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 |