Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet

Industry

CPC
F02K1/40

This industry / category may be too specific. Please go to a parent level for more data

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

F02K1/40Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet

Industries

Patents Grantslast 30 patents

Information Patent Grant
Exhaust duct for gas turbine engine
- Patent number 11,952,962
- Issue date Apr 9, 2024
- Pratt & Whitney Canada Corp.
- Eray Akcayoz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Vectoring exhaust nozzle for an aircraft powerplant
- Patent number 11,867,135
- Issue date Jan 9, 2024
- RTX Corporation
- Michael Murphy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Deflectable distributed aerospike rocket nozzle
- Patent number 11,352,978
- Issue date Jun 7, 2022
- Raytheon Company
- Daniel K. Johnson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust duct and exhaust duct assembly and aircraft using the exhau...
- Patent number 11,319,897
- Issue date May 3, 2022
- HANWHA AEROSPACE CO., LTD
- Young Jung Joo
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Convergent divergent exit nozzle for a gas turbine engine
- Patent number 11,236,701
- Issue date Feb 1, 2022
- Raytheon Technologies Corporation
- Dmitriy B. Sidelkovskiy
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
Gas expander
- Patent number 10,767,508
- Issue date Sep 8, 2020
- Mitsubishi Heavy Industries Compressor Corporation
- Naoto Yonemura
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Flight control mechanisms and methods of operating aircraft with fl...
- Patent number 10,704,496
- Issue date Jul 7, 2020
- The Boeing Company
- Robert Michael Lee
- 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
AFT exhaust system for rotary wing aircraft
- Patent number 10,562,641
- Issue date Feb 18, 2020
- Sikorsky Aircraft Corporation
- Joseph Pantalone
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Exhaust duct
- Patent number 10,514,003
- Issue date Dec 24, 2019
- Pratt & Whitney Canada Corp.
- Eray Akcayoz
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Convergent divergent exit nozzle for a gas turbine engine
- Patent number 10,371,092
- Issue date Aug 6, 2019
- United Technologies Corporation
- Dmitriy B. Sidelkovskiy
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Fairing for a mixer of a nozzle of a dual-flow turbomachine
- Patent number 10,273,904
- Issue date Apr 30, 2019
- SAFRAN AIRCRAFT ENGINES
- Benoit Argemiro Matthieu Debray
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbine engine nozzle having confluent streams and including a core...
- Patent number 10,167,814
- Issue date Jan 1, 2019
- SAFRAN AIRCRAFT ENGINES
- Romain Ferrier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust impingement cooling
- Patent number 9,995,181
- Issue date Jun 12, 2018
- Lockheed Martin Corporation
- Daniel N. Miller
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine nozzles with embossments in airfoil cavities
- Patent number 9,745,920
- Issue date Aug 29, 2017
- General Electric Company
- Martin James Jasper
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
System and method for exhausting combustion gases from gas turbine...
- Patent number 9,631,542
- Issue date Apr 25, 2017
- General Electric Company
- Moorthi Subramaniyan
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Propfan engine
- Patent number 8,689,558
- Issue date Apr 8, 2014
- Rolls-Royce PLC
- Kenneth J Mackie
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Outlet device for a jet engine and a craft comprising such an outle...
- Patent number 8,215,096
- Issue date Jul 10, 2012
- Volvo Aero Corporation
- Anders Lundbladh
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Jet engine nozzle exit configurations, including projections orient...
- Patent number 8,157,207
- Issue date Apr 17, 2012
- The Boeing Company
- Vinod G. Mengle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Arrangement for propelling an aircraft, aircraft and outlet nozzle...
- Patent number 8,061,145
- Issue date Nov 22, 2011
- Volvo Aero Corporation
- Bernhard Gustafsson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Outlet device for a jet engine and a jet engine comprising such an...
- Patent number 7,900,460
- Issue date Mar 8, 2011
- Volvo Aero Corporation
- Melker Härefors
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turbofan exhaust system
- Patent number 7,845,156
- Issue date Dec 7, 2010
- SNECMA
- Pascal Moise Michel Bigot
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Exhaust assembly forming a horizontal propulsion gas elbow in an ai...
- Patent number 7,784,284
- Issue date Aug 31, 2010
- SNECMA
- Edgar Brunet
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Exhaust assembly forming a horizontal propulsion gas elbow in an ai...
- Patent number 7,681,400
- Issue date Mar 23, 2010
- Snecma
- Thomas Daris
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Thrust orienting nozzle
- Patent number 7,631,486
- Issue date Dec 15, 2009
- SNECMA
- Alain Page
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Serrated nozzle trailing edge for exhaust noise suppression
- Patent number 7,543,452
- Issue date Jun 9, 2009
- United Technologies Corporation
- Ramons Andris Reba
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Exhaust nozzle for an engine of a flying craft
- Patent number 7,533,517
- Issue date May 19, 2009
- SNECMA
- Bruno Albert Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Device for mixing two flows of fluid which are initially guided sep...
- Patent number 7,299,635
- Issue date Nov 27, 2007
- MTU Aero Engines GmbH
- Karl Katheder
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Bifurcated turbofan nozzle
- Patent number 6,820,410
- Issue date Nov 23, 2004
- The NORDAM Group, INC.
- Jean-Pierre Lair
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
AVIATION TURBOFAN ENGINE AND FAN DUCT NOZZLE
- Publication number 20240124121
- Publication date Apr 18, 2024
- BEIJING AERONAUTICAL SCIENCE & TECHNOLOGY RESEARCH INSTITUTE, COMMERCIAL AIRC...
- Zheng CUI
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
THRUST ENHANCING DEVICE
- Publication number 20240084763
- Publication date Mar 14, 2024
- Sung Woo KIM
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEFLECTABLE DISTRIBUTED AEROSPIKE ROCKET NOZZLE
- Publication number 20210404415
- Publication date Dec 30, 2021
- Raytheon Company
- Daniel K. Johnson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST DUCT AND EXHAUST DUCT ASSEMBLY AND AIRCRAFT USING THE EXHAU...
- Publication number 20210215121
- Publication date Jul 15, 2021
- HANWHA AEROSPACE CO., LTD.
- Young Jung JOO
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT JET ENGINE COMPRISING MEANS FOR VARYING ITS OUTPUT SURFACE...
- Publication number 20200025128
- Publication date Jan 23, 2020
- Airbus Operations SAS
- Antoine COUSIN
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
TURBOFAN ENGINE
- Publication number 20190016471
- Publication date Jan 17, 2019
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Jan LIESER
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT AND FLIGHT CONTROL MECHANISMS USED ON AIRCRAFT
- Publication number 20180334247
- Publication date Nov 22, 2018
- The Boeing Company
- Robert Michael Lee
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
FLIGHT CONTROL MECHANISMS AND METHODS OF OPERATING AIRCRAFT WITH FL...
- Publication number 20180334246
- Publication date Nov 22, 2018
- The Boeing Company
- Robert Michael Lee
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NOZZLE AND NOZZLE ASSEMBLY FOR GAS TURBINE ENGINE
- Publication number 20170082062
- Publication date Mar 23, 2017
- Michael Anthony Ruthemeyer
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBINE ENGINE NOZZLE HAVING CONFLUENT STREAMS AND INCLUDING A CORE...
- Publication number 20160237949
- Publication date Aug 18, 2016
- SNECMA
- Romain FERRIER
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST DUCT
- Publication number 20160177872
- Publication date Jun 23, 2016
- Pratt & Whitney Canada Corp.
- ERAY AKCAYOZ
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEVICE FOR CONNECTING TWO SEGMENTS OF A PROPELLING NOZZLE
- Publication number 20160169155
- Publication date Jun 16, 2016
- SNECMA
- Dominique INDERSIE
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
FAIRING FOR A MIXER OF A NOZZLE OF A DUAL-FLOW TURBOMACHINE
- Publication number 20160131077
- Publication date May 12, 2016
- SNECMA
- Benoit Argemiro Matthieu DEBRAY
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Gas Turbine Nozzle
- Publication number 20160076483
- Publication date Mar 17, 2016
- Generl Electric Company
- Martin James Jasper
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ANGLED REVERSE CORE GAS TURBINE ENGINE WITH WIDENED NOZZLE
- Publication number 20150240745
- Publication date Aug 27, 2015
- United Technologies Corporation
- Wesley K. Lord
- 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
Exhaust impingement cooling
- Publication number 20130133857
- Publication date May 30, 2013
- Lockheed Martin Corporation
- Daniel N. Miller
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PROPFAN ENGINE
- Publication number 20100293920
- Publication date Nov 25, 2010
- Rolls-Royce plc
- Kenneth J. MACKIE
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
OUTLET DEVICE FOR A JET ENGINE AND A CRAFT COMPRISING SUCH AN OUTLE...
- Publication number 20090211224
- Publication date Aug 27, 2009
- VOLVO AERO CORPORATION
- Anders Lundladh
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Jet Engine Nozzle Exit Configurations, Including Projections Orient...
- Publication number 20080272228
- Publication date Nov 6, 2008
- The Boeing Company
- Vinod G. Mengle
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Arrangement for Propelling an Aircraft, Aircraft and Outlet Nozzle...
- Publication number 20080236138
- Publication date Oct 2, 2008
- VOLVO AERO CORPORATION
- Bernhard Gustafsson
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Outlet Device for a Jet Engine and a Jet Engine Comprising Such an...
- Publication number 20080016873
- Publication date Jan 24, 2008
- VOLVO AERO CORPORATION
- Melker Harefors
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST ASSEMBLY FORMING A HORIZONTAL PROPULSION GAS ELBOW IN AN AI...
- Publication number 20070266712
- Publication date Nov 22, 2007
- SNECMA
- Edgar Brunet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST ASSEMBLY FORMING A HORIZONTAL PROPULSION GAS ELBOW IN AN AI...
- Publication number 20070251211
- Publication date Nov 1, 2007
- SNECMA
- Thomas Daris
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBOFAN EXHAUST SYSTEM
- Publication number 20070176053
- Publication date Aug 2, 2007
- SNECMA
- Pascal Moise Michel BIGOT
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Serrated nozzle trailing edge for exhaust noise suppression
- Publication number 20070033922
- Publication date Feb 15, 2007
- United Technologies Corporation
- Ramons Andris Reba
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
THRUST ORIENTING NOZZLE
- Publication number 20070000233
- Publication date Jan 4, 2007
- SNECMA
- Alain Page
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Exhaust nozzle for an engine of a flying craft
- Publication number 20060230744
- Publication date Oct 19, 2006
- SNECMA
- Bruno Albert Beutin
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Ejector Nozzle
- Publication number 20060027679
- Publication date Feb 9, 2006
- Jack Edward Gratteau
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Device for mixing two flows of fluid which are initially guided sep...
- Publication number 20050022502
- Publication date Feb 3, 2005
- Karl Katheder
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Exhaust duct for gas turbine engine

Vectoring exhaust nozzle for an aircraft powerplant

Deflectable distributed aerospike rocket nozzle

Exhaust duct and exhaust duct assembly and aircraft using the exhau...

Convergent divergent exit nozzle for a gas turbine engine

Gas turbine engine exhaust component

Gas expander

Flight control mechanisms and methods of operating aircraft with fl...

Nacelle for an aircraft engine with variable section nozzle

AFT exhaust system for rotary wing aircraft

Exhaust duct

Convergent divergent exit nozzle for a gas turbine engine

Fairing for a mixer of a nozzle of a dual-flow turbomachine

Turbine engine nozzle having confluent streams and including a core...

Exhaust impingement cooling

Gas turbine nozzles with embossments in airfoil cavities

System and method for exhausting combustion gases from gas turbine...

Propfan engine

Outlet device for a jet engine and a craft comprising such an outle...

Jet engine nozzle exit configurations, including projections orient...

Arrangement for propelling an aircraft, aircraft and outlet nozzle...

Outlet device for a jet engine and a jet engine comprising such an...

Turbofan exhaust system

Exhaust assembly forming a horizontal propulsion gas elbow in an ai...

Exhaust assembly forming a horizontal propulsion gas elbow in an ai...

Thrust orienting nozzle

Serrated nozzle trailing edge for exhaust noise suppression

Exhaust nozzle for an engine of a flying craft

Device for mixing two flows of fluid which are initially guided sep...

Bifurcated turbofan nozzle

Patents Applicationslast 30 patents

AVIATION TURBOFAN ENGINE AND FAN DUCT NOZZLE

THRUST ENHANCING DEVICE

DEFLECTABLE DISTRIBUTED AEROSPIKE ROCKET NOZZLE

EXHAUST DUCT AND EXHAUST DUCT ASSEMBLY AND AIRCRAFT USING THE EXHAU...

AIRCRAFT JET ENGINE COMPRISING MEANS FOR VARYING ITS OUTPUT SURFACE...

TURBOFAN ENGINE

AIRCRAFT AND FLIGHT CONTROL MECHANISMS USED ON AIRCRAFT

FLIGHT CONTROL MECHANISMS AND METHODS OF OPERATING AIRCRAFT WITH FL...

NOZZLE AND NOZZLE ASSEMBLY FOR GAS TURBINE ENGINE

TURBINE ENGINE NOZZLE HAVING CONFLUENT STREAMS AND INCLUDING A CORE...

EXHAUST DUCT

DEVICE FOR CONNECTING TWO SEGMENTS OF A PROPELLING NOZZLE

FAIRING FOR A MIXER OF A NOZZLE OF A DUAL-FLOW TURBOMACHINE

Gas Turbine Nozzle

ANGLED REVERSE CORE GAS TURBINE ENGINE WITH WIDENED NOZZLE

PRESSURE BALANCED AREA CONTROL OF HIGH ASPECT RATIO NOZZLE

Exhaust impingement cooling

PROPFAN ENGINE

OUTLET DEVICE FOR A JET ENGINE AND A CRAFT COMPRISING SUCH AN OUTLE...

Jet Engine Nozzle Exit Configurations, Including Projections Orient...

Arrangement for Propelling an Aircraft, Aircraft and Outlet Nozzle...

Outlet Device for a Jet Engine and a Jet Engine Comprising Such an...

EXHAUST ASSEMBLY FORMING A HORIZONTAL PROPULSION GAS ELBOW IN AN AI...

EXHAUST ASSEMBLY FORMING A HORIZONTAL PROPULSION GAS ELBOW IN AN AI...

TURBOFAN EXHAUST SYSTEM

Serrated nozzle trailing edge for exhaust noise suppression

THRUST ORIENTING NOZZLE

Exhaust nozzle for an engine of a flying craft

Ejector Nozzle

Device for mixing two flows of fluid which are initially guided sep...