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84 条记录 (耗时 0.013 秒)

    Carbon nanotube yarn heater
    22.
    发明授权
    Carbon nanotube yarn heater 有权

    公开(公告)号：US10425993B2

    公开(公告)日：2019-09-24

    申请号：US15373368

    申请日：2016-12-08

    申请人： Goodrich Corporation

    发明人： Casey Slane ,  Jin Hu ,  Galdemir Cezar Botura ,  Nathaniel Ching

    IPC分类号： H05B3/12 ,  H05B3/14 ,  H05B3/20 ,  H05B3/28 ,  H05B3/34

    摘要： A heating element includes a bottom layer, a web consisting of a carbon nanotube (CNT) yarn wherein the web is affixed to a first side of the bottom layer, and an encapsulating layer positioned on the web and the first side of the bottom layer. A method for making a heating element includes providing a bottom layer, inserting a plurality of pegs into the bottom layer such that a portion of each peg protrudes from the bottom layer, weaving a CNT yarn around the protruding portions of the plurality of pegs to form a CNT web, affixing the CNT web to the bottom layer, and encapsulating the CNT web and the bottom layer to form the heating element.

    Adjusting CNT resistance using perforated CNT sheets
    24.
    发明授权
    Adjusting CNT resistance using perforated CNT sheets 有权

    公开(公告)号：US10264627B2

    公开(公告)日：2019-04-16

    申请号：US15373363

    申请日：2016-12-08

    申请人： Goodrich Corporation

    发明人： Brad Hartzler ,  Tommy M. Wilson, Jr. ,  Galdemir Cezar Botura ,  Wenping Zhao ,  Zaffir A. Chaudhry ,  James A. Mullen

    IPC分类号： H05B3/20 ,  H05B3/10 ,  H05B3/12 ,  H05B3/14 ,  H05B3/40 ,  H05B3/00 ,  H05B3/34

    摘要： One example of a heating element includes a first carbon nanotube (CNT) layer and a second CNT layer. At least a portion of the first CNT layer overlaps at least a portion of the second CNT layer, and the first CNT layer includes a first perforated region having a plurality of perforations. Another heating element includes a CNT sheet with a first perforated region having a plurality of perforations and a first perforation density and a second perforated region having a plurality of perforations and a second perforation density different from the first perforation density. A method of forming a heating element includes perforating a first CNT layer so that it includes a perforated region and stacking the first CNT layer with a second CNT layer such that at least a portion of the first CNT layer overlaps at least a portion of the second CNT layer.

    Aircraft ice protection optimization based on ice-detection input
    28.
    发明授权
    Aircraft ice protection optimization based on ice-detection input 有权
    基于冰检测输入的飞机防冰优化

    公开(公告)号：US09555894B2

    公开(公告)日：2017-01-31

    申请号：US13871207

    申请日：2013-04-26

    申请人： GOODRICH CORPORATION

    发明人： Galdemir Cezar Botura ,  Dave Bert Sweet ,  James Thomas Hindel ,  Darren Glenn Jackson

    IPC分类号： B64D15/12 ,  B64D15/20

    CPC分类号： B64D15/12 ,  B64D15/20 ,  B64D15/22

    摘要： An aircraft ice protection system (10) comprises an ice protection device (21), an onboard power source (30), a supply line (31) from the power source (30) to the device (21), a controller (41) which controls the line (31), and an optimizer (50) which conveys operation-optimizing instructions (51) to the controller (41). An ice detector (60) provides an input (70) to the optimizer (50) and this ice-condition input (70) is used to generate the operation-optimizing instructions (51).

    摘要翻译： 飞机防冰系统（10）包括防冰装置（21），车载电源（30），从电源（30）到装置（21）的供应管线（31），控制器（41） 控制线路（31）的优化器（50）和将操作优化指令（51）传送到控制器（41）的优化器（50）。 冰检测器（60）向优化器（50）提供输入（70），并且该冰条件输入（70）用于产生操作优化指令（51）。

    Control of electric pump-driven deicer
    29.
    发明授权
    Control of electric pump-driven deicer 有权

    公开(公告)号：US12097963B2

    公开(公告)日：2024-09-24

    申请号：US17495260

    申请日：2021-10-06

    申请人： Goodrich Corporation

    发明人： Casey Slane ,  Jeffrey Martin Werbelow ,  Guangqing Shen ,  Galdemir Cezar Botura

    IPC分类号： B64D15/22 ,  B64D15/16

    CPC分类号： B64D15/22 ,  B64D15/166

    摘要： Examples described herein provide a computer-implemented method that includes receiving static data about an aircraft. The method further includes receiving dynamic data about flight conditions for a flight of the aircraft. The method further includes determining, based on the static data and the dynamic data, an amount of air pressure and a volumetric air flow to apply from an electric pump to a deicing device. The method further includes controlling the electric pump to cause the electric pump to apply the amount of air pressure and the volumetric air flow to the deicing device.

    Carbon nanotube yarn for pneumatic de-icer stitching
    30.
    发明授权
    Carbon nanotube yarn for pneumatic de-icer stitching 有权

    公开(公告)号：US11975849B2

    公开(公告)日：2024-05-07

    申请号：US17346731

    申请日：2021-06-14

    申请人： Goodrich Corporation

    发明人： Casey Slane ,  Daniel Waina ,  Galdemir Cezar Botura

    IPC分类号： B32B9/00 ,  B64D15/16 ,  C01B32/158 ,  D02G3/02

    CPC分类号： B64D15/166 ,  C01B32/158 ,  D02G3/02 ,  C01B2202/22 ,  D10B2101/122

    摘要： A de-icing assembly for a surface of an aircraft includes: a carcass with a first layer, a second layer, and a carcass centerline and a plurality of seams sewn into the carcass, wherein the plurality of seams join the first and second layers of the carcass together. The assembly includes a plurality of inflation passages formed by the plurality of seams and disposed between the first and second layers of the carcass. The system also includes a manifold fluidly connected to and disposed beneath the carcass, the manifold comprising a width and a manifold centerline oriented approximately perpendicular or parallel to the carcass centerline. The seams are sown by a stitchline formed of carbon nanotube yarn.