F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 3/04 (2006.01) F01D 13/02 (2006.01) F02C 7/12 (2006.01)
Patent
CA 2453634
A device and method for recuperating a gas turbine engine comprises a compressor [10] being configured to receive a coolant fluid stream, to compress the coolant fluid stream and to discharge the compressed coolant fluid stream to a turbine [14] in fluid communication with the compressor [10]. The compressed coolant fluid stream undergoing thermal exchange within the turbine [14], exit the turbine [14] thereafter. A source of a working fluid stream [44] is in fluid communication with the turbine [14]. The working fluid stream [44] is fluidly isolated from a portion of the coolant fluid stream and undergoing thermodynamic expansion through the turbine [14] to extract energy therefrom. Where desired, the entire coolant fluid stream is fluidly isolated from the working fluid stream [44]. At least a portion of the coolant fluid stream is channeled downstream of the turbine [14] to supply a preheated process fluid stream to another process.
Balan Chellappa
Bunker Ronald Scott
Company General Electric
Craig Wilson And Company
LandOfFree
Turbo recuperator device does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Turbo recuperator device, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbo recuperator device will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1881664