国家/地区 世界知识产权组织（2）
IPC部 B（3）
IPC大类 B64（3） B05（2） C09（2）
F02（2）
IPC小类 B64D（3）
IPC B05D001/36（2） B05D005/00（2） C09D005/00（2）
C09D007/61（2） C09D007/65（2）
发明人
公开年 2023（3）
申请年 2022（3）
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

Coated product used in e.g. aircraft propulsion system component, comprises product, and coating applied to at least part of product, where coating comprises polymer matrix material, inorganic filler, organic filler, and lamellar filler.

PICOT O, BEDEL V

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