with control of fuel supply

Industry

CPC
F02K1/17

This industry / category may be too specific. Please go to a parent level for more data

Parent Industries

FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F02Combustion engines F02KJET-PROPULSION PLANTS F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle Jet pipes or nozzles peculiar thereto

Current Industry

F02K1/17with control of fuel supply

Industries

Please log in for detailed analytics

Patents Grantslast 30 patents

Information Patent Grant
Variable displacement pumps
- Patent number 12,071,942
- Issue date Aug 27, 2024
- Hamilton Sundstrand Corporation
- Matej Rutar
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Fiber optic exit area sensing for gas turbine engine nozzles
- Patent number 11,421,607
- Issue date Aug 23, 2022
- Raytheon Technologies Corporation
- Jason J. Jackowski
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Control system
- Patent number 11,236,683
- Issue date Feb 1, 2022
- Rolls-Royce PLC
- Vasileios Kyritsis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method and system for limiting power of an engine
- Patent number 10,823,113
- Issue date Nov 3, 2020
- Pratt & Whitney Canada Corp.
- Sylvain Lamarre
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Control device of a variable section nozzle and the implementation...
- Patent number 10,787,995
- Issue date Sep 29, 2020
- SAFRAN AIRCRAFT ENGINES
- Pierre Caruel
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Optimal thrust control of an aircraft engine
- Patent number 10,711,734
- Issue date Jul 14, 2020
- Raytheon Technologies Corporation
- Chaohong Cai
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Optimal thrust control of an aircraft engine
- Patent number 10,253,725
- Issue date Apr 9, 2019
- United Technologies Corporation
- Chaohong Cai
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Control scheme using variable area turbine and exhaust nozzle to re...
- Patent number 9,822,731
- Issue date Nov 21, 2017
- United Technologies Corporation
- Daniel Bernard Kupratis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Device for controlling a variable section nozzle of an aircraft
- Patent number 9,488,131
- Issue date Nov 8, 2016
- Airbus Operations (S.A.S.)
- Guillaume Bulin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Fuel feed circuit with hydraulic actuator and fuel metering unit fo...
- Patent number 9,222,418
- Issue date Dec 29, 2015
- SNECMA
- Nicolas Alain Bader
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Method of controlling speed transients in a turbine engine
- Patent number 9,206,746
- Issue date Dec 8, 2015
- SNECMA
- Cedrik Djelassi
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Fladed supersonic missile turbojet
- Patent number 7,475,545
- Issue date Jan 13, 2009
- General Electric Company
- James Edward Johnson
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Supersonic missile turbojet engine
- Patent number 7,424,805
- Issue date Sep 16, 2008
- General Electric Company
- James Edward Johnson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
External system and method for rocket exhaust plume signature tailo...
- Patent number 6,655,124
- Issue date Dec 2, 2003
- Northrop Grumman Corporation
- Charles A. Vickery
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Device for economizing fuel supply in a fuel supply circuit
- Patent number 6,655,123
- Issue date Dec 2, 2003
- SNECMA Moteurs
- Marie-Trinité Rose Blot-Carretero
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine fuel control method
- Patent number 6,584,762
- Issue date Jul 1, 2003
- General Electric Company
- Barton Hunter Snow
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine fuel control system
- Patent number 6,487,847
- Issue date Dec 3, 2002
- General Electric Company
- Barton Hunter Snow
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Rapid response attitude control logic for shaft-driven lift fan STO...
- Patent number 6,270,037
- Issue date Aug 7, 2001
- United Technologies Corporation
- Richard A. Freese
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rapid thrust response control logic for shaft-driven lift fan STOVL...
- Patent number 6,269,627
- Issue date Aug 7, 2001
- United Technologies Corporation
- Richard A. Freese
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Pressure based close loop thrust control in a turbofan engine
- Patent number 5,303,545
- Issue date Apr 19, 1994
- United Technologies Corporation
- Louis J. Larkin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Sub-idle stability enhancement and rotating stall recovery
- Patent number 5,269,136
- Issue date Dec 14, 1993
- United Technologies Corporation
- Syed J. Khalid
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Control system and method for controlling a gas turbine engine
- Patent number 5,197,280
- Issue date Mar 30, 1993
- General Electric Company
- R. Sheldon Carpenter
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Control of low compressor vanes and fuel for a gas turbine engine
- Patent number 5,133,182
- Issue date Jul 28, 1992
- United Technologies Corporation
- Juan A. Marcos
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Active geometry control system for gas turbine engines
- Patent number 4,947,643
- Issue date Aug 14, 1990
- United Technologies Corporation
- Robert R. Pollak
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Control of high compressor vanes and fuel for a gas turbine engine
- Patent number 4,928,482
- Issue date May 29, 1990
- United Technologies Corporation
- Robert R. Pollak
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Transient control system for gas turbine engine
- Patent number 4,809,500
- Issue date Mar 7, 1989
- United Technologies Corporation
- William C. Roberts
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Device for controlling and regulating the cross section of a variab...
- Patent number 4,501,117
- Issue date Feb 26, 1985
- Societe Nationale d'Etude de Construction de Moteurs d'Aviation
- Guy M. C. Canivet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
System for controlling the thrust nozzle adjustment of dual cycle g...
- Patent number 4,489,550
- Issue date Dec 25, 1984
- Messerschmitt-Boelkow-Blohm Gesellschaft mit beschraenkter Haftung
- Juergen Peikert
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
System for controlling the thrust nozzle adjustment of dual cycle g...
- Patent number 4,467,600
- Issue date Aug 28, 1984
- Messerschmitt-Boelkow-Blohm GmbH
- Jurgen Peikert
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Method and apparatus for controlling a gas turbine engine
- Patent number 4,414,807
- Issue date Nov 15, 1983
- United Technologies Corporation
- Walter B. Kerr
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
Ramjet Engine with Rotating Detonation Combustion System and Method...
- Publication number 20200040843
- Publication date Feb 6, 2020
- GENERAL ELECTRIC COMPANY
- Sibtosh Pal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
OPTIMAL THRUST CONTROL OF AN AIRCRAFT ENGINE
- Publication number 20200025130
- Publication date Jan 23, 2020
- United Technologies Corporation
- Chaohong Cai
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD AND SYSTEM FOR LIMITING POWER OF AN ENGINE
- Publication number 20190055901
- Publication date Feb 21, 2019
- Pratt & Whitney Canada Corp.
- Sylvain LAMARRE
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
CONTROL DEVICE OF A VARIABLE SECTION NOZZLE AND THE IMPLEMENTATION...
- Publication number 20170276092
- Publication date Sep 28, 2017
- SAFRAN AIRCRAFT ENGINES
- Pierre CARUEL
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Optimal Thrust Control of an Aircraft Engine
- Publication number 20160138523
- Publication date May 19, 2016
- United Technologies Corporation
- Chaohong Cai
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Fast Response Bypass Engine
- Publication number 20140137538
- Publication date May 22, 2014
- United Technologies Corporation
- James W. Fuller
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEVICE FOR CONTROLLING A VARIABLE SECTION NOZZLE OF AN AIRCRAFT
- Publication number 20130269312
- Publication date Oct 17, 2013
- AIRBUS OPERATIONS (SAS)
- Guillaume BULIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD OF CONTROLLING SPEED TRANSIENTS IN A TURBINE ENGINE
- Publication number 20130008171
- Publication date Jan 10, 2013
- SNECMA
- Cedrik DJELASSI
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
FUEL FEED CIRCUIT FOR AN AEROENGINE
- Publication number 20120266600
- Publication date Oct 25, 2012
- SNECMA
- Nicolas Alain Bader
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEM AND METHOD FOR CONTROLLING A GAS TURBINE ENGINE AFTERBURNER
- Publication number 20120174559
- Publication date Jul 12, 2012
- Honeywell International Inc.
- Richard Ling
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Fladed supersonic missile turbojet
- Publication number 20060242941
- Publication date Nov 2, 2006
- General Electric Company
- James Edward Johnson
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
Supersonic missile turbojet engine
- Publication number 20060242943
- Publication date Nov 2, 2006
- General Electric Company
- James Edward Johnson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
External system and method for rocket exhaust plume signature tailo...
- Publication number 20030159427
- Publication date Aug 28, 2003
- Charles A. Vickery
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Gas turbine engine fuel control system and method
- Publication number 20030074884
- Publication date Apr 24, 2003
- Barton Hunter Snow
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Device and process for economizing fuel supply in a fuel supply cir...
- Publication number 20020050140
- Publication date May 2, 2002
- SNECMA MOTEURS
- Marie-Trinite Rose Blot-Carretero
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...

with control of fuel supply

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Variable displacement pumps

Fiber optic exit area sensing for gas turbine engine nozzles

Control system

Method and system for limiting power of an engine

Control device of a variable section nozzle and the implementation...

Optimal thrust control of an aircraft engine

Optimal thrust control of an aircraft engine

Control scheme using variable area turbine and exhaust nozzle to re...

Device for controlling a variable section nozzle of an aircraft

Fuel feed circuit with hydraulic actuator and fuel metering unit fo...

Method of controlling speed transients in a turbine engine

Fladed supersonic missile turbojet

Supersonic missile turbojet engine

External system and method for rocket exhaust plume signature tailo...

Device for economizing fuel supply in a fuel supply circuit

Gas turbine engine fuel control method

Gas turbine engine fuel control system

Rapid response attitude control logic for shaft-driven lift fan STO...

Rapid thrust response control logic for shaft-driven lift fan STOVL...

Pressure based close loop thrust control in a turbofan engine

Sub-idle stability enhancement and rotating stall recovery

Control system and method for controlling a gas turbine engine

Control of low compressor vanes and fuel for a gas turbine engine

Active geometry control system for gas turbine engines

Control of high compressor vanes and fuel for a gas turbine engine

Transient control system for gas turbine engine

Device for controlling and regulating the cross section of a variab...

System for controlling the thrust nozzle adjustment of dual cycle g...

System for controlling the thrust nozzle adjustment of dual cycle g...

Method and apparatus for controlling a gas turbine engine

Patents Applicationslast 30 patents

Ramjet Engine with Rotating Detonation Combustion System and Method...

OPTIMAL THRUST CONTROL OF AN AIRCRAFT ENGINE

METHOD AND SYSTEM FOR LIMITING POWER OF AN ENGINE

CONTROL DEVICE OF A VARIABLE SECTION NOZZLE AND THE IMPLEMENTATION...

Optimal Thrust Control of an Aircraft Engine

Fast Response Bypass Engine

DEVICE FOR CONTROLLING A VARIABLE SECTION NOZZLE OF AN AIRCRAFT

METHOD OF CONTROLLING SPEED TRANSIENTS IN A TURBINE ENGINE

FUEL FEED CIRCUIT FOR AN AEROENGINE

SYSTEM AND METHOD FOR CONTROLLING A GAS TURBINE ENGINE AFTERBURNER

Fladed supersonic missile turbojet

Supersonic missile turbojet engine

External system and method for rocket exhaust plume signature tailo...

Gas turbine engine fuel control system and method

Device and process for economizing fuel supply in a fuel supply cir...