by transversely deforming an internal member

Industry

CPC
F02K1/085

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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

F02K1/085by transversely deforming an internal member

Industries

Patents Grantslast 30 patents

Information Patent Grant
Internal structure of a primary exhaust duct having a separator of...
- Patent number 11,519,302
- Issue date Dec 6, 2022
- Airbus Operations SAS
- Sandrine Andre
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Ramjet engine with rotating detonation combustion system and method...
- Patent number 11,359,578
- Issue date Jun 14, 2022
- General Electric Company
- Sibtosh Pal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
Moveable exhaust plug liner
- Patent number 10,570,852
- Issue date Feb 25, 2020
- United Technologies Corporation
- Andre L. Bent
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine engines with variable area nozzle
- Patent number 10,550,797
- Issue date Feb 4, 2020
- MRA Systems, LLC
- Graham Frank Howarth
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Variable fan nozzle using shape memory material
- Patent number 10,371,001
- Issue date Aug 6, 2019
- United Technologies Corporation
- Constantine Baltas
- F03 - MACHINES OR ENGINES FOR LIQUIDS WIND, SPRING WEIGHT AND MISCELLANEOUS M...
Information Patent Grant
Variable area bypass nozzle
- Patent number 10,260,427
- Issue date Apr 16, 2019
- United Technologies Corporation
- John R. Buey
- Y10 - TECHNICAL SUBJECTS COVERED BY FORMER USPC
Information Patent Grant
Variable-section nozzle, and aircraft turbojet engine nacelle equip...
- Patent number 9,850,776
- Issue date Dec 26, 2017
- Aircelle
- Hervé Hurlin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Variable area nozzle for gas turbine engine
- Patent number 9,828,943
- Issue date Nov 28, 2017
- United Technologies Corporation
- Richard Alan Weiner
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Foldable guiding ventilator cover for an aircraft engine assembly
- Patent number 9,783,314
- Issue date Oct 10, 2017
- Airbus Operations SAS
- Olivier Pautis
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Inner structure for an aircraft nacelle
- Patent number 9,382,845
- Issue date Jul 5, 2016
- AIRCELLE
- Herve Hurlin
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Variable fan nozzle using shape memory material
- Patent number 9,328,695
- Issue date May 3, 2016
- United Technologies Corporation
- Constantine Baltas
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine with variable area fan nozzle bladder system
- Patent number 9,010,126
- Issue date Apr 21, 2015
- United Technologies Corporation
- Alfred M. Stern
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Temperature activatable actuator
- Patent number 8,931,269
- Issue date Jan 13, 2015
- Rolls-Royce PLC
- Christopher G. Bright
- F03 - MACHINES OR ENGINES FOR LIQUIDS WIND, SPRING WEIGHT AND MISCELLANEOUS M...
Information Patent Grant
Nacelle with an adaptable outlet section
- Patent number 8,875,518
- Issue date Nov 4, 2014
- Aircelle
- Thierry Jacques Albert Le Docte
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft gas turbine with variable bypass nozzle by deforming element
- Patent number 8,850,824
- Issue date Oct 7, 2014
- Rolls-Royce Deutschland Ltd & Co KG
- Predrag Todorovic
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine having core auxiliary duct passage
- Patent number 8,371,806
- Issue date Feb 12, 2013
- United Technologies Corporation
- Daniel B. Kupratis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Bladder type variable area fan nozzle
- Patent number 8,276,364
- Issue date Oct 2, 2012
- United Technologies Corporation
- Glenn Levasseur
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Continuously variable flow nozzle assembly
- Patent number 8,161,754
- Issue date Apr 24, 2012
- Rolls-Royce PLC
- Christopher Thomas John Sheaf
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Nozzle with yaw vectoring vane
- Patent number 8,020,367
- Issue date Sep 20, 2011
- General Electric Company
- Michael Jay Toffan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Central body for a turbojet exhaust channel, turbojet
- Patent number 7,886,543
- Issue date Feb 15, 2011
- SNECMA
- Thomas Alain Christian Vincent
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbofan engine nozzle assembly and method of operating same
- Patent number 7,726,116
- Issue date Jun 1, 2010
- General Electric Company
- Paul D. Kemper
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Variable area throat exhaust nozzle with vectorable sideways shifti...
- Patent number 7,096,662
- Issue date Aug 29, 2006
- General Electric Company
- Edward James Wehner
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Stowable mixer ejection nozzle
- Patent number 5,941,065
- Issue date Aug 24, 1999
- The Boeing Company
- Gary L. Lidstone
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Supersonic engine apparatus and method with ejector/suppressor
- Patent number 5,761,899
- Issue date Jun 9, 1998
- The Boeing Company
- Garry W. Klees
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Plug-type exhaust nozzle having a variable centerbody and translati...
- Patent number 4,802,629
- Issue date Feb 7, 1989
- The Boeing Company
- Garry W. Klees
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Two-dimensional nozzle
- Patent number 4,295,611
- Issue date Oct 20, 1981
- United Technologies Corporation
- Thomas A. Wynosky
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable area exhaust nozzle
- Patent number 4,241,876
- Issue date Dec 30, 1980
- General Motors Corporation
- George H. Pedersen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
3612402
- Patent number 3,612,402
- Issue date Oct 12, 1971
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
3433244
- Patent number 3,433,244
- Issue date Mar 18, 1969
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
VARIABLE THREE DIMENSIONAL CONVERGENT-DIVERGENT NOZZLE
- Publication number 20220120237
- Publication date Apr 21, 2022
- CFD Research Corporation
- Joseph Roger Herdy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
JET ENGINE WITH A RADIALLY VARIABLE WALL
- Publication number 20190376470
- Publication date Dec 12, 2019
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag TODOROVIC
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
FOLDABLE GUIDING VENTILATOR COVER FOR AN AIRCRAFT ENGINE ASSEMBLY
- Publication number 20160031563
- Publication date Feb 4, 2016
- Airbus Operations SAS
- Olivier Pautis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INNER STRUCTURE FOR AN AIRCRAFT NACELLE
- Publication number 20140140830
- Publication date May 22, 2014
- Herve Hurlin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE
- Publication number 20130121824
- Publication date May 16, 2013
- United Technologies Corporation
- Daniel B. Kupratis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Aircraft gas turbine with variable bypass nozzle
- Publication number 20130008147
- Publication date Jan 10, 2013
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag TODOROVIC
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TEMPERATURE ACTIVATABLE ACTUATOR
- Publication number 20120067042
- Publication date Mar 22, 2012
- Rolls-Royce plc
- Christopher G. Bright
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE
- Publication number 20120023961
- Publication date Feb 2, 2012
- Daniel B. Kupratis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
NACELLE WITH AN ADAPTABLE OUTLET SECTION
- Publication number 20110214747
- Publication date Sep 8, 2011
- Aircelle
- Thierry Jacques Albert Le Docte
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
BLADDER TYPE VARIABLE AREA FAN NOZZLE
- Publication number 20100139240
- Publication date Jun 10, 2010
- Glenn Levasseur
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
VARIABLE FAN NOZZLE USING SHAPE MEMORY MATERIAL
- Publication number 20100037588
- Publication date Feb 18, 2010
- Constantine Baltas
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE WITH VARIABLE AREA FAN NOZZLE BLADDER SYSTEM
- Publication number 20090208328
- Publication date Aug 20, 2009
- Alfred M. Stern
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE
- Publication number 20090092480
- Publication date Apr 9, 2009
- Daniel B. Kupratis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
NOZZLE WITH YAW VECTORING VANE
- Publication number 20090064660
- Publication date Mar 12, 2009
- Michael Jay Toffan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NOZZLE ASSEMBLY
- Publication number 20080166227
- Publication date Jul 10, 2008
- Rolls-Royce plc
- CHRISTOPHER THOMAS JOHN SHEAF
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOFAN ENGINE NOZZLE ASSEMBLY AND METHOD OF OPERATING SAME
- Publication number 20080110154
- Publication date May 15, 2008
- Paul D. Kemper
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
CENTRAL BODY FOR A TURBOJET EXHAUST CHANNEL, TURBOJET
- Publication number 20070272477
- Publication date Nov 29, 2007
- SNECMA
- Thomas Alain Christian VINCENT
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
VARIABLE AREA THROAT EXHAUST NOZZLE WITH VECTORABLE SIDEWAYS SHIFTI...
- Publication number 20060064962
- Publication date Mar 30, 2006
- Edward James Wehner
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

by transversely deforming an internal member

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Internal structure of a primary exhaust duct having a separator of...

Ramjet engine with rotating detonation combustion system and method...

High flow plug nozzle apparatus and method of using the same

Moveable exhaust plug liner

Turbine engines with variable area nozzle

Variable fan nozzle using shape memory material

Variable area bypass nozzle

Variable-section nozzle, and aircraft turbojet engine nacelle equip...

Variable area nozzle for gas turbine engine

Foldable guiding ventilator cover for an aircraft engine assembly

Inner structure for an aircraft nacelle

Variable fan nozzle using shape memory material

Gas turbine engine with variable area fan nozzle bladder system

Temperature activatable actuator

Nacelle with an adaptable outlet section

Aircraft gas turbine with variable bypass nozzle by deforming element

Gas turbine engine having core auxiliary duct passage

Bladder type variable area fan nozzle

Continuously variable flow nozzle assembly

Nozzle with yaw vectoring vane

Central body for a turbojet exhaust channel, turbojet

Turbofan engine nozzle assembly and method of operating same

Variable area throat exhaust nozzle with vectorable sideways shifti...

Stowable mixer ejection nozzle

Supersonic engine apparatus and method with ejector/suppressor

Plug-type exhaust nozzle having a variable centerbody and translati...

Two-dimensional nozzle

Variable area exhaust nozzle

3612402

3433244

Patents Applicationslast 30 patents

VARIABLE THREE DIMENSIONAL CONVERGENT-DIVERGENT NOZZLE

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

JET ENGINE WITH A RADIALLY VARIABLE WALL

FOLDABLE GUIDING VENTILATOR COVER FOR AN AIRCRAFT ENGINE ASSEMBLY

INNER STRUCTURE FOR AN AIRCRAFT NACELLE

GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE

Aircraft gas turbine with variable bypass nozzle

TEMPERATURE ACTIVATABLE ACTUATOR

GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE

NACELLE WITH AN ADAPTABLE OUTLET SECTION

BLADDER TYPE VARIABLE AREA FAN NOZZLE

VARIABLE FAN NOZZLE USING SHAPE MEMORY MATERIAL

GAS TURBINE ENGINE WITH VARIABLE AREA FAN NOZZLE BLADDER SYSTEM

GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE

NOZZLE WITH YAW VECTORING VANE

NOZZLE ASSEMBLY

TURBOFAN ENGINE NOZZLE ASSEMBLY AND METHOD OF OPERATING SAME

CENTRAL BODY FOR A TURBOJET EXHAUST CHANNEL, TURBOJET

VARIABLE AREA THROAT EXHAUST NOZZLE WITH VECTORABLE SIDEWAYS SHIFTI...