by axially moving or transversely deforming an internal member

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CPC
F02K1/08

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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

F02K1/08by axially moving or transversely deforming an internal member

Industries

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Patents Grantslast 30 patents

Information Patent Grant
Variable area nozzle for an aircraft engine
- Patent number 12,152,551
- Issue date Nov 26, 2024
- RTX Corporation
- Michael G. McCaffrey
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable area nozzle assembly for an aircraft propulsion system
- Patent number 12,110,839
- Issue date Oct 8, 2024
- RTX Corporation
- Michael G. McCaffrey
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle assembly for an aircraft propulsion system
- Patent number 12,103,695
- Issue date Oct 1, 2024
- Pratt & Whitney Canada Corp.
- Michel Labrecque
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Liquid hydrogen-liquid oxygen fueled powerplant
- Patent number 11,905,914
- Issue date Feb 20, 2024
- RTX Corporation
- Walter A. Ledwith
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Supersonic aircraft turbofan engine
- Patent number 11,884,414
- Issue date Jan 30, 2024
- Rolls-Royce PLC
- Robert J Corin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable area exhaust nozzle system and method for control thereof
- Patent number 11,732,673
- Issue date Aug 22, 2023
- General Electric Company
- Mustafa Dindar
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Single movement convergent and convergent-divergent nozzle
- Patent number 11,680,495
- Issue date Jun 20, 2023
- Rolls-Royce North American Technologies Inc.
- Andrew Sanderson
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
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
Propelling nozzle for a turbofan engine on a supersonic aircraft
- Patent number 11,448,162
- Issue date Sep 20, 2022
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag Todorovic
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Split sleeve hidden door thrust reverser
- Patent number 11,434,850
- Issue date Sep 6, 2022
- Rohr, Inc.
- Timothy Gormley
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Reconfigurable exhaust nozzle for a gas turbine engine
- Patent number 11,408,368
- Issue date Aug 9, 2022
- Rolls-Royce North American Technologies Inc.
- David L. Sutterfield
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
Exhaust nozzle having a compliant shell for a gas turbine engine
- Patent number 11,326,551
- Issue date May 10, 2022
- Rolls-Royce North American Technologies Inc.
- David L. Sutterfield
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle of a gas turbine engine
- Patent number 11,326,552
- Issue date May 10, 2022
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag Todorovic
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Single movement convergent and convergent-divergent nozzle
- Patent number 11,319,832
- Issue date May 3, 2022
- Rolls-Royce North American Technologies Inc.
- Andrew Sanderson
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Exhaust nozzle with centerbody support structure for a gas turbine...
- Patent number 11,313,320
- Issue date Apr 26, 2022
- Rolls-Royce North American Technologies Inc.
- David L. Sutterfield
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle of a gas turbine engine
- Patent number 11,313,321
- Issue date Apr 26, 2022
- Rolls-Royce Deutschland Ltd & Co KG
- Predrag Todorovic
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle
- Patent number 11,306,680
- Issue date Apr 19, 2022
- Rolls-Royce PLC
- Jack F Colebrooke
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable area nozzle exhaust system with integrated thrust reverser
- Patent number 11,286,878
- Issue date Mar 29, 2022
- Rolls-Royce North American Technologies Inc.
- Todd S. Taylor
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Methodology for minimizing aerodynamic buzz in an exhaust nozzle
- Patent number 11,274,631
- Issue date Mar 15, 2022
- Rolls-Royce North American Technologies Inc.
- Andrew Sanderson
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Exhaust nozzle with vane support structure for a gas turbine engine
- Patent number 11,274,630
- Issue date Mar 15, 2022
- Rolls-Royce North American Technologies Inc.
- David L. Sutterfield
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Auxiliary device for three air flow path gas turbine engine
- Patent number 11,261,827
- Issue date Mar 1, 2022
- Raytheon Technologies Corporation
- Gary D. Roberge
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle of a gas turbine engine
- Patent number 11,248,561
- Issue date Feb 15, 2022
- Rolls-Royce Deutschland Ltd & Co KG
- Predrag Todorovic
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle of a gas turbine engine
- Patent number 11,215,140
- Issue date Jan 4, 2022
- Rolls-Royce Deutschland Ltd & Co KG
- Predrag Todorovic
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Nacelle of a turbojet comprising a reverser flap and a deployment s...
- Patent number 11,215,142
- Issue date Jan 4, 2022
- Airbus Operations SAS
- Olivier Pautis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle of a gas turbine engine
- Patent number 11,187,186
- Issue date Nov 30, 2021
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag Todorovic
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Dual-mode plug nozzle
- Patent number 11,143,052
- Issue date Oct 12, 2021
- General Electric Company
- Trevor Andrew Tersmette
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Supersonic aircraft turbofan
- Patent number 11,053,886
- Issue date Jul 6, 2021
- Rolls-Royce PLC
- John R Whurr
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Tail cone apparatus and methods for reducing nozzle surface tempera...
- Patent number 10,787,994
- Issue date Sep 29, 2020
- The Boeing Company
- Chad M. Winkler
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Convergent-divergent nozzle for a turbofan engine of a supersonic a...
- Patent number 10,738,735
- Issue date Aug 11, 2020
- Rolls-Royce Deutschland Ltd & Co KG
- Predrag Todorovic
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
VARIABLE AREA EXHAUST NOZZLE SYSTEM AND METHOD FOR CONTROL THEREOF
- Publication number 20230035756
- Publication date Feb 2, 2023
- GENERAL ELECTRIC COMPANY
- Mustafa Dindar
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SINGLE MOVEMENT CONVERGENT AND CONVERGENT-DIVERGENT NOZZLE
- Publication number 20220235668
- Publication date Jul 28, 2022
- Rolls-Royce North American Technologies Inc.
- Andrew Sanderson
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
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
VARIABLE AREA NOZZLE EXHAUST SYSTEM WITH INTEGRATED THRUST REVERSER
- Publication number 20210301761
- Publication date Sep 30, 2021
- Rolls-Royce North American Technologies Inc.
- Todd S. Taylor
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST NOZZLE WITH VANE SUPPORT STRUCTURE FOR A GAS TURBINE ENGINE
- Publication number 20210270207
- Publication date Sep 2, 2021
- Rolls-Royce North American Technologies Inc.
- David L. Sutterfield
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METHODOLOGY FOR MINIMIZING AERODYNAMIC BUZZ IN AN EXHAUST NOZZLE
- Publication number 20210270206
- Publication date Sep 2, 2021
- Rolls-Royce North American Technologies Inc.
- Andrew Sanderson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST NOZZLE
- Publication number 20210222647
- Publication date Jul 22, 2021
- Rolls-Royce plc
- Jack F. COLEBROOKE
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
EXHAUST NOZZLE OF A GAS TURBINE ENGINE
- Publication number 20210189998
- Publication date Jun 24, 2021
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag TODOROVIC
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST NOZZLE OF A GAS TURBINE ENGINE
- Publication number 20210189999
- Publication date Jun 24, 2021
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag TODOROVIC
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST NOZZLE OF A GAS TURBINE ENGINE
- Publication number 20210190002
- Publication date Jun 24, 2021
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag TODOROVIC
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE OF A TURBOJET COMPRISING A REVERSER FLAP AND A DEPLOYMENT S...
- Publication number 20200240360
- Publication date Jul 30, 2020
- Airbus Operations SAS
- Olivier Pautis
- 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
SPLIT SLEEVE HIDDEN DOOR THRUST REVERSER
- Publication number 20200025144
- Publication date Jan 23, 2020
- Timothy Gormley
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DUAL-MODE PLUG NOZZLE
- Publication number 20200025022
- Publication date Jan 23, 2020
- GENERAL ELECTRIC COMPANY
- Trevor Andrew Tersmette
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
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
EXHAUST NOZZLE CONTROL FOR A GAS TURBINE ENGINE
- Publication number 20180291837
- Publication date Oct 11, 2018
- Gary D. Roberge
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT GAS TURBINE HAVING A VARIABLE OUTLET NOZZLE OF A BYPASS FL...
- Publication number 20180266361
- Publication date Sep 20, 2018
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Frank Uwe KOEPF
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
CONVERGENT-DIVERGENT NOZZLE FOR A TURBOFAN ENGINE OF A SUPERSONIC A...
- Publication number 20180245539
- Publication date Aug 30, 2018
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag TODOROVIC
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
DIELECTRIC SEAL DEVICE
- Publication number 20170167441
- Publication date Jun 15, 2017
- Rohr, Inc.
- Joel H. Frank
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CHEVRON SYSTEM FOR GAS TURBINE ENGINE
- Publication number 20170122255
- Publication date May 4, 2017
- Pratt & Whitney Canada Corp.
- Ninad Joshi
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT ENGINE ASSEMBLY COMPRISING AT LEAST TWO REAR ENGINE ATTACH...
- Publication number 20170096229
- Publication date Apr 6, 2017
- AIRBUS OPERATIONS (SAS)
- Olivier PAUTIS
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST NOZZLE CONTROL FOR A GAS TURBINE ENGINE
- Publication number 20160377026
- Publication date Dec 29, 2016
- Gary D. Roberge
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
VARIABLE AREA FAN NOZZLE WITH DRIVE SYSTEM HEALTH MONITORING
- Publication number 20160230701
- Publication date Aug 11, 2016
- Rohr, Inc.
- Kevin Robert Scanlon
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
Gas Turbine Engine System for Modulating Flow of Fan By-Pass Air an...
- Publication number 20160153397
- Publication date Jun 2, 2016
- United Technologies Corporation
- Jeffrey A. Lovett
- 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
NOZZLE HAVING A VARIABLE NECK SECTION FOR A SPACECRAFT THRUSTER PRO...
- Publication number 20160003195
- Publication date Jan 7, 2016
- HERAKLES
- Mathieu CLERMONT
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
VARIABLE-SECTION NOZZLE, AND AIRCRAFT TURBOJET ENGINE NACELLE EQUIP...
- Publication number 20150345423
- Publication date Dec 3, 2015
- Aircelle
- Hervé Hurlin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST NOZZLE AND METHOD FOR CHANGING EXHAUST FLOW PATH
- Publication number 20150048177
- Publication date Feb 19, 2015
- JAPAN AEROSPACE EXPLORATION AGENCY
- Junichi Akatsuka
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST DIFFUSER
- Publication number 20140161603
- Publication date Jun 12, 2014
- GENERAL ELECTRIC COMPANY
- Rohit Chouhan
- 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

by axially moving or transversely deforming an internal member

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Variable area nozzle for an aircraft engine

Variable area nozzle assembly for an aircraft propulsion system

Exhaust nozzle assembly for an aircraft propulsion system

Liquid hydrogen-liquid oxygen fueled powerplant

Supersonic aircraft turbofan engine

Variable area exhaust nozzle system and method for control thereof

Single movement convergent and convergent-divergent nozzle

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

Propelling nozzle for a turbofan engine on a supersonic aircraft

Split sleeve hidden door thrust reverser

Reconfigurable exhaust nozzle for a gas turbine engine

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

Exhaust nozzle having a compliant shell for a gas turbine engine

Exhaust nozzle of a gas turbine engine

Single movement convergent and convergent-divergent nozzle

Exhaust nozzle with centerbody support structure for a gas turbine...

Exhaust nozzle of a gas turbine engine

Exhaust nozzle

Variable area nozzle exhaust system with integrated thrust reverser

Methodology for minimizing aerodynamic buzz in an exhaust nozzle

Exhaust nozzle with vane support structure for a gas turbine engine

Auxiliary device for three air flow path gas turbine engine

Exhaust nozzle of a gas turbine engine

Exhaust nozzle of a gas turbine engine

Nacelle of a turbojet comprising a reverser flap and a deployment s...

Exhaust nozzle of a gas turbine engine

Dual-mode plug nozzle

Supersonic aircraft turbofan

Tail cone apparatus and methods for reducing nozzle surface tempera...

Convergent-divergent nozzle for a turbofan engine of a supersonic a...

Patents Applicationslast 30 patents

VARIABLE AREA EXHAUST NOZZLE SYSTEM AND METHOD FOR CONTROL THEREOF

SINGLE MOVEMENT CONVERGENT AND CONVERGENT-DIVERGENT NOZZLE

VARIABLE THREE DIMENSIONAL CONVERGENT-DIVERGENT NOZZLE

VARIABLE AREA NOZZLE EXHAUST SYSTEM WITH INTEGRATED THRUST REVERSER

EXHAUST NOZZLE WITH VANE SUPPORT STRUCTURE FOR A GAS TURBINE ENGINE

METHODOLOGY FOR MINIMIZING AERODYNAMIC BUZZ IN AN EXHAUST NOZZLE

EXHAUST NOZZLE

EXHAUST NOZZLE OF A GAS TURBINE ENGINE

EXHAUST NOZZLE OF A GAS TURBINE ENGINE

EXHAUST NOZZLE OF A GAS TURBINE ENGINE

NACELLE OF A TURBOJET COMPRISING A REVERSER FLAP AND A DEPLOYMENT S...

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

SPLIT SLEEVE HIDDEN DOOR THRUST REVERSER

DUAL-MODE PLUG NOZZLE

JET ENGINE WITH A RADIALLY VARIABLE WALL

EXHAUST NOZZLE CONTROL FOR A GAS TURBINE ENGINE

AIRCRAFT GAS TURBINE HAVING A VARIABLE OUTLET NOZZLE OF A BYPASS FL...

CONVERGENT-DIVERGENT NOZZLE FOR A TURBOFAN ENGINE OF A SUPERSONIC A...

DIELECTRIC SEAL DEVICE

CHEVRON SYSTEM FOR GAS TURBINE ENGINE

AIRCRAFT ENGINE ASSEMBLY COMPRISING AT LEAST TWO REAR ENGINE ATTACH...

EXHAUST NOZZLE CONTROL FOR A GAS TURBINE ENGINE

VARIABLE AREA FAN NOZZLE WITH DRIVE SYSTEM HEALTH MONITORING

Gas Turbine Engine System for Modulating Flow of Fan By-Pass Air an...

FOLDABLE GUIDING VENTILATOR COVER FOR AN AIRCRAFT ENGINE ASSEMBLY

NOZZLE HAVING A VARIABLE NECK SECTION FOR A SPACECRAFT THRUSTER PRO...

VARIABLE-SECTION NOZZLE, AND AIRCRAFT TURBOJET ENGINE NACELLE EQUIP...

EXHAUST NOZZLE AND METHOD FOR CHANGING EXHAUST FLOW PATH

EXHAUST DIFFUSER

INNER STRUCTURE FOR AN AIRCRAFT NACELLE