国家/地区 法国（2）
IPC部 B（2）
IPC大类 B64（2）
IPC小类 B64D（2）
IPC
发明人
公开年
申请年 2022（2）
专利权人

Annular air inlet lip for nacelle of e.g. turbofan engine of aircraft, has upstream annular wall connecting external and internal annular walls to delimit cavity, where thermal transfer coating is located on portions of surface of lip.

DIGEOS V E A, COATLENZOTTI C, LE DOCTE T J A

Solid polymer conductive composite used for non-metallic aircraft fuel delivery system component, is prepared from composition comprising polyaryletherketone polymer, conductive filler, and dispersing and processing additive.

MAPKAR J A, SALUNKE N, DEMUTH M J