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    Aircraft and airborne electrical power and thermal management system
    1.
    发明授权
    Aircraft and airborne electrical power and thermal management system 有权
    飞机和机载电力和热力管理系统

    公开(公告)号：US08967531B2

    公开(公告)日：2015-03-03

    申请号：US13432842

    申请日：2012-03-28

    Applicant: Steven Gagne ,  Rigoberto Rodriguez ,  William L. Siegel ,  John R. Arvin

    Inventor： Steven Gagne ,  Rigoberto Rodriguez ,  William L. Siegel ,  John R. Arvin

    IPC: B64D41/00 ,  B64D13/00 ,  B64D13/08 ,  F02C7/32 ,  B64D13/06

    CPC classification number: B64D13/006 ,  B64D13/08 ,  B64D33/04 ,  B64D33/08 ,  B64D41/00 ,  B64D41/007 ,  B64D2013/0614 ,  B64D2013/0674 ,  F02C6/08 ,  F02C7/32 ,  H02K7/1823

    Abstract: A unique airborne electrical power and thermal management system and a unique aircraft having a unique airborne electrical power and thermal management system are provided. The electrical power and thermal management system includes a turbine, which may power loads, for example but not limited to, a generator and a refrigerant compressor. The turbine may be in fluid communication with a gas turbine engine bleed air source to extract power from bleed air for powering the loads. A combustor may be fluidly disposed between the bleed air source and the turbine. The turbine may be part of a gas turbine engine distinct from a propulsion gas turbine engine. In one aspect, at least a portion of the electrical power and thermal management system may be disposed within an aircraft external pod. The pod may be configured to appear similar to a conventional external fuel tank pod employed by the aircraft.

    Abstract translation: 提供独特的机载电力和热管理系统和独特的飞机，具有独特的机载电力和热管理系统。 电力和热管理系统包括涡轮机，其可以为例如但不限于发电机和制冷剂压缩机的负载供电。 涡轮机可以与燃气涡轮发动机排气源流体连通，以从放气中提取动力以为负载供电。 燃烧器可以流体地设置在排放空气源和涡轮机之间。 涡轮机可以是不同于推进燃气涡轮发动机的燃气涡轮发动机的一部分。 在一个方面，电力和热管理系统的至少一部分可以设置在飞行器外部舱内。 荚可以被配置为看起来类似于飞机使用的常规外部燃料箱舱。

    AIRBORNE COOLING SYSTEM
    2.
    发明申请
    AIRBORNE COOLING SYSTEM 有权
    AIRBORNE冷却系统

    公开(公告)号：US20120256045A1

    公开(公告)日：2012-10-11

    申请号：US13432482

    申请日：2012-03-28

    Applicant: Steven Gagne

    Inventor： Steven Gagne

    IPC: B64D33/10 ,  B64D1/12

    CPC classification number: B64D1/08 ,  B64D13/00 ,  B64D33/10 ,  B64D2013/0614 ,  B64D2013/0674 ,  F28D5/00 ,  F28D2021/0021 ,  F41H13/0043 ,  F42B15/34

    Abstract: An aircraft having a cooling system is disclosed. The cooling system can be used to cool a heat emitting component. In one form the cooling system is a refrigerant system and includes a relatively high temperature device such as, but not limited to, a condenser. The relatively high temperature component is placed in thermal communication with a passing air flow. In one embodiment the aircraft includes a pod in which at least a portion of the cooling system is disposed. For example, a condenser of a vapor cycle refrigerant system can be located in the pod and in thermal communication with the air flow. The cooling system can also include a device capable of delivering a cooling fluid into the air flow and/or to the relatively high temperature component. The cooling fluid can be evaporated to provided additional cooling.

    Abstract translation: 公开了一种具有冷却系统的飞机。 冷却系统可用于冷却发热部件。 在一种形式中，冷却系统是制冷剂系统，并且包括相对高温的装置，例如但不限于冷凝器。 相对较高的温度部件被放置成与通过的空气流热连通。 在一个实施例中，飞行器包括其中布置有冷却系统的至少一部分的舱。 例如，蒸气循环制冷剂系统的冷凝器可以位于容器中并与气流热连通。 冷却系统还可以包括能够将冷却流体输送到空气流和/或相对高温部件的装置。 冷却液可以被蒸发以提供额外的冷却。

    Carrier for a paint tray
    3.
    发明授权
    Carrier for a paint tray 失效
    载体油漆托盘

    公开(公告)号：US07194786B2

    公开(公告)日：2007-03-27

    申请号：US10841170

    申请日：2004-05-07

    Applicant: Larry Steven Gagne

    Inventor： Larry Steven Gagne

    IPC: A45C3/00

    CPC classification number: B44D3/14 ,  Y10T16/44 ,  Y10T16/4559

    Abstract: A carrier for a paint tray is provided, the tray having an inner wall defining a container for containing paint and an outer wall for supporting the container, the inner and outer walls defining a space therebetween accessible from underneath the tray. The carrier comprises a coupler for coupling to the paint tray and a lifting member connected to the coupler. The coupler comprises a coupling member for insertion into the space between said inner and outer wall and having wall engaging means for engaging the interior faces of both said inner and outer walls simultaneously when inserted into said space to secure the member within the space and to support said tray from the coupling member.

    Abstract translation: 提供了用于油漆托盘的托架，托盘具有限定用于容纳油漆的容器的内壁和用于支撑容器的外壁，内壁和外壁限定了可从托盘下方进入的空间。 载体包括用于联接到油漆盘的耦合器和连接到耦合器的提升构件。 联接器包括用于插入到所述内壁和外壁之间的空间中的联接构件，并且具有壁接合装置，用于当插入所述空间中时同时接合所述内壁和外壁的内表面，以将构件固定在空间内并支撑 所述托盘来自联接构件。

    Paint container holder
    6.
    发明授权
    Paint container holder 有权
    油漆容器架

    公开(公告)号：US08366061B2

    公开(公告)日：2013-02-05

    申请号：US11995604

    申请日：2006-07-14

    Applicant: Joseph Lorney Rose ,  Larry Steven Gagne

    Inventor： Joseph Lorney Rose ,  Larry Steven Gagne

    IPC: A47G23/02

    CPC classification number: B44D3/14 ,  B44D3/126

    Abstract: A holder for a paint container can be used on uneven surfaces. The holder comprises a support base. Pivotally coupled to the support base is at least one leg and/or a lifting member. The at least one leg is selectively positionable for fixing the angular orientation of the at least one leg relative to the paint container support base. The lifting member may be located to support a paint container across a lateral axis extending substantially above a combined center of gravity of the holder and the paint container.

    Abstract translation: 用于油漆容器的支架可用于不平坦的表面。 保持器包括支撑基座。 枢转地联接到支撑基座上的是至少一个腿部和/或提升部件。 所述至少一个腿部可选择性地定位成用于固定所述至少一个腿部相对于所述涂料容器支撑基座的角度取向。 提升构件可以被定位成在基本上在保持器和油漆容器的组合重心上方延伸的横向轴线上支撑油漆容器。

    THERMAL SYSTEM HAVING ELECTRICAL DEVICE
    7.
    发明申请
    THERMAL SYSTEM HAVING ELECTRICAL DEVICE 审中-公开
    具有电气设备的热系统

    公开(公告)号：US20120266612A1

    公开(公告)日：2012-10-25

    申请号：US13451643

    申请日：2012-04-20

    Applicant: Rigoberto Rodriguez ,  Steven Gagne ,  Donald W. Burns

    Inventor： Rigoberto Rodriguez ,  Steven Gagne ,  Donald W. Burns

    IPC: F25D31/00 ,  H05K7/20 ,  H02K9/00

    CPC classification number: H05K7/20936 ,  F25B31/006 ,  H02K9/12 ,  H02K9/14 ,  H02K11/33

    Abstract: A thermal system is disclosed in thermal communication with an electrical device. In one form the thermal system is a refrigeration system having a compressor, condenser, and evaporator. The electrical device can be disposed within the thermal system such that a working fluid of the thermal system exchanges heat with the electrical device. In one embodiment the thermal system includes a container in which the electrical device is disposed. The working fluid in the container can, but need not, remain in substantially the same physical state when transferring heat with the electrical device.

    Abstract translation: 公开了一种与电气设备热连接的热系统。 在一种形式中，热系统是具有压缩机，冷凝器和蒸发器的制冷系统。 电气设备可以设置在热系统内，使得热系统的工作流体与电气设备交换热量。 在一个实施例中，热系统包括其中设置电气设备的容器。 当与电气设备传热时，容器中的工作流体可以但不一定保持基本上相同的物理状态。

    LANDFILL GAS UTILIZATION
    10.
    发明申请
    LANDFILL GAS UTILIZATION 审中-公开
    LANDFILL气体利用

    公开(公告)号：US20110283708A1

    公开(公告)日：2011-11-24

    申请号：US12786361

    申请日：2010-05-24

    Applicant: RIGO RODRIGUEZ ,  Mat French ,  George Hutchins ,  Steven Gagne

    Inventor： RIGO RODRIGUEZ ,  Mat French ,  George Hutchins ,  Steven Gagne

    IPC: F02C3/22

    CPC classification number: F02C3/22 ,  F01D25/08 ,  F02C3/20 ,  F02C3/28 ,  F02C7/18 ,  F02C7/224 ,  F02C7/32 ,  F02K9/64 ,  F05B2260/205 ,  F05D2220/75

    Abstract: A method for utilizing landfill gas is disclosed herein. The method includes the step of collecting landfill gas. The method also includes the step of fueling a turbine engine that is at least part of a power generation system with the landfill gas to generate power. The method also includes the step of cooling one or more components of the power generation system with the landfill gas prior to the fueling step. A power generation system capable of practicing the method is also disclosed. A landfill gas utilization system capable of practicing the method is also disclosed.

    Abstract translation: 本文公开了一种利用填埋气体的方法。 该方法包括收集填埋气体的步骤。 该方法还包括对具有填埋气体的发电系统的至少一部分的涡轮发动机加油以发电的步骤。 该方法还包括在加油步骤之前用填埋气体冷却发电系统的一个或多个组件的步骤。 还公开了能够实施该方法的发电系统。 还公开了能够实施该方法的填埋气体利用系统。

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