the plant being of the multiple flow type

Industry

CPC
F02K3/077

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Parent Industries

FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F02Combustion engines F02KJET-PROPULSION PLANTS F02K3/00Plants including a gas turbine driving a compressor or a ducted fan

Current Industry

F02K3/077the plant being of the multiple flow type

Industries

Patents Grantslast 30 patents

Information Patent Grant
Turbomachinery engines with high-speed low-pressure turbines
- Patent number 12,012,901
- Issue date Jun 18, 2024
- General Electric Company
- Pranav R. Kamat
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Variable pitch fans for turbomachinery engines
- Patent number 11,946,437
- Issue date Apr 2, 2024
- General Electric Company
- Daniel A. Niergarth
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Aircraft propulsion assembly comprising two adjacent engines, of wh...
- Patent number 11,878,809
- Issue date Jan 23, 2024
- Airbus Operations S.A.S.
- Camil Negulescu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine with third stream
- Patent number 11,859,516
- Issue date Jan 2, 2024
- General Electric Company
- David Marion Ostdiek
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Splitter and guide vane arrangement for gas turbine engines
- Patent number 11,781,506
- Issue date Oct 10, 2023
- RTX Corporation
- Daniel Bernard Kupratis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Boost spool flow control and generator load matching via load compr...
- Patent number 11,639,690
- Issue date May 2, 2023
- Raytheon Technologies Corporation
- Daniel B. Kupratis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Triple flow aircraft turbomachine provided with a power transmissio...
- Patent number 11,555,454
- Issue date Jan 17, 2023
- SAFRAN TRANSMISSION SYSTEMS
- Guillaume Pierre Mouly
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Anti-unstart for combined cycle high mach vehicles
- Patent number 11,512,667
- Issue date Nov 29, 2022
- Rolls-Royce North American Technologies Inc.
- Kaare P. Erickson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Double flow turbojet including an intermediate flow path dedicated...
- Patent number 11,499,439
- Issue date Nov 15, 2022
- SAFRAN AIRCRAFT ENGINES
- Antoine Jean-Philippe Beaujard
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine with third stream
- Patent number 11,492,918
- Issue date Nov 8, 2022
- General Electric Company
- David Marion Ostdiek
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable pitch fans for turbomachinery engines
- Patent number 11,454,195
- Issue date Sep 27, 2022
- General Electric Company
- Daniel A. Niergarth
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turboshaft engine with axial compressor
- Patent number 11,408,343
- Issue date Aug 9, 2022
- Raytheon Technologies Corporation
- Paul R. Hanrahan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Inlet guide vane draw heat exchanger system
- Patent number 11,300,049
- Issue date Apr 12, 2022
- Rolls-Royce North American Technologies Inc.
- Douglas David Dierksmeier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
External core gas turbine engine assembly
- Patent number 11,286,885
- Issue date Mar 29, 2022
- Raytheon Technologies Corporation
- William G. Sheridan
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Auxiliary device for three air flow path gas turbine engine
- Patent number 11,261,827
- Issue date Mar 1, 2022
- Raytheon Technologies Corporation
- Gary D. Roberge
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbomachine having inner and outer fans with hub-tip ratios
- Patent number 11,247,780
- Issue date Feb 15, 2022
- Rolls-Royce PLC
- Giles E Harvey
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine and an airflow control system
- Patent number 11,236,639
- Issue date Feb 1, 2022
- Raytheon Technologies Corporation
- Christopher J. Hanlon
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Convergent divergent exit nozzle for a gas turbine engine
- Patent number 11,236,701
- Issue date Feb 1, 2022
- Raytheon Technologies Corporation
- Dmitriy B. Sidelkovskiy
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Lobed gas discharge fairing for a turbofan engine
- Patent number 11,199,134
- Issue date Dec 14, 2021
- Ford Global Technologies, LLC
- Edward Nicholas Shipley
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Heat exchange module for a turbine engine
- Patent number 11,149,644
- Issue date Oct 19, 2021
- Raytheon Technologies Corporation
- Frederick M. Schwarz
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Grant
Adaptive engine with boost spool
- Patent number 11,143,142
- Issue date Oct 12, 2021
- United Technologies Corporation
- Paul R. Hanrahan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Intercooled cooling air heat exchanger arrangement
- Patent number 11,073,085
- Issue date Jul 27, 2021
- Raytheon Technologies Corporation
- Joseph B. Staubach
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Aircraft with multiple fan propulsion assembly fixed under the wing
- Patent number 11,059,597
- Issue date Jul 13, 2021
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert Beutin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Translating outer cowl flow modulation device and method
- Patent number 10,975,804
- Issue date Apr 13, 2021
- Raytheon Technologies Corporation
- John R. Buey
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Involute trapped vortex combustor assembly
- Patent number 10,976,053
- Issue date Apr 13, 2021
- General Electric Company
- Gregory Allen Boardman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Internal mixing of a portion of fan exhaust flow and full core exha...
- Patent number 10,954,890
- Issue date Mar 23, 2021
- The Boeing Company
- Matthew D. Moore
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Nacelle-integrated air-driven augmentor fan for increasing propulso...
- Patent number 10,907,578
- Issue date Feb 2, 2021
- The Boeing Company
- Mithra M. K. V. Sankrithi
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Aircraft with a propulsion unit with offset fan
- Patent number 10,850,859
- Issue date Dec 1, 2020
- SAFRAN AIRCRAFT ENGINES
- Kevin Morgane Lemarchand
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine with distributed fans
- Patent number 10,837,359
- Issue date Nov 17, 2020
- Raytheon Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Multi-bypass stream gas turbine engine with enlarged bypass flow area
- Patent number 10,823,086
- Issue date Nov 3, 2020
- Raytheon Technologies Corporation
- Michael R. Thomas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
SPLITTER AND GUIDE VANE ARRANGEMENT FOR GAS TURBINE ENGINES
- Publication number 20230407817
- Publication date Dec 21, 2023
- RTX Corporation
- Daniel Bernard Kupratis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH THIRD STREAM
- Publication number 20230076976
- Publication date Mar 9, 2023
- GENERAL ELECTRIC COMPANY
- David Marion Ostdiek
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
THREE-STREAM GAS TURBINE ENGINE WITH EMBEDDED ELECTRIC MACHINE
- Publication number 20220333553
- Publication date Oct 20, 2022
- GENERAL ELECTRIC COMPANY
- Darek Tomasz Zatorski
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TRIPLE FLOW AIRCRAFT TURBOMACHINE PROVIDED WITH A POWER TRANSMISSIO...
- Publication number 20220235710
- Publication date Jul 28, 2022
- SAFRAN TRANSMISSIONS SYTEMS
- Guillaume Pierre MOULY
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBINE ENGINE WITH STRUTS
- Publication number 20220106907
- Publication date Apr 7, 2022
- GENERAL ELECTRIC COMPANY
- William Joseph Bowden
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
METHOD FOR CONSTRUCTING ENGINES OR MOTORS CONTAINED IN A CYLINDRICA...
- Publication number 20200325779
- Publication date Oct 15, 2020
- CARPYZ SAS
- Pierre CARROUSET
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ANTI-UNSTART FOR COMBINED CYCLE HIGH MACH VEHICLES
- Publication number 20200271074
- Publication date Aug 27, 2020
- Rolls-Royce North American Technologies Inc.
- Kaare P. Erickson
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
AUXILIARY DEVICE FOR THREE AIR FLOW PATH GAS TURBINE ENGINE
- Publication number 20200102913
- Publication date Apr 2, 2020
- United Technologies Corporation
- Gary D. Roberge
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ADAPTIVE ENGINE WITH BOOST SPOOL
- Publication number 20200040848
- Publication date Feb 6, 2020
- United Technologies Corporation
- Paul R. Hanrahan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
MULTI-BYPASS STREAM GAS TURBINE ENGINE WITH ENLARGED BYPASS FLOW AREA
- Publication number 20200025104
- Publication date Jan 23, 2020
- United Technologies Corporation
- Michael R. Thomas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TRANSLATING OUTER COWL FLOW MODULATION DEVICE AND METHOD
- Publication number 20200025148
- Publication date Jan 23, 2020
- United Technologies Corporation
- John R. Buey
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE-INTEGRATED AIR-DRIVEN AUGMENTOR FAN FOR INCREASING PROPULSO...
- Publication number 20200025146
- Publication date Jan 23, 2020
- The Boeing Company
- Mithra M.K.V. Sankrithi
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
VARIABLE AREA EXHAUST MIXER FOR A GAS TURBINE ENGINE
- Publication number 20190316544
- Publication date Oct 17, 2019
- Jeffery A. Lovett
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
HEAT EXCHANGE MODULE FOR A TURBINE ENGINE
- Publication number 20190218973
- Publication date Jul 18, 2019
- United Technologies Corporation
- Frederick M. Schwarz
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Application
INVOLUTE TRAPPED VORTEX COMBUSTOR ASSEMBLY
- Publication number 20190120493
- Publication date Apr 25, 2019
- GENERAL ELECTRIC COMPANY
- Gregory Allen Boardman
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
GAS TURBINE ENGINE WITH SELECTIVE FLOW PATH
- Publication number 20190113234
- Publication date Apr 18, 2019
- United Technologies Corporation
- Steven M. O'Flarity
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBINE ENGINE WITH STRUTS
- Publication number 20190107046
- Publication date Apr 11, 2019
- GENERAL ELECTRIC COMPANY
- William Joseph Bowden
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
CONVERGENT DIVERGENT EXIT NOZZLE FOR A GAS TURBINE ENGINE
- Publication number 20190017470
- Publication date Jan 17, 2019
- United Technologies Corporation
- Dmitriy B. Sidelkovskiy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INTERNAL MIXING OF A PORTION OF FAN EXHAUST FLOW AND FULL CORE EXHA...
- Publication number 20190010895
- Publication date Jan 10, 2019
- The Boeing Company
- Matthew D. MOORE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ANNULAR AIRFLOW ACTUATION SYSTEM FOR VARIABLE CYCLE GAS TURBINE ENG...
- Publication number 20180306123
- Publication date Oct 25, 2018
- United Technologies Corporation
- Felix Izquierdo
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIRCRAFT WITH MULTIPLE FAN PROPULSION ASSEMBLY FIXED UNDER THE WING
- Publication number 20180281978
- Publication date Oct 4, 2018
- SAFRAN AIRCRAFT ENGINES
- Bruno Albert BEUTIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ENGINE DRIVEN BY SC02 CYCLE WITH INDEPENDENT SHAFTS FOR COMBUSTION...
- Publication number 20180238269
- Publication date Aug 23, 2018
- Rolls-Royce North American Technologies, Inc.
- Michael J Armstrong
- F22 - STEAM GENERATION
Information Patent Application
FLOW PATH ROUTING WITHIN A GAS TURBINE ENGINE
- Publication number 20180195463
- Publication date Jul 12, 2018
- United Technologies Corporation
- Gary D. Roberge
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE
- Publication number 20180149115
- Publication date May 31, 2018
- Rolls-Royce plc
- Ahmed M Y RAZAK
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH DISTRIBUTED FANS
- Publication number 20170306842
- Publication date Oct 26, 2017
- United Technologies Corporation
- Gabriel L. Suciu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE-INTEGRATED AIR-DRIVEN AUGMENTOR FAN FOR INCREASING PROPULSO...
- Publication number 20170122257
- Publication date May 4, 2017
- The Boeing Company
- Mithra M.K.V. Sankrithi
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE DRIVEN BY SCO2 CYCLE WITH ADVANCED HEAT REJECTION
- Publication number 20170058834
- Publication date Mar 2, 2017
- Rolls-Royce Corporation
- Igor Vaisman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ADAPTIVE AIRCRAFT ENGINE AND AIRCRAFT HAVING AN ADAPTIVE ENGINE
- Publication number 20160347463
- Publication date Dec 1, 2016
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Dimitrie NEGULESCU
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
THREE-STREAM GAS TURBINE ENGINE ARCHITECTURE
- Publication number 20160312740
- Publication date Oct 27, 2016
- United Technologies Corporation
- Daniel Bernard Kupratis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINES WITH INTERCOOLERS AND RECUPERATORS
- Publication number 20160305324
- Publication date Oct 20, 2016
- United Technologies Corporation
- John W. Magowan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

the plant being of the multiple flow type

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Turbomachinery engines with high-speed low-pressure turbines

Variable pitch fans for turbomachinery engines

Aircraft propulsion assembly comprising two adjacent engines, of wh...

Gas turbine engine with third stream

Splitter and guide vane arrangement for gas turbine engines

Boost spool flow control and generator load matching via load compr...

Triple flow aircraft turbomachine provided with a power transmissio...

Anti-unstart for combined cycle high mach vehicles

Double flow turbojet including an intermediate flow path dedicated...

Gas turbine engine with third stream

Variable pitch fans for turbomachinery engines

Turboshaft engine with axial compressor

Inlet guide vane draw heat exchanger system

External core gas turbine engine assembly

Auxiliary device for three air flow path gas turbine engine

Turbomachine having inner and outer fans with hub-tip ratios

Gas turbine engine and an airflow control system

Convergent divergent exit nozzle for a gas turbine engine

Lobed gas discharge fairing for a turbofan engine

Heat exchange module for a turbine engine

Adaptive engine with boost spool

Intercooled cooling air heat exchanger arrangement

Aircraft with multiple fan propulsion assembly fixed under the wing

Translating outer cowl flow modulation device and method

Involute trapped vortex combustor assembly

Internal mixing of a portion of fan exhaust flow and full core exha...

Nacelle-integrated air-driven augmentor fan for increasing propulso...

Aircraft with a propulsion unit with offset fan

Gas turbine engine with distributed fans

Multi-bypass stream gas turbine engine with enlarged bypass flow area

Patents Applicationslast 30 patents

SPLITTER AND GUIDE VANE ARRANGEMENT FOR GAS TURBINE ENGINES

GAS TURBINE ENGINE WITH THIRD STREAM

THREE-STREAM GAS TURBINE ENGINE WITH EMBEDDED ELECTRIC MACHINE

TRIPLE FLOW AIRCRAFT TURBOMACHINE PROVIDED WITH A POWER TRANSMISSIO...

TURBINE ENGINE WITH STRUTS

METHOD FOR CONSTRUCTING ENGINES OR MOTORS CONTAINED IN A CYLINDRICA...

ANTI-UNSTART FOR COMBINED CYCLE HIGH MACH VEHICLES

AUXILIARY DEVICE FOR THREE AIR FLOW PATH GAS TURBINE ENGINE

ADAPTIVE ENGINE WITH BOOST SPOOL

MULTI-BYPASS STREAM GAS TURBINE ENGINE WITH ENLARGED BYPASS FLOW AREA

TRANSLATING OUTER COWL FLOW MODULATION DEVICE AND METHOD

NACELLE-INTEGRATED AIR-DRIVEN AUGMENTOR FAN FOR INCREASING PROPULSO...

VARIABLE AREA EXHAUST MIXER FOR A GAS TURBINE ENGINE

HEAT EXCHANGE MODULE FOR A TURBINE ENGINE

INVOLUTE TRAPPED VORTEX COMBUSTOR ASSEMBLY

GAS TURBINE ENGINE WITH SELECTIVE FLOW PATH

TURBINE ENGINE WITH STRUTS

CONVERGENT DIVERGENT EXIT NOZZLE FOR A GAS TURBINE ENGINE

INTERNAL MIXING OF A PORTION OF FAN EXHAUST FLOW AND FULL CORE EXHA...

ANNULAR AIRFLOW ACTUATION SYSTEM FOR VARIABLE CYCLE GAS TURBINE ENG...

AIRCRAFT WITH MULTIPLE FAN PROPULSION ASSEMBLY FIXED UNDER THE WING

ENGINE DRIVEN BY SC02 CYCLE WITH INDEPENDENT SHAFTS FOR COMBUSTION...

FLOW PATH ROUTING WITHIN A GAS TURBINE ENGINE

GAS TURBINE ENGINE

GAS TURBINE ENGINE WITH DISTRIBUTED FANS

NACELLE-INTEGRATED AIR-DRIVEN AUGMENTOR FAN FOR INCREASING PROPULSO...

GAS TURBINE ENGINE DRIVEN BY SCO2 CYCLE WITH ADVANCED HEAT REJECTION

ADAPTIVE AIRCRAFT ENGINE AND AIRCRAFT HAVING AN ADAPTIVE ENGINE

THREE-STREAM GAS TURBINE ENGINE ARCHITECTURE

GAS TURBINE ENGINES WITH INTERCOOLERS AND RECUPERATORS