国家/地区 欧洲专利局（EPO）（6）
IPC部 F（6）
IPC大类 F01（6） B32（2） C23（2）
IPC小类 F01D（6）
IPC F01D005/28（4） B32B009/00（2） C23C028/00（2）
F01D005/14（2）
发明人
公开年
申请年 2011（2）  2016（2） 
专利权人 SIEMENS AG（2）

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

Blade comprises metallic substrate and coating system atop the substrate at the tip and comprises first layer of nickel, abrasive layer, comprises matrix and abrasive is partially embedded in the matrix.

JOOST W J, MAALOUF F S, MARTEL N T

Graphene heat pipe for gas turbine engine for aircraft, comprises body with graphene, where body is provided with hot side to accept heat from gas turbine engine, and end cap is provided to establish closed fluid flow environment.

FORCIER M P, STAUBACH J B

Wrap for a casing surrounding rotating element of a core engine of a turbofan engine, has matrix that is configured receive mechanical fastener to stabilize graphene sheets and gap is provided between the abutted sheets.

GUIJARRO VALENCIA A, GUIJARRO V A, GUGARO V A

Component e.g. high temperature operating element such as turbine blade has graphene layer which is directly arranged on substrate made of nickel-or cobalt-based superalloy, and metallic protective layer is formed on substrate.

CLOSSENVON LANKEN SCHULZ M, KADAU K

Low pressure shovel for e.g. steam turbine in airplane engine, has blade root connected to shovel blade and closing shovel blade in extension that is in radial alignment regarding axis, where shovel is made of monocrystalline graphene.

HAJE D