国家/地区 世界知识产权组织（2）
IPC部 B（2）
IPC大类 B64（2）
IPC小类 B64D（2）
IPC F02C007/047（2）
发明人
公开年
申请年
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

Thermally-conductive film of heating apparatus mounted in gas turbine engine, comprises graphene sheet and resin sheet that are formed in sheet form by making surface direction or out-plane direction into thickness direction.

IKEDA K, ISHIKAWA N, FUNATSU T, OYAMA K