发明名称 Heating elements for aircraft heated floor panels
摘要 A method of forming a heating element includes depositing a conductive ink of silver particles in an epoxy resin on a dielectric film to create a conductive circuit, and heat curing the conductive circuit to achieve a resistivity of the heating element less than 1.68×10−6 ohm·meter. An aircraft heated floor panel includes at least one floor panel of an aircraft includes a conductive circuit positioned within the floor panel having a conductive ink of silver particles in an epoxy resin on a dielectric film.
申请公布号 US9623951(B2) 申请公布日期 2017.04.18
申请号 US201414179281 申请日期 2014.02.12
申请人 Goodrich Corporation 发明人 Hu Jin;Hamm Richard R.;Roach Kevin E.
分类号 B60L1/02;B64C1/18;B64D13/00;F24D13/02;H05B3/16;H05K3/38;H05B3/26;H05K3/12;H05K1/16 主分类号 B60L1/02
代理机构 Locke Lord LLP 代理人 Locke Lord LLP ;Wofsy Scott D.;Carroll Alicia J.
主权项 1. A method of forming a heating element, the method comprising: depositing a conductive ink of silver particles in an epoxy resin on a dielectric film to create a conductive circuit; and heat curing the conductive circuit to achieve a resistivity of the heating element less than 1.68×10−6 ohm·meter, wherein a 0.001 inch (50.8 microns) to 0.004 inch (101.6 microns) thick post-cure layer of the conductive ink is configured to achieve the resistivity of the heating element and be bent around a ¼ inch (0.635 cm) diameter cylinder rod without experiencing electric resistance degradation, wherein the silver loading is between 65%-95% weight/weight of dry ink.
地址 Charlotte NC US