by means of pivoted eyelids

Industry

CPC
F02K1/11

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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

F02K1/11by means of pivoted eyelids

Industries

Patents Grantslast 30 patents

Information Patent Grant
Variable area nozzle for aircraft propulsion system
- Patent number 12,031,445
- Issue date Jul 9, 2024
- Rohr, Inc.
- Ann Khidekel
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
System for actuating a panel of a turbojet engine nacelle
- Patent number 10,774,786
- Issue date Sep 15, 2020
- SAFRAN NACELLES
- Patrick Gonidec
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
Thrust reverse variable area fan nozzle
- Patent number 10,001,080
- Issue date Jun 19, 2018
- The Boeing Company
- David F. Cerra
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
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
Rocket turbopump valves and associated systems and methods
- Patent number 9,217,389
- Issue date Dec 22, 2015
- Blue Origin, LLC
- Gerald A. Lee
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Integrated variable area nozzle and thrust reversing mechanism
- Patent number 8,720,182
- Issue date May 13, 2014
- United Technologies Corporation
- Ashok K. Jain
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust reverser
- Patent number 8,051,639
- Issue date Nov 8, 2011
- The NORDAM Group, INC.
- Jean-Pierre Lair
- 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
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
Vectorable variable area nozzle
- Patent number 6,910,328
- Issue date Jun 28, 2005
- Rolls-Royce PLC
- Nicolas J. Joyce
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Jet engine nozzle with variable thrust vectoring and exhaust area
- Patent number 6,546,716
- Issue date Apr 15, 2003
- Jean-Pierre Lair
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Engine nozzle arrangement for an aircraft
- Patent number 6,381,950
- Issue date May 7, 2002
- Bae Systems plc
- Colin Whaites
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turbojet engine thrust reverser and exhaust nozzle
- Patent number 6,289,670
- Issue date Sep 18, 2001
- SNECMA Moteurs
- Gilles Alain Charier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbo jet engine exhaust nozzle with masked gas jet
- Patent number 6,179,225
- Issue date Jan 30, 2001
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation “SNECMA”
- Philippe Pierre Bouiller
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Converging exhaust nozzle fitted with translating cold flaps
- Patent number 6,164,563
- Issue date Dec 26, 2000
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Philippe Pierre Vincent Bouiller
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable geometry exhaust nozzle for a turbine engine
- Patent number 5,833,140
- Issue date Nov 10, 1998
- United Technologies Corporation
- Constantino V. Loffredo
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbine engine equipped with thrust reverser
- Patent number 5,666,802
- Issue date Sep 16, 1997
- Jean-Pierre Lair
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable area outlet of a gas turbine engine discharge nozzle
- Patent number 5,476,224
- Issue date Dec 19, 1995
- Rolls-Royce plc
- Robert C. Tonks
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust reversing device for jet aircraft engines
- Patent number 5,392,991
- Issue date Feb 28, 1995
- Finmeccanica S.p.A. - Ramo Aziendale Alenia
- Alfredo Gatti
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbine engine equipped with thrust reverser
- Patent number 5,372,006
- Issue date Dec 13, 1994
- Aeronautical Concept of Exhaust, Ltd.
- Jean-Pierre Lair
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Jet engine provided with a thrust reverser
- Patent number 5,310,117
- Issue date May 10, 1994
- The Dee Howard Company
- Etienne Fage
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable area exhaust nozzle
- Patent number 5,221,048
- Issue date Jun 22, 1993
- Jean-Pierre Lair
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Jet engine provided with a thrust reverser
- Patent number 5,192,023
- Issue date Mar 9, 1993
- The Dee Howard Company
- Etienne Fage
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Jet engine provided with a thrust reverser
- Patent number 4,966,327
- Issue date Oct 30, 1990
- The Dee Howard Company
- Etienne Fage
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbojet engine having a thrust reverser door and variable exhaust...
- Patent number 4,865,256
- Issue date Sep 12, 1989
- Societe anonyme dite Hispano-Suiza
- Lionel F. G. J. Durand
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Yaw and pitch convergent-divergent thrust vectoring nozzle
- Patent number 4,836,451
- Issue date Jun 6, 1989
- United Technologies Corporation
- Paul W. Herrick
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable flow area nozzle
- Patent number 4,732,324
- Issue date Mar 22, 1988
- Rolls-Royce Inc.
- Douglas J. Nightingale
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Variable geometry nozzle with thrust reverser for a turbomachine
- Patent number 4,463,902
- Issue date Aug 7, 1984
- Rolls-Royce Inc.
- Douglas J. Nightingale
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Flight thrust reverser and vertical thrust control divergent nozzle...
- Patent number 4,194,692
- Issue date Mar 25, 1980
- Rohr Industries, Inc.
- Robert A. Dickenson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
METHOD OF VARYING A FAN DUCT NOZZLE THROAT AREA OF A GAS TURBINE EN...
- Publication number 20120124963
- Publication date May 24, 2012
- THE BOEING COMPANY
- Mark E. Howe
- A63 - SPORTS GAMES AMUSEMENTS
Information Patent Application
INTEGRATED VARIABLE AREA NOZZLE AND THRUST REVERSING MECHANISM
- Publication number 20100269485
- Publication date Oct 28, 2010
- Ashok K. Jain
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Thrust Reverser
- Publication number 20090126341
- Publication date May 21, 2009
- Jean-Pierre Lair
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
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...
Information Patent Application
Jet engine nozzle with variable thrust vectoring and exhaust area
- Publication number 20020158146
- Publication date Oct 31, 2002
- Jean-Pierre Lair
- B64 - AIRCRAFT AVIATION COSMONAUTICS

by means of pivoted eyelids

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Variable area nozzle for aircraft propulsion system

System for actuating a panel of a turbojet engine nacelle

Nacelle for an aircraft engine with variable section nozzle

Thrust reverse variable area fan nozzle

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

Rocket turbopump valves and associated systems and methods

Integrated variable area nozzle and thrust reversing mechanism

Thrust reverser

Nozzle with yaw vectoring vane

Thrust vectoring and variable exhaust area for jet engine nozzle

Vectorable variable area nozzle

Jet engine nozzle with variable thrust vectoring and exhaust area

Engine nozzle arrangement for an aircraft

Turbojet engine thrust reverser and exhaust nozzle

Turbo jet engine exhaust nozzle with masked gas jet

Converging exhaust nozzle fitted with translating cold flaps

Variable geometry exhaust nozzle for a turbine engine

Turbine engine equipped with thrust reverser

Variable area outlet of a gas turbine engine discharge nozzle

Thrust reversing device for jet aircraft engines

Turbine engine equipped with thrust reverser

Jet engine provided with a thrust reverser

Variable area exhaust nozzle

Jet engine provided with a thrust reverser

Jet engine provided with a thrust reverser

Turbojet engine having a thrust reverser door and variable exhaust...

Yaw and pitch convergent-divergent thrust vectoring nozzle

Variable flow area nozzle

Variable geometry nozzle with thrust reverser for a turbomachine

Flight thrust reverser and vertical thrust control divergent nozzle...

Patents Applicationslast 30 patents

METHOD OF VARYING A FAN DUCT NOZZLE THROAT AREA OF A GAS TURBINE EN...

INTEGRATED VARIABLE AREA NOZZLE AND THRUST REVERSING MECHANISM

Thrust Reverser

NOZZLE WITH YAW VECTORING VANE

Thrust vectoring and variable exhaust area for jet engine nozzle

Jet engine nozzle with variable thrust vectoring and exhaust area