conjointly with another control

Industry

CPC
F02K1/16

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

F02K1/16conjointly with another control

Industries

Please log in for detailed analytics

Patents Grantslast 30 patents

Information Patent Grant
Propulsion system for an aircraft
- Patent number 11,686,246
- Issue date Jun 27, 2023
- Gulfstream Aerospace Corporation
- Shawn Bennett
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Supersonic air intake passage capable of achieving synchronous adju...
- Patent number 11,542,867
- Issue date Jan 3, 2023
- Nanjing University of Aeronautics and Astronautics
- Huijun Tan
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
Jet engine
- Patent number 10,975,775
- Issue date Apr 13, 2021
- IHI Corporation
- Takehiko Kimura
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
High flow plug nozzle apparatus and method of using the same
- Patent number 10,724,472
- Issue date Jul 28, 2020
- AERION INTELLECTUAL PROPERTY MANAGEMENT CORPORATION
- James D. Chase
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine with low fan noise
- Patent number 10,704,415
- Issue date Jul 7, 2020
- Raytheon Technologies Corporation
- Bruce L. Morin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine with low fan noise
- Patent number 10,526,914
- Issue date Jan 7, 2020
- United Technologies Corporation
- Bruce L. Morin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Telescoping electrical cable
- Patent number 10,422,301
- Issue date Sep 24, 2019
- The Boeing Company
- Kent Edmund Karnofski
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
High performance robust gas turbine exhaust with variable (adaptive...
- Patent number 10,329,945
- Issue date Jun 25, 2019
- SIEMENS ENERGY, INC.
- Anil L. Salunkhe
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft vapour trail control system
- Patent number 9,739,207
- Issue date Aug 22, 2017
- Rolls-Royce PLC
- Malcolm Hillel
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
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
Thrust reverser and variable area fan nozzle actuation system and m...
- Patent number 8,978,356
- Issue date Mar 17, 2015
- The Boeing Company
- Michael John Burgess
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Grant
Gas turbine engine having slim-line nacelle
- Patent number 8,844,294
- Issue date Sep 30, 2014
- United Technologies Corporation
- Stephen A. Morford
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Nozzle with an adjustable throat
- Patent number 8,769,959
- Issue date Jul 8, 2014
- Rolls-Royce Corporation
- Von David Baker
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine having slim-line nacelle
- Patent number 8,726,632
- Issue date May 20, 2014
- United Technologies Corporation
- Stephen A. Morford
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Operational line management of low pressure compressor in a turbofa...
- Patent number 8,601,786
- Issue date Dec 10, 2013
- United Technologies Corporation
- Wayne Hurwitz
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Hydraulic control system for a thrust reversal device
- Patent number 8,601,789
- Issue date Dec 10, 2013
- Aircelle
- Vincent Pierre Le Coq
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine with variable area fan nozzle positioned for sta...
- Patent number 8,596,072
- Issue date Dec 3, 2013
- United Technologies Corporation
- Eric J. Wehmeier
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Control system for turbojet engine nacelle
- Patent number 8,578,699
- Issue date Nov 12, 2013
- Aircelle
- Benoit Kubiak
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Noise reduction of supersonic jet engines
- Patent number 8,443,931
- Issue date May 21, 2013
- Lockheed Martin Corporation
- Anthony R. Pilon
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbofan engine operation control
- Patent number 8,365,513
- Issue date Feb 5, 2013
- United Technologies Corporation
- William J. McVey
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine having slim-line nacelle
- Patent number 8,353,164
- Issue date Jan 15, 2013
- United Technologies Corporation
- Stephen A. Morford
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Variable area nozzle assisted noise control of a gas turbine engine
- Patent number 8,313,285
- Issue date Nov 20, 2012
- United Technologies Corporation
- Wesley K. Lord
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Variable area fan nozzle for accommodating a foreign object strike...
- Patent number 8,308,423
- Issue date Nov 13, 2012
- United Technologies Corporation
- Andrew P. Berryann
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine with variable area fan nozzle positioned for sta...
- Patent number 8,291,690
- Issue date Oct 23, 2012
- United Technologies Corporation
- Eric J. Wehmeier
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Control systems and method for controlling a load point of a gas tu...
- Patent number 8,240,152
- Issue date Aug 14, 2012
- General Electric Company
- Constantin Dinu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Detecting ice buildup on an aircraft engine and actuating the turbo...
- Patent number 8,209,950
- Issue date Jul 3, 2012
- United Technologies Corporation
- Ashok K. Jain
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Control systems and method for controlling a load point of a gas tu...
- Patent number 8,127,557
- Issue date Mar 6, 2012
- General Electric Company
- Constantin Dinu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine with fan variable area nozzle having a rotationa...
- Patent number 7,966,827
- Issue date Jun 28, 2011
- United Technologies Corporation
- Eric W. Alletzhauser
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method and apparatus for an aerodynamic stability management system
- Patent number 7,827,803
- Issue date Nov 9, 2010
- General Electric Company
- Aspi Rustom Wadia
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
JET ENGINE
- Publication number 20170370295
- Publication date Dec 28, 2017
- IHI Corporation
- Takehiko KIMURA
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEVICE FOR CONTROLLING A NOZZLE OF VARIABLE CROSS-SECTION OF AN AIR...
- Publication number 20160006375
- Publication date Jan 7, 2016
- AIRBUS OPERATIONS (SAS)
- Guillaume BULIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE HAVING SLIM-LINE NACELLE
- Publication number 20140216002
- Publication date Aug 7, 2014
- United Technologies Corporation
- Stephen A. Morford
- 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
GAS TURBINE ENGINE WITH VARIABLE AREA FAN NOZZLE POSITIONED FOR STA...
- Publication number 20130213055
- Publication date Aug 22, 2013
- Eric J. Wehmeier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
HYDRAULIC CONTROL SYSTEM FOR A THRUST REVERSAL DEVICE
- Publication number 20130061572
- Publication date Mar 14, 2013
- Aircelle
- Vincent Pierre Germain LE COQ
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NOISE REDUCTION OF SUPERSONIC JET ENGINES
- Publication number 20120255806
- Publication date Oct 11, 2012
- Lockheed Martin Corporation
- Anthony R. Pilon
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
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
Thrust Reverser and Variable Area Fan Nozzle Actuation System and M...
- Publication number 20120137654
- Publication date Jun 7, 2012
- THE BOEING COMPANY
- Michael John Burgess
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Application
VARIABLE AREA FAN NOZZLE FAN FLUTTER MANAGEMENT SYSTEM
- Publication number 20120110980
- Publication date May 10, 2012
- Zbigniew M. Grabowski
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
Control Systems and Method for Controlling a Load Point of a Gas Tu...
- Publication number 20110308256
- Publication date Dec 22, 2011
- GENERAL ELECTRIC COMPANY
- Constantin Dinu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Control System
- Publication number 20110192135
- Publication date Aug 11, 2011
- Goodrich Actuation Systems Limited
- Richard John McKay
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CONTROL SYSTEMS AND METHOD FOR CONTROLLING A LOAD POINT OF A GAS T...
- Publication number 20110056181
- Publication date Mar 10, 2011
- GENERAL ELECTRIC COMPANY
- Constantin Dinu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
NOZZLE WITH AN ADJUSTABLE THROAT
- Publication number 20100327078
- Publication date Dec 30, 2010
- Von David Baker
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CONTROL SYSTEM FOR TURBOJET ENGINE NACELLE
- Publication number 20100313546
- Publication date Dec 16, 2010
- Aircelle
- Benoit Kubiak
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE HAVING SLIM-LINE NACELLE
- Publication number 20100269486
- Publication date Oct 28, 2010
- Stephen A. Morford
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE HAVING SLIM-LINE NACELLE
- Publication number 20100269512
- Publication date Oct 28, 2010
- Stephen A. Morford
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
OPERATIONAL LINE MANAGEMENT OF LOW PRESSURE COMPRESSOR IN A TURBOFA...
- Publication number 20100058735
- Publication date Mar 11, 2010
- Wayne Hurwitz
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
CONTROLLING ICE BUILDUP ON AIRCRAFT ENGINE AND NACELLE STATIC AND R...
- Publication number 20100043390
- Publication date Feb 25, 2010
- Ashok K. Jain
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBOFAN ENGINE OPERATION CONTROL
- Publication number 20100011740
- Publication date Jan 21, 2010
- UNITED TECHNOLOGIES CORORATION
- William J. McVey
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
VARIABLE AREA FAN NOZZLE FOR ACCOMMODATING A FOREIGN OBJECT STRIKE...
- Publication number 20100003121
- Publication date Jan 7, 2010
- Andrew P. Berryann
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
VARIABLE AREA NOZZLE ASSISTED NOISE CONTROL OF A GAS TURBINE ENGINE
- Publication number 20090297338
- Publication date Dec 3, 2009
- Wesley K. Lord
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
VARIABLE AREA FAN NOZZLE FAN FLUTTER MANAGEMENT SYSTEM
- Publication number 20090226303
- Publication date Sep 10, 2009
- Zbigniew M. Grabowski
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE HAVING A ROTATIONA...
- Publication number 20090064659
- Publication date Mar 12, 2009
- Eric W. Alletzhauser
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Gas turbine engine having slim-line nacelle
- Publication number 20080092548
- Publication date Apr 24, 2008
- United Technologies Corporation
- Stephen A. Morford
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Nozzle with an adjustable throat
- Publication number 20070256419
- Publication date Nov 8, 2007
- Rolls-Royce Corporation
- Von David Baker
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Thrust reverser for a jet engine and hydraulic actuator
- Publication number 20040068977
- Publication date Apr 15, 2004
- Richard John McKay
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...

conjointly with another control

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Propulsion system for an aircraft

Supersonic air intake passage capable of achieving synchronous adju...

Fiber optic exit area sensing for gas turbine engine nozzles

Jet engine

High flow plug nozzle apparatus and method of using the same

Gas turbine engine with low fan noise

Gas turbine engine with low fan noise

Telescoping electrical cable

High performance robust gas turbine exhaust with variable (adaptive...

Aircraft vapour trail control system

Device for controlling a variable section nozzle of an aircraft

Thrust reverser and variable area fan nozzle actuation system and m...

Gas turbine engine having slim-line nacelle

Nozzle with an adjustable throat

Gas turbine engine having slim-line nacelle

Operational line management of low pressure compressor in a turbofa...

Hydraulic control system for a thrust reversal device

Gas turbine engine with variable area fan nozzle positioned for sta...

Control system for turbojet engine nacelle

Noise reduction of supersonic jet engines

Turbofan engine operation control

Gas turbine engine having slim-line nacelle

Variable area nozzle assisted noise control of a gas turbine engine

Variable area fan nozzle for accommodating a foreign object strike...

Gas turbine engine with variable area fan nozzle positioned for sta...

Control systems and method for controlling a load point of a gas tu...

Detecting ice buildup on an aircraft engine and actuating the turbo...

Control systems and method for controlling a load point of a gas tu...

Gas turbine engine with fan variable area nozzle having a rotationa...

Method and apparatus for an aerodynamic stability management system

Patents Applicationslast 30 patents

JET ENGINE

DEVICE FOR CONTROLLING A NOZZLE OF VARIABLE CROSS-SECTION OF AN AIR...

GAS TURBINE ENGINE HAVING SLIM-LINE NACELLE

DEVICE FOR CONTROLLING A VARIABLE SECTION NOZZLE OF AN AIRCRAFT

GAS TURBINE ENGINE WITH VARIABLE AREA FAN NOZZLE POSITIONED FOR STA...

HYDRAULIC CONTROL SYSTEM FOR A THRUST REVERSAL DEVICE

NOISE REDUCTION OF SUPERSONIC JET ENGINES

SYSTEM AND METHOD FOR CONTROLLING A GAS TURBINE ENGINE AFTERBURNER

Thrust Reverser and Variable Area Fan Nozzle Actuation System and M...

VARIABLE AREA FAN NOZZLE FAN FLUTTER MANAGEMENT SYSTEM

Control Systems and Method for Controlling a Load Point of a Gas Tu...

Control System

CONTROL SYSTEMS AND METHOD FOR CONTROLLING A LOAD POINT OF A GAS T...

NOZZLE WITH AN ADJUSTABLE THROAT

CONTROL SYSTEM FOR TURBOJET ENGINE NACELLE

GAS TURBINE ENGINE HAVING SLIM-LINE NACELLE

GAS TURBINE ENGINE HAVING SLIM-LINE NACELLE

OPERATIONAL LINE MANAGEMENT OF LOW PRESSURE COMPRESSOR IN A TURBOFA...

CONTROLLING ICE BUILDUP ON AIRCRAFT ENGINE AND NACELLE STATIC AND R...

TURBOFAN ENGINE OPERATION CONTROL

VARIABLE AREA FAN NOZZLE FOR ACCOMMODATING A FOREIGN OBJECT STRIKE...

VARIABLE AREA NOZZLE ASSISTED NOISE CONTROL OF A GAS TURBINE ENGINE

VARIABLE AREA FAN NOZZLE FAN FLUTTER MANAGEMENT SYSTEM

GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE HAVING A ROTATIONA...

Gas turbine engine having slim-line nacelle

Nozzle with an adjustable throat

Thrust reverser for a jet engine and hydraulic actuator