-fractional end. The plastic-optical fiber has a first end and a second end. The first end of the plastic-optical fiber is optically coupled to the fused-fractional end of the 1:N-split fiber.

    Abstract translation: 提供了一种用于低损耗无源光学集线器的节点。 低损耗无源光学集线器包括1：N分离光纤和塑料光纤。 1：N分裂光纤具有熔融分数端和N个第二分数端。 1：N分割纤维由N个子纤维形成。 N个子纤维各自具有第一分数末端和第二分数末端。 N个第一分数端被融合以形成熔融分数端。 塑料光纤具有第一端和第二端。 塑料光纤的第一端光耦合到1：N分割光纤的熔断端。

    AIRCRAFT LANDING GEAR WHEEL-DRIVE SYSTEM
    10.
    发明申请
    AIRCRAFT LANDING GEAR WHEEL-DRIVE SYSTEM 有权
    飞机起落架齿轮传动系统

    公开(公告)号：US20170057624A1

    公开(公告)日：2017-03-02

    申请号：US14839065

    申请日：2015-08-28

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Charles Lo ,  Allan Steves

    IPC: B64C25/34 ,  B64C25/40 ,  B64C25/42

    CPC classification number: B64C25/405 ,  B60T1/10 ,  B60T8/1703 ,  B60T10/04 ,  B60T2270/60 ,  B60W30/18127 ,  B64C25/42 ,  F16D57/06 ,  Y02T50/823

    Abstract: An aircraft landing gear wheel-drive system includes a first wheel drive unit for driving a first landing gear wheel of the aircraft and a second wheel drive unit for driving a second landing gear wheel of the aircraft. The first wheel drive unit has a first range of torque to speed (T/S) ratios. The second wheel drive unit has a second range of T/S ratios. The first range of T/S ratios is greater than the second range of T/S ratios.

    Abstract translation: 飞机起落架驱动系统包括用于驱动飞行器的第一起落架的第一轮驱动单元和用于驱动飞行器的第二起落架的第二轮驱动单元。 第一轮驱动单元具有第一范围的转矩（T / S）比。 第二轮驱动单元具有第二范围的T / S比。 T / S比率的第一范围大于T / S比的第二范围。

Patent Agency Ranking