A clearance reducing system for turbomachinery is provided. In one embodiment, a
turbomachinery apparatus having a shaft rotatable about an axis, with an impeller coupled …

(57) ABSTRACT A gas turbine engine includes a circumferential row of blades, with the
blades having respective blade tips. A seal is disposed about the blades. The seal has an …

A gas turbine engine includes an inlet duct, a compressor section, a combustor section, and
a turbine section connected to drive the compressor section. The compressor section …

US20220259700A1 - Max phase-gold composites and methods for making the same - Google
Patents US20220259700A1 - Max phase-gold composites and methods for making the same …

A fan motor according to an embodiment of the present invention may include: an impeller a
hub connected to a rotary shaft and at least one blade formed on the outer surface of the …

A method of manufacturing a gas turbine engine air seal comprising forming at least one
MAX phase particle. The method includes coating the at least one MAX phase particle with a …

An object is to provide a method of manufacturing a supercharger that can promptly and
easily form an abradable layer in a supercharger. A method of manufacturing a …

A fan motor according to an embodiment of the present invention may include: an impeller a
hub connected to a rotary shaft and at least one blade formed on the outer surface of the …

A gas turbine engine includes a circumferential row of blades, with the blades having
respective blade tips. A seal is disposed about the blades. The seal has an abradable layer …

The present disclosure relates to a gas turbine part, which can be exposed to high
temperatures and centrifugal forces within a gas turbine. The gas turbine part can include …