About 12 results
https://drivepatents.com/patents/1393281 · 15 Apr 2026
A heat exchanger having: front and aft ends (110, 120); heat exchanger cores (130) in an annular loop (140) that define circumferential gaps (150) between adjacent pairs of the cores, the cores, individually or as axially aligned sets, extend from the fron...
https://drivepatents.com/patents/968733 · 15 Oct 2014
A method for regulating CO emissions of a gas turbine (1) with a compressor (4) and a turbine (8) is intended to permit comparatively lower power output of the gas turbine during part-load operation while maintaining compliant CO emissions. For this purpos...
https://drivepatents.com/patents/991185 · 1 May 2013
A thermal management system (100) for a gas turbine engine (20) includes a first heat exchanger (66) that provides a first conditioned fluid (83), a second heat exchanger (68) in series flow communication with the first heat exchanger (66) and that exchang...
https://drivepatents.com/patents/984960 · 24 Apr 2013
An integrated thermal system (80) for a gas turbine engine (20) includes an Air-Oil Cooler (88) and an Air-Air PreCooler (92) within a housing (89), the Air-Air PreCooler (92) being downstream of the Air-Oil Cooler (88).
https://drivepatents.com/patents/998877 · 29 Aug 2012
A gas turbine engine recuperator (30) including a plurality of independent arcuate segments (32), each segment having an inlet connection member (58) designed to sealingly engage a plenum (28) in fluid flow communication with the compressor discharge, and ...
https://drivepatents.com/patents/998878 · 29 Aug 2012
A gas turbine engine recuperator (30) includes exhaust passages (42) providing fluid flow communication between an exhaust inlet (50) and an exhaust outlet (52). The exhaust inlet (50) is oriented to receive exhaust flow from a turbine (18) of the engine (...
https://drivepatents.com/patents/998875 · 29 Aug 2012
A gas turbine engine recuperator (30) includes exhaust passages (42) providing fluid flow communication between an exhaust inlet (50) and an exhaust outlet (52). The exhaust inlet (50) is oriented to receive exhaust flow from a turbine (18) of the engine (...
https://drivepatents.com/patents/1070421 · 1 Feb 2006
A method for assembling a gas turbine engine includes fabricating a heat exchanger (50) that includes a first manifold (56) including an inlet and an outlet (72), a first quantity of heat exchanger elements (84) coupled in flow communication with the manif...
https://drivepatents.com/patents/1073051 · 26 Oct 2005
A method for assembling a gas turbine engine (10) including a compressor (14) and a combustor (18) includes providing a heat exchanger assembly that includes at least one heat exchanger (60), and coupling the heat exchanger assembly to the gas turbine engi...
https://drivepatents.com/patents/1089270 · 3 Mar 2004
A heat exchanger (100) for a turbine is provided wherein the heat exchanger (100) comprises a heat transfer cell (110) comprising a sheet of material (120) having two opposed ends (130, 135) and two opposed sides (140, 145). In addition, a plurality of con...