Nozzles having means

Industry

CPC
F02K1/44

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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

F02K1/44Nozzles having means

Industries

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Patents Grantslast 30 patents

Information Patent Grant
Supersonic aircraft and method of reducing sonic booms and jet noise
- Patent number 12,110,841
- Issue date Oct 8, 2024
- Japan Aerospace Exploration Agency
- Junichi Akatsuka
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Ultra quiet split flow thrust reverser
- Patent number 11,959,438
- Issue date Apr 16, 2024
- Medhat Osman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft engine exhaust systems enabling reduced length aft strut f...
- Patent number 11,827,373
- Issue date Nov 28, 2023
- The Boeing Company
- Abhishek Sahay
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Lobed tubular piece made of a composite with unidirectional fibers
- Patent number 11,472,133
- Issue date Oct 18, 2022
- SAFRAN NACELLES
- Bertrand Desjoyeaux
- C04 - CEMENTS CONCRETE ARTIFICIAL STONE CERAMICS REFRACTORIES
Information Patent Grant
Acoustic fairing
- Patent number 11,448,161
- Issue date Sep 20, 2022
- Rohr, Inc.
- Pablo T. Sanz Martinez
- 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
Nozzle of a turbomachine provided with chevrons with a non-axisymme...
- Patent number 11,274,632
- Issue date Mar 15, 2022
- SAFRAN AIRCRAFT ENGINES
- Jonathan Langridge
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
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
Gas turbine engine exhaust component
- Patent number 10,774,685
- Issue date Sep 15, 2020
- RATHEON TECHNOLOGIES CORPORATION
- Jonathan Jeffery Eastwood
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Acoustic liners and method of shaping an inlet of an acoustic liner
- Patent number 10,563,578
- Issue date Feb 18, 2020
- MRA Systems, LLC
- Andrew Michael Roach
- B05 - SPRAYING OR ATOMISING IN GENERAL APPLYING LIQUIDS OR OTHER FLUENT MATER...
Information Patent Grant
Nozzle of a turbomachine provided with chevrons with a non-axisymme...
- Patent number 10,302,043
- Issue date May 28, 2019
- SAFRAN AIRCRAFT ENGINES
- Jonathan Langridge
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbomachine test bench with active noise control
- Patent number 10,161,267
- Issue date Dec 25, 2018
- Safran Aero Boosters SA
- Benoit Meys
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
Exhaust assembly center body
- Patent number 9,551,239
- Issue date Jan 24, 2017
- Rohr, Inc.
- Stuart James Byrne
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Noise reduction system
- Patent number 9,528,468
- Issue date Dec 27, 2016
- IHI Corporation
- Nozomi Tanaka
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Passive edge-tone suppression method
- Patent number 9,488,129
- Issue date Nov 8, 2016
- King Fahd University of Petroleum & Minerals
- Mohamed Yunus Mohamed Ismail
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Rotational annular airscrew with integrated acoustic arrester
- Patent number 9,476,385
- Issue date Oct 25, 2016
- The Boeing Company
- Matthew D. Moore
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Sound absorber, sound absorber assembly and an engine with a sound...
- Patent number 9,303,588
- Issue date Apr 5, 2016
- Airbus Defence and Space GmbH
- Reinhard Pongratz
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Exhaust cone
- Patent number 9,062,610
- Issue date Jun 23, 2015
- Rolls-Royce PLC
- Romuald Morvant
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust cone for aircraft turbojet engine
- Patent number 9,051,899
- Issue date Jun 9, 2015
- Aircelle
- Helene Malot
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Noise reducing device and jet propulsion system
- Patent number 8,904,795
- Issue date Dec 9, 2014
- IHI Corporation
- Tsutomu Oishi
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Device and method for controlling vortex structures in a turbulent...
- Patent number 8,904,801
- Issue date Dec 9, 2014
- Airbus
- Victor Feliksovitch Kopiev
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Noise reduction system with chamber
- Patent number 8,813,907
- Issue date Aug 26, 2014
- IHI Corporation
- Nozomi Tanaka
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Sound absorber for a gas turbine exhaust cone, and method for the p...
- Patent number 8,783,412
- Issue date Jul 22, 2014
- Rolls-Royce Deutschland Ltd & Co KG
- Predrag Todorovic
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Jet engine exhaust nozzle and associated system and method of use
- Patent number 8,746,613
- Issue date Jun 10, 2014
- Williams International Co., L.L.C.
- Mark E. Suchezky
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Acoustic panel for a turbojet engine nacelle, with in-built fasteners
- Patent number 8,579,078
- Issue date Nov 12, 2013
- Aircelle
- Herve Hurlin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas-turbine exhaust cone
- Patent number 8,307,945
- Issue date Nov 13, 2012
- Rolls-Royce Deutschland Ltd & Co KG
- Predrag Todorovic
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Inlet bleed heat system with ejector/mixer nozzles for noise reduction
- Patent number 8,272,222
- Issue date Sep 25, 2012
- General Electric Company
- Hua Zhang
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Device that makes it possible to improve the effectiveness of the a...
- Patent number 8,167,232
- Issue date May 1, 2012
- Airbus Operations SAS
- Fabrice Gantie
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Stave and ring CMC nozzle
- Patent number 8,047,004
- Issue date Nov 1, 2011
- The Boeing Company
- John Joseph Brown
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
FLUIDIC PROPULSION SYSTEM ENCLOSURE
- Publication number 20240229737
- Publication date Jul 11, 2024
- Freedom Flight Works Inc.
- Austin Blue
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ULTRA QUIET SPLIT FLOW THRUST REVERSER
- Publication number 20230213001
- Publication date Jul 6, 2023
- Medhat Osman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SUPERSONIC AIRCRAFT AND METHOD OF REDUCING SONIC BOOMS AND JET NOISE
- Publication number 20220268236
- Publication date Aug 25, 2022
- JAPAN AEROSPACE EXPLORATION AGENCY
- Junichi AKATSUKA
- G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information Patent Application
SYSTEMS AND METHODS FOR NON-CONTACT BORING
- Publication number 20220056800
- Publication date Feb 24, 2022
- ArcByt, Inc.
- Ian Wright
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
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
STRUCTURAL AND/OR ACOUSTIC PANEL OF A NACELLE OF AN AIRCRAFT PROPUL...
- Publication number 20200300196
- Publication date Sep 24, 2020
- SAFRAN NACELLES
- Bertrand DESJOYEAUX
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ACOUSTIC FAIRING
- Publication number 20200080512
- Publication date Mar 12, 2020
- Rohr, Inc.
- Pablo T. Sanz Martinez
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TAIL CONE APPARATUS AND METHODS FOR REDUCING NOZZLE SURFACE TEMPERA...
- Publication number 20190323453
- Publication date Oct 24, 2019
- The Boeing Company
- Chad M. Winkler
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
NOZZLE OF A TURBOMACHINE PROVIDED WITH CHEVRONS WITH A NON-AXISYMME...
- Publication number 20190234345
- Publication date Aug 1, 2019
- SAFRAN AIRCRAFT ENGINES
- Jonathan Langridge
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOFAN ENGINE FOR A CIVIL SUPERSONIC AIRCRAFT
- Publication number 20180094605
- Publication date Apr 5, 2018
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Knut ROSENAU
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PASSIVE EDGE-TONE SUPPRESSION METHOD
- Publication number 20160333823
- Publication date Nov 17, 2016
- KING FAHD UNIVERSITY OF PETROLEUM AND MINERALS
- MOHAMED YUNUS MOHAMED ISMAIL
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST ASSEMBLY CENTER BODY
- Publication number 20160312662
- Publication date Oct 27, 2016
- Rohr, Inc.
- Stuart James Byrne
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
HIGH TEMPERATURE, LOW OXIDATION, AMORPHOUS SILICON-COATED TITANIUM
- Publication number 20160265441
- Publication date Sep 15, 2016
- Rohr, Inc.
- DAVID E. PIERICK
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NOZZLE OF A TURBOMACHINE PROVIDED WITH CHEVRONS WITH A NON-AXISYMME...
- Publication number 20160160797
- Publication date Jun 9, 2016
- SNECMA
- Jonathan LANGRIDGE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ROTATIONAL ANNULAR AIRSCREW WITH INTEGRATED ACOUSTIC ARRESTER
- Publication number 20150000252
- Publication date Jan 1, 2015
- Matthew D. Moore
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST CONE
- Publication number 20140209408
- Publication date Jul 31, 2014
- Rolls-Royce plc
- Romuald MORVANT
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST CONE FOR AIRCRAFT TURBOJET ENGINE
- Publication number 20140158458
- Publication date Jun 12, 2014
- Aircelle
- Helene Malot
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SOUND ABSORBER FOR A GAS TURBINE EXHAUST CONE, AND METHOD FOR THE P...
- Publication number 20130306401
- Publication date Nov 21, 2013
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag TODOROVIC
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PRESSURE BALANCED AREA CONTROL OF HIGH ASPECT RATIO NOZZLE
- Publication number 20130232949
- Publication date Sep 12, 2013
- Gary J. Dillard
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ACOUSTIC PANEL FOR A TURBOJET ENGINE NACELLE, WITH IN-BUILT FASTENERS
- Publication number 20130133977
- Publication date May 30, 2013
- Herve Hurlin
- B32 - LAYERED PRODUCTS
Information Patent Application
NOISE REDUCTION SYSTEM
- Publication number 20120240587
- Publication date Sep 27, 2012
- Nozomi Tanaka
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
NOISE REDUCTION SYSTEM WITH CHAMBER
- Publication number 20120228054
- Publication date Sep 13, 2012
- Nozomi Tanaka
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS-TURBINE EXHAUST CONE
- Publication number 20120006614
- Publication date Jan 12, 2012
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag TODOROVIC
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Ejector/Mixer Nozzle for Noise Reduction
- Publication number 20110162383
- Publication date Jul 7, 2011
- Hua Zhang
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
NOISE REDUCING DEVICE AND JET PROPULSION SYSTEM
- Publication number 20110000181
- Publication date Jan 6, 2011
- Tsutomu Oishi
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
DEVICE AND METHOD FOR CONTROLLING VORTEX STRUCTURES IN A TURBULENT...
- Publication number 20100326060
- Publication date Dec 30, 2010
- AIRBUS
- Victor Feliksovitch Kopiev
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Jet Engine Exhaust Nozzle and Associated System and Method of Use
- Publication number 20100212288
- Publication date Aug 26, 2010
- WILLIAMS INTERNATIONAL CO., L.L.C.
- Mark L. SUCHEZKY
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
COATING
- Publication number 20100119819
- Publication date May 13, 2010
- John R. Rodgers
- C23 - COATING METALLIC MATERIAL COATING MATERIAL WITH METALLIC MATERIAL CHEMI...
Information Patent Application
DEVICE THAT MAKES IT POSSIBLE TO IMPROVE THE EFFECTIVENESS OF THE A...
- Publication number 20100038476
- Publication date Feb 18, 2010
- AIRBUS FRANCE
- Fabrice Gantie
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
LOW NOISE AIRCRAFT
- Publication number 20100006697
- Publication date Jan 14, 2010
- JAPAN AEROSPACE EXPLORATION AGENCY
- Shigeru Horinouchi
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Nozzles having means

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Supersonic aircraft and method of reducing sonic booms and jet noise

Ultra quiet split flow thrust reverser

Aircraft engine exhaust systems enabling reduced length aft strut f...

Lobed tubular piece made of a composite with unidirectional fibers

Acoustic fairing

Variable area nozzle exhaust system with integrated thrust reverser

Nozzle of a turbomachine provided with chevrons with a non-axisymme...

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

Gas turbine engine exhaust component

Acoustic liners and method of shaping an inlet of an acoustic liner

Nozzle of a turbomachine provided with chevrons with a non-axisymme...

Turbomachine test bench with active noise control

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

Exhaust assembly center body

Noise reduction system

Passive edge-tone suppression method

Rotational annular airscrew with integrated acoustic arrester

Sound absorber, sound absorber assembly and an engine with a sound...

Exhaust cone

Exhaust cone for aircraft turbojet engine

Noise reducing device and jet propulsion system

Device and method for controlling vortex structures in a turbulent...

Noise reduction system with chamber

Sound absorber for a gas turbine exhaust cone, and method for the p...

Jet engine exhaust nozzle and associated system and method of use

Acoustic panel for a turbojet engine nacelle, with in-built fasteners

Gas-turbine exhaust cone

Inlet bleed heat system with ejector/mixer nozzles for noise reduction

Device that makes it possible to improve the effectiveness of the a...

Stave and ring CMC nozzle

Patents Applicationslast 30 patents

FLUIDIC PROPULSION SYSTEM ENCLOSURE

ULTRA QUIET SPLIT FLOW THRUST REVERSER

SUPERSONIC AIRCRAFT AND METHOD OF REDUCING SONIC BOOMS AND JET NOISE

SYSTEMS AND METHODS FOR NON-CONTACT BORING

VARIABLE AREA NOZZLE EXHAUST SYSTEM WITH INTEGRATED THRUST REVERSER

STRUCTURAL AND/OR ACOUSTIC PANEL OF A NACELLE OF AN AIRCRAFT PROPUL...

ACOUSTIC FAIRING

TAIL CONE APPARATUS AND METHODS FOR REDUCING NOZZLE SURFACE TEMPERA...

NOZZLE OF A TURBOMACHINE PROVIDED WITH CHEVRONS WITH A NON-AXISYMME...

TURBOFAN ENGINE FOR A CIVIL SUPERSONIC AIRCRAFT

PASSIVE EDGE-TONE SUPPRESSION METHOD

EXHAUST ASSEMBLY CENTER BODY

HIGH TEMPERATURE, LOW OXIDATION, AMORPHOUS SILICON-COATED TITANIUM

NOZZLE OF A TURBOMACHINE PROVIDED WITH CHEVRONS WITH A NON-AXISYMME...

ROTATIONAL ANNULAR AIRSCREW WITH INTEGRATED ACOUSTIC ARRESTER

EXHAUST CONE

EXHAUST CONE FOR AIRCRAFT TURBOJET ENGINE

SOUND ABSORBER FOR A GAS TURBINE EXHAUST CONE, AND METHOD FOR THE P...

PRESSURE BALANCED AREA CONTROL OF HIGH ASPECT RATIO NOZZLE

ACOUSTIC PANEL FOR A TURBOJET ENGINE NACELLE, WITH IN-BUILT FASTENERS

NOISE REDUCTION SYSTEM

NOISE REDUCTION SYSTEM WITH CHAMBER

GAS-TURBINE EXHAUST CONE

Ejector/Mixer Nozzle for Noise Reduction

NOISE REDUCING DEVICE AND JET PROPULSION SYSTEM

DEVICE AND METHOD FOR CONTROLLING VORTEX STRUCTURES IN A TURBULENT...

Jet Engine Exhaust Nozzle and Associated System and Method of Use

COATING

DEVICE THAT MAKES IT POSSIBLE TO IMPROVE THE EFFECTIVENESS OF THE A...

LOW NOISE AIRCRAFT