HEATED FLOOR PANELS
    31.
    发明申请
    HEATED FLOOR PANELS 审中-公开

    公开(公告)号:US20200011542A1

    公开(公告)日:2020-01-09

    申请号:US16026336

    申请日:2018-07-03

    Abstract: A heater panel includes a core and a heater/dielectric layer including a positive thermal coefficient (PTC) heater layer between a pair of dielectric layers. A structural facing is included, wherein the heater/dielectric layer is bonded directly between the core and the structural facing. A second structural facing can be bonded to the core opposite the heater/dielectric layer. An impact layer can be bonded to the structural facing, e.g., the first structural facing described above, opposite the heater/dielectric layer.

    Carbon nanotube yarn heater
    32.
    发明授权

    公开(公告)号:US10425993B2

    公开(公告)日:2019-09-24

    申请号:US15373368

    申请日:2016-12-08

    Abstract: 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.

    Control of electric pump-driven deicer

    公开(公告)号:US12097963B2

    公开(公告)日:2024-09-24

    申请号:US17495260

    申请日:2021-10-06

    CPC classification number: B64D15/22 B64D15/166

    Abstract: 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

    公开(公告)号:US11975849B2

    公开(公告)日:2024-05-07

    申请号:US17346731

    申请日:2021-06-14

    Abstract: 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.

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