国家/地区 美国（2）
IPC部 B（2）
IPC大类 B32（2）
IPC小类 B32B（2）
IPC B32B037/02（2）
发明人
公开年
申请年
专利权人

Aircraft engine component used as gearboxes, comprises wall comprising aluminum alloy and/or magnesium alloy, and protective coating comprising prime layer, silicone elastomer layer and abrasion resistant layer covering surface of wall.

IURLARO S, GARGIOLI A, GARABELLO M, GAROFALO S, GILARDI E, PICA O, ARGENTIERI G

Resistive heated aircraft component for ice protection system of aircraft, has graphene paper and pair of electrodes that are configured to conduct electrical current and protective layer is located on first face of graphene paper.

BLANCO VARELA T, MARTIN MORENO Z, BUTRAGUENO MARTINEZ A, SANCHEZ HUERTAS G, ADRIAN AROCHA L G, BONNACURSO E, BONACCURSO E, BUTRAGUENOMARTINEZ A, SANCHEZ H G, ADRIAN A L G, BLANCO V T, MARTIN M Z