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    Aircraft with Electrically Conductive Nanocoating
    1.
    发明申请
    Aircraft with Electrically Conductive Nanocoating 有权
    具有导电纳米涂层的飞机

    公开(公告)号：US20140252164A1

    公开(公告)日：2014-09-11

    申请号：US13789269

    申请日：2013-03-07

    Applicant: BELL HELICOPTER TEXTRON INC.

    Inventor： Daniel P. Sottiaux ,  Hunter Davis

    IPC: H01B5/14 ,  B64D45/02

    CPC classification number: H01B5/14 ,  B64C27/35 ,  B64D45/02 ,  C09D5/24 ,  H05K9/0079

    Abstract: A device has a first electrically conductive component, a second electrically conductive component, and an electrically conductive nanocoating (ECN) electrically connecting the first electrically conductive component to the second electrically conductive component. An aircraft has an engine, a fuselage, and a device having a first electrically conductive component, a second electrically conductive component, and an electrically conductive nanocoating (ECN) electrically connecting the first electrically conductive component to the second electrically conductive component. A method of providing an electrical conduction path includes providing a first electrically conductive component, providing a second electrically conductive component, and decreasing an electrical resistance between the first electrically conductive component and the second electrically conductive component using an electrically conductive nanocoating (ECN).

    Abstract translation: 器件具有第一导电部件，第二导电部件和将第一导电部件电连接到第二导电部件的导电纳米涂覆（ECN）。 飞机具有发动机，机身以及具有第一导电部件，第二导电部件和将第一导电部件电连接到第二导电部件的导电纳米涂层（ECN）的装置。 提供导电路径的方法包括提供第一导电部件，提供第二导电部件，以及使用导电纳米涂层（ECN）减小第一导电部件和第二导电部件之间的电阻。

    Aircraft with Protective Nanocoating
    2.
    发明申请
    Aircraft with Protective Nanocoating 有权
    具有防护纳米技术的飞机

    公开(公告)号：US20140252157A1

    公开(公告)日：2014-09-11

    申请号：US13789273

    申请日：2013-03-07

    Applicant: BELL HELICOPTER TEXTRON INC.

    Inventor： Daniel P. Sottiaux ,  Frank Bradley Stamps

    IPC: F16C33/04

    CPC classification number: B64C27/35 ,  B64D2045/009 ,  F16C33/04 ,  F16C33/121

    Abstract: An aircraft component has an exterior surface and a protective nanocoating carried by the exterior surface. An aircraft has an engine, a fuselage, and a component having an exterior surface and a protective nano coating carried by the exterior surface. A method of protecting an aircraft component includes selecting at least one harmful environmental component and applying a protective nanocoating to the aircraft component, wherein the protective nanocoating is configured to protect the aircraft component from the selected harmful environmental component.

    Abstract translation: 飞机部件具有由外表面承载的外表面和保护性纳米涂层。 飞机具有发动机，机身和具有由外表面承载的外表面和保护性纳米涂层的部件。 保护飞行器部件的方法包括选择至少一个有害的环境部件并对飞行器部件施加保护性纳米涂覆，其中所述保护性纳米覆盖被配置为保护飞行器部件免受所选择的有害环境部件的影响。

    Aircraft with electrically conductive nanocoating
    7.
    发明授权
    Aircraft with electrically conductive nanocoating 有权
    具有导电纳米涂层的飞机

    公开(公告)号：US08998124B2

    公开(公告)日：2015-04-07

    申请号：US13789269

    申请日：2013-03-07

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Daniel P. Sottiaux ,  Hunter Davis

    IPC: H01B5/14 ,  B64D45/02 ,  C09D5/24 ,  B64C27/35 ,  H05K9/00

    CPC classification number: H01B5/14 ,  B64C27/35 ,  B64D45/02 ,  C09D5/24 ,  H05K9/0079

    Abstract: A device has a first electrically conductive component, a second electrically conductive component, and an electrically conductive nanocoating (ECN) electrically connecting the first electrically conductive component to the second electrically conductive component. An aircraft has an engine, a fuselage, and a device having a first electrically conductive component, a second electrically conductive component, and an electrically conductive nanocoating (ECN) electrically connecting the first electrically conductive component to the second electrically conductive component. A method of providing an electrical conduction path includes providing a first electrically conductive component, providing a second electrically conductive component, and decreasing an electrical resistance between the first electrically conductive component and the second electrically conductive component using an electrically conductive nanocoating (ECN).

    Abstract translation: 器件具有第一导电部件，第二导电部件和将第一导电部件电连接到第二导电部件的导电纳米涂覆（ECN）。 飞机具有发动机，机身以及具有第一导电部件，第二导电部件和将第一导电部件电连接到第二导电部件的导电纳米涂层（ECN）的装置。 提供导电路径的方法包括提供第一导电部件，提供第二导电部件，以及使用导电纳米涂覆（ECN）减小第一导电部件和第二导电部件之间的电阻。

    Low Shear Modulus Transition Shim for Elastomeric Bearing Bonding in Torsional Applications
    8.
    发明申请
    Low Shear Modulus Transition Shim for Elastomeric Bearing Bonding in Torsional Applications 有权
    低剪切模量过渡垫用于扭转应用中的弹性轴承粘合

    公开(公告)号：US20140255191A1

    公开(公告)日：2014-09-11

    申请号：US13793683

    申请日：2013-03-11

    Applicant: BELL HELICOPTER TEXTRON INC.

    Inventor： Chad Lewis Jarrett ,  Frank Bradley Stamps ,  Daniel P. Sottiaux

    IPC: F16C33/04 ,  F16C27/02 ,  B64C27/35

    CPC classification number: F16C33/04 ,  B64C27/33 ,  B64C27/35 ,  F16C27/02 ,  F16F1/3842

    Abstract: A bearing assembly comprises a bearing, a shim disposed within the bearing, and a component disposed within the shim. The shim comprises a first material, the component comprises a second material, and the first material has an elastic modulus value that is lower than an elastic modulus value of the second material. An apparatus comprises an elastomeric bearing, a fiberglass shim, and a steel spindle that is connected to the elastomeric bearing through the shim. A method for reducing strain in an adhesive layer that connects a bearing to a component comprises selecting a shim material having an elastic modulus value that is less than an elastic modulus value of the component and providing instructions to connect the component to the shim by placing the adhesive layer between an outer surface of the component and an inner surface of the shim.

    Abstract translation: 轴承组件包括轴承，设置在轴承内的垫片和设置在垫片内的部件。 垫片包括第一材料，该部件包括第二材料，并且第一材料具有低于第二材料的弹性模量值的弹性模量值。 一种装置包括弹性轴承，玻璃纤维垫片和通过垫片连接到弹性轴承的钢质心轴。 一种用于减小将轴承与部件连接在一起的粘合剂层中的应变的方法包括选择弹性模量值小于该部件的弹性模量值的垫片材料，并提供将部件连接到垫片上的指令， 组件的外表面和垫片的内表面之间的粘合剂层。

    Aircraft with protective nanocoating
    10.
    发明授权
    Aircraft with protective nanocoating 有权
    具有保护性纳米涂层的飞机

    公开(公告)号：US09352829B2

    公开(公告)日：2016-05-31

    申请号：US13789273

    申请日：2013-03-07

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Daniel P. Sottiaux ,  Frank Bradley Stamps

    IPC: B64C27/35 ,  F16C33/12 ,  F16C33/04 ,  B64D45/00

    CPC classification number: B64C27/35 ,  B64D2045/009 ,  F16C33/04 ,  F16C33/121

    Abstract: An aircraft component has an exterior surface and a protective nanocoating carried by the exterior surface. An aircraft has an engine, a fuselage, and a component having an exterior surface and a protective nano coating carried by the exterior surface. A method of protecting an aircraft component includes selecting at least one harmful environmental component and applying a protective nanocoating to the aircraft component, wherein the protective nanocoating is configured to protect the aircraft component from the selected harmful environmental component.

    Abstract translation: 飞机部件具有由外表面承载的外表面和保护性纳米涂层。 飞机具有发动机，机身和具有由外表面承载的外表面和保护性纳米涂层的部件。 保护飞行器部件的方法包括选择至少一个有害的环境部件并对飞行器部件施加保护性纳米涂覆，其中所述保护性纳米覆盖被配置为保护飞行器部件免受所选择的有害环境部件的影响。

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