of one series of flaps hinged at their upstream ends on a substantially axially movable structure

Industry

CPC
F02K1/1261

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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

F02K1/1261of one series of flaps hinged at their upstream ends on a substantially axially movable structure

Industries

Patents Grantslast 30 patents

Information Patent Grant
Aircraft with electric propulsor
- Patent number 11,338,926
- Issue date May 24, 2022
- Rolls-Royce North American Technologies Inc.
- Douglas D. Dierksmeier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Nacelle for an aircraft engine with variable section nozzle
- Patent number 10,619,598
- Issue date Apr 14, 2020
- Aircelle
- Peter Segat
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Fan variable area nozzle for a gas turbine engine fan nacelle with...
- Patent number 10,519,898
- Issue date Dec 31, 2019
- United Technologies Corporation
- Robert L. Gukeisen
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Thrust reverser for a nacelle of an aircraft turbojet engine
- Patent number 10,458,363
- Issue date Oct 29, 2019
- SAFRAN NACELLES
- Pierre Moradell-Casellas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Pivot door thrust reverser with variable area nozzle
- Patent number 10,400,621
- Issue date Sep 3, 2019
- United Technologies Corporation
- Nigel David Sawyers-Abbott
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Thrust vectoring nozzle
- Patent number 10,385,805
- Issue date Aug 20, 2019
- Rolls-Royce PLC
- Jack F Colebrooke
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
System for actuating an exhaust cowl
- Patent number 10,371,089
- Issue date Aug 6, 2019
- United Technologies Corporation
- Donald W. Peters
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Nacelle for a turbojet engine with a variable nozzle
- Patent number 10,125,721
- Issue date Nov 13, 2018
- Aircelle
- Olivier Kerbler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Nacelle for an aircraft turbojet engine comprising a secondary nozz...
- Patent number 10,100,780
- Issue date Oct 16, 2018
- SAFRAN NACELLES
- Sarah Tissot
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Dual panel actuator system for jet engines
- Patent number 10,040,563
- Issue date Aug 7, 2018
- Geoffrey P. Pinto
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Thrust reverser for an aircraft turbojet engine nacelle
- Patent number 10,001,081
- Issue date Jun 19, 2018
- SAFRAN NACELLES
- Mathieu Lerouvreur
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Thrust reverser for nacelle of aircraft turbofan
- Patent number 9,995,246
- Issue date Jun 12, 2018
- SAFRAN NACELLES
- Patrick Gonidec
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
Axially translating and radially tilting fan nozzle segments with c...
- Patent number 9,803,585
- Issue date Oct 31, 2017
- Geoffrey P. Pinto
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Bent connecting rod fitted with at least one self-aligning means
- Patent number 9,212,689
- Issue date Dec 15, 2015
- Aircelle
- Guy Bernard Vauchel
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
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
Aeroengine nozzle
- Patent number 8,235,646
- Issue date Aug 7, 2012
- Rolls-Royce PLC
- Brian R. Lace
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust vectoring and variable exhaust area for jet engine nozzle
- Patent number 6,938,408
- Issue date Sep 6, 2005
- Propulsion Vectoring, L.P.
- Jean-Pierre Lair
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Sliding throat gas turbine engine nozzle
- Patent number 5,431,344
- Issue date Jul 11, 1995
- United Technologies Corporation
- Rudolph J. Novotny
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable area nozzle for turbomachines
- Patent number 5,273,213
- Issue date Dec 28, 1993
- Rolls-Royce Limited
- William J. Lewis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Sync-ring assembly for a gas turbine engine exhaust nozzle
- Patent number 5,239,815
- Issue date Aug 31, 1993
- United Technologies Corporation
- William K. Barcza
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine nozzle
- Patent number 5,110,050
- Issue date May 5, 1992
- Rolls Royce (1971) Limited
- Douglas J. Nightingale
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Vectorable variable flow area propulsion nozzle
- Patent number 4,984,741
- Issue date Jan 15, 1991
- Rolls-Royce Inc.
- Douglas J. Nightingale
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine powerplant with flow control devices
- Patent number 4,716,724
- Issue date Jan 5, 1988
- Rolls-Royce plc
- Arnold C. Newton
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable configuration exhaust discharge opening for a jet propulsi...
- Patent number 4,638,946
- Issue date Jan 27, 1987
- Rolls-Royce Limited
- John M. Hall
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
Nozzles for gas turbine engines
- Patent number 4,141,501
- Issue date Feb 27, 1979
- Rolls Royce (1971) Limited
- Douglas J. Nightingale
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Nozzles for gas turbine engines
- Patent number 4,049,199
- Issue date Sep 20, 1977
- Rolls-Royce (1971) Limited
- Douglas John Nightingale
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
In-flight modulating thrust reverser
- Patent number 3,981,450
- Issue date Sep 21, 1976
- The United States of America as represented by the Secretary of the Air Force
- Arthur McCardle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
3837577
- Patent number 3,837,577
- Issue date Sep 24, 1974
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
AIRCRAFT WITH ELECTRIC PROPULSOR
- Publication number 20200047896
- Publication date Feb 13, 2020
- Rolls-Royce North American Technologies Inc.
- Douglas D. Dierksmeier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
THRUST VECTORING NOZZLE
- Publication number 20180119641
- Publication date May 3, 2018
- Rolls-Royce plc
- Jack F. COLEBROOKE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
THRUST REVERSER FOR AN AIRCRAFT TURBOJET ENGINE NACELLE
- Publication number 20180112626
- Publication date Apr 26, 2018
- SAFRAN NACELLES
- Mathieu LEROUVREUR
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
THRUST REVERSER FOR A NACELLE OF AN AIRCRAFT TURBOJET ENGINE
- Publication number 20180080409
- Publication date Mar 22, 2018
- SAFRAN NACELLES
- Pierre MORADELL-CASELLAS
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
THRUST REVERSER FOR NACELLE OF AIRCRAFT TURBOFAN
- Publication number 20170328305
- Publication date Nov 16, 2017
- SAFRAN NACELLES
- Patrick GONIDEC
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE FOR A TURBOJET ENGINE WITH A VARIABLE NOZZLE
- Publication number 20160115902
- Publication date Apr 28, 2016
- Aircelle
- Olivier KERBLER
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Fan Variable Area Nozzle for a Gas Turbine Engine Fan Nacelle With...
- Publication number 20150361919
- Publication date Dec 17, 2015
- United Technologies Corporation
- Robert L. Gukeisen
- 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
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
BENT CONNECTING ROD FITTED WITH AT LEAST ONE SELF-ALIGNING MEANS
- Publication number 20120006000
- Publication date Jan 12, 2012
- Aircelle
- Guy Bernard Vauchel
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
BYPASS TURBOJET ENGINE NACELLE
- Publication number 20110030338
- Publication date Feb 10, 2011
- Aircelle
- Guy Bernard Vauchel
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
FAN VARIABLE AREA NOZZLE FOR A GAS TURBINE ENGINE FAN NACELLE WITH...
- Publication number 20090266912
- Publication date Oct 29, 2009
- Robert L. Gukeisen
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
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
Aeroengine nozzle
- Publication number 20080069687
- Publication date Mar 20, 2008
- Rolls-Royce plc
- Brian R. Lace
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Thrust vectoring and variable exhaust area for jet engine nozzle
- Publication number 20030159430
- Publication date Aug 28, 2003
- Jean-Pierre Lair
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

of one series of flaps hinged at their upstream ends on a substantially axially movable structure

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Aircraft with electric propulsor

Nacelle for an aircraft engine with variable section nozzle

Fan variable area nozzle for a gas turbine engine fan nacelle with...

Thrust reverser for a nacelle of an aircraft turbojet engine

Pivot door thrust reverser with variable area nozzle

Thrust vectoring nozzle

System for actuating an exhaust cowl

Nacelle for a turbojet engine with a variable nozzle

Nacelle for an aircraft turbojet engine comprising a secondary nozz...

Dual panel actuator system for jet engines

Thrust reverser for an aircraft turbojet engine nacelle

Thrust reverser for nacelle of aircraft turbofan

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

Axially translating and radially tilting fan nozzle segments with c...

Bent connecting rod fitted with at least one self-aligning means

Gas turbine engine having core auxiliary duct passage

Aeroengine nozzle

Thrust vectoring and variable exhaust area for jet engine nozzle

Sliding throat gas turbine engine nozzle

Variable area nozzle for turbomachines

Sync-ring assembly for a gas turbine engine exhaust nozzle

Gas turbine engine nozzle

Vectorable variable flow area propulsion nozzle

Gas turbine engine powerplant with flow control devices

Variable configuration exhaust discharge opening for a jet propulsi...

Two-dimensional nozzle

Nozzles for gas turbine engines

Nozzles for gas turbine engines

In-flight modulating thrust reverser

3837577

Patents Applicationslast 30 patents

AIRCRAFT WITH ELECTRIC PROPULSOR

THRUST VECTORING NOZZLE

THRUST REVERSER FOR AN AIRCRAFT TURBOJET ENGINE NACELLE

THRUST REVERSER FOR A NACELLE OF AN AIRCRAFT TURBOJET ENGINE

THRUST REVERSER FOR NACELLE OF AIRCRAFT TURBOFAN

NACELLE FOR A TURBOJET ENGINE WITH A VARIABLE NOZZLE

Fan Variable Area Nozzle for a Gas Turbine Engine Fan Nacelle With...

GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE

GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE

BENT CONNECTING ROD FITTED WITH AT LEAST ONE SELF-ALIGNING MEANS

BYPASS TURBOJET ENGINE NACELLE

FAN VARIABLE AREA NOZZLE FOR A GAS TURBINE ENGINE FAN NACELLE WITH...

GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE

Aeroengine nozzle

Thrust vectoring and variable exhaust area for jet engine nozzle