#F01K25/103

SUPERCRITICAL CARBON DIOXIDE-COOLED GENERATOR AND TURBINE

Power generation systems are described. The systems include a shaft (508, 608, 708), a compressor (202) operably coupled to a first end of the shaft (508, 608, 708), a turbine operably coupled to a se…

DRIVE·Jan 7·2 min read

F01K25/103 HAMILTON SUNDSTRAND CORP [US]

METHODS AND SYSTEMS FOR GENERATING POWER AND THERMAL MANAGEMENT HAVING DUAL LOOP ARCHITECTURE

Methods and apparatus for power generation and/or thermal management on a high speed flight vehicle (102) include circulating a power generation loop working fluid (122) through a power generation loo…

DRIVE·Jun 19·1 min read

F01K25/103 BOEING CO [US]

SUPERCRITICAL CO2 CYCLE FOR GAS TURBINE ENGINES USING PARTIAL CORE EXHAUST FLOW

A gas turbine engine (400) includes a compressor section, a combustor section, a turbine section, a nozzle section, and the compressor section, the combustor section, the turbine section, and the nozz…

DRIVE·Dec 27·1 min read

F01K25/103 RTX CORP [US]