Deployable nozzles

Industry

CPC
F02K9/976

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Parent Industries

FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F02Combustion engines F02KJET-PROPULSION PLANTS F02K9/00Rocket- engine plants

Current Industry

F02K9/976Deployable nozzles

Industries

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Patents Grantslast 30 patents

Information Patent Grant
Multi-pulse rocket propulsion motor
- Patent number 11,352,981
- Issue date Jun 7, 2022
- Exquadrum, Inc.
- Kevin E. Mahaffy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Device for modulating a gas ejection section
- Patent number 10,690,090
- Issue date Jun 23, 2020
- ARIANEGROUP SAS
- Pascal Caubet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Fragmenting nozzle system
- Patent number 10,690,091
- Issue date Jun 23, 2020
- Aerojet Rocketdyne, Inc.
- Phillip Stracener
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Fragmenting nozzle system
- Patent number 10,598,129
- Issue date Mar 24, 2020
- Aerojet Rocketdyne, Inc.
- Douglass McPherson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Spacecraft nozzle comprising an improved deployment system
- Patent number 10,578,056
- Issue date Mar 3, 2020
- ARIANEGROUP SAS
- Robert Gazave
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Expandable exhaust cone
- Patent number 10,563,620
- Issue date Feb 18, 2020
- Rolls-Royce North American Technologies Inc.
- Douglas D. Dierksmeier
- F42 - AMMUNITION BLASTING
Information Patent Grant
Spring-assisted deployment of a pivotable rocket motor
- Patent number 10,094,646
- Issue date Oct 9, 2018
- The Boeing Company
- Justin G. Albright
- F42 - AMMUNITION BLASTING
Information Patent Grant
Launcher stage comprising a temporary support structure for tempora...
- Patent number 9,989,015
- Issue date Jun 5, 2018
- SNECMA
- Olivier Condaminet
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Threaded rod for system for deploying a deployable divergent segmen...
- Patent number 9,631,577
- Issue date Apr 25, 2017
- SNECMA
- Jacques Lelong
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
System for reducing the dynamic behavior of the movable segment of...
- Patent number 9,494,110
- Issue date Nov 15, 2016
- SNECMA
- Noël David
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Extendable nozzle for rocket engine
- Patent number 9,200,597
- Issue date Dec 1, 2015
- Florida Turbine Technologies, Inc.
- Alex Pinera
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Convex thermal shield for rocket engine with extendable divergent n...
- Patent number 9,169,807
- Issue date Oct 27, 2015
- SNECMA
- Olivier Dobek
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Fastener fitting between the movable portion of a deployable diverg...
- Patent number 9,080,533
- Issue date Jul 14, 2015
- SNECMA
- Michel Fiolek
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rocket nozzle assembly
- Patent number 8,952,304
- Issue date Feb 10, 2015
- Alliant Techsystems, Inc.
- Joseph O. Bellotte
- F42 - AMMUNITION BLASTING
Information Patent Grant
Deployable divergent nozzle for a propulsive unit
- Patent number 8,893,503
- Issue date Nov 25, 2014
- SNECMA
- Olivier Condaminet
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Extendible exhaust nozzle bell for a rocket engine
- Patent number 7,571,610
- Issue date Aug 11, 2009
- EADS Space Transportation GmbH
- Joachim Kretschmer
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Extendible exhaust nozzle bell for a rocket engine
- Patent number 7,299,636
- Issue date Nov 27, 2007
- EADS Space Transportation GmbH
- Franz Sperber
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Method for extending a nozzle and extended nozzle for rocket drives
- Patent number 7,287,369
- Issue date Oct 30, 2007
- EADS Space Transportation GmbH
- Gerald Hagemann
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Engine with a central spike for a space launcher
- Patent number 6,901,740
- Issue date Jun 7, 2005
- Eads Launch Vehicles
- Max Calabro
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Nozzle extension
- Patent number 6,817,184
- Issue date Nov 16, 2004
- Astrium GmbH
- Josef Groeber
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aerospike augmentation of microthruster impulse
- Patent number 6,487,844
- Issue date Dec 3, 2002
- TRW Inc.
- Peter D. Lohn
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Deployable diverging part for a thruster
- Patent number 6,418,710
- Issue date Jul 16, 2002
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation - S.N.E.C....
- Bruno Perrier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Extendable divergent tail pipe propulsion unit
- Patent number 6,205,772
- Issue date Mar 27, 2001
- Societe Nationale d'etude et de Construction de Motenrs d'Aviation
- Bruno Perrier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Expandable nozzle mechanism for a rocket engine
- Patent number 5,641,123
- Issue date Jun 24, 1997
- Mitsubishi Jukogyo Kabushiki Kaisha
- Kenji Kishimoto
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rocket nozzle for a rocket engine
- Patent number 5,619,851
- Issue date Apr 15, 1997
- United Technologies Corporation
- Donald E. Johnson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Self-locking and reversible mechanism for deploying the diverging p...
- Patent number 5,282,576
- Issue date Feb 1, 1994
- Societe Europeenne de Propulsion
- Luc H. Chatenet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Extendible nozzle
- Patent number 5,048,289
- Issue date Sep 17, 1991
- Rockwell International Corporation
- William S. Brown
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Diverging portion of discontinuous curvature for a rocket engine no...
- Patent number 4,947,644
- Issue date Aug 14, 1990
- Societe Europeenne de Propulsion
- Eric Hermant
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rocket motor extendible nozzle exit cone
- Patent number 4,872,612
- Issue date Oct 10, 1989
- Morton Thiokol, Inc.
- Victor Singer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Spring apparatus
- Patent number 4,856,765
- Issue date Aug 15, 1989
- Kohno; Masahiro
- Masahiro Kohno
- B66 - HOISTING LIFTING HAULING

Patents Applicationslast 30 patents

Information Patent Application
EXPANDABLE EXHAUST CONE
- Publication number 20180045142
- Publication date Feb 15, 2018
- Rolls-Royce Corporation
- Douglas D. Dierksmeier
- F42 - AMMUNITION BLASTING
Information Patent Application
SPACECRAFT NOZZLE COMPRISING AN IMPROVED DEPLOYMENT SYSTEM
- Publication number 20170306889
- Publication date Oct 26, 2017
- Airbus Safran Launchers SAS
- Robert GAZAVE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LAUNCHER STAGE COMPRISING A TEMPORARY SUPPORT STRUCTURE FOR TEMPORA...
- Publication number 20150047362
- Publication date Feb 19, 2015
- SNECMA
- Olivier Condaminet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ROCKET NOZZLE ASSEMBLY
- Publication number 20140291441
- Publication date Oct 2, 2014
- ALLIANT TECHSYSTEMS INC.
- Joseph O. Bellotte
- F42 - AMMUNITION BLASTING
Information Patent Application
SYSTEM FOR REDUCING THE DYNAMIC BEHAVIOR OF THE MOVABLE SEGMENT OF...
- Publication number 20140175191
- Publication date Jun 26, 2014
- SNECMA
- Noël David
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
THREADED ROD FOR SYSTEM FOR DEPLOYING A DEPLOYABLE DIVERGENT SEGMEN...
- Publication number 20140131481
- Publication date May 15, 2014
- SNECMA
- Jacques LELONG
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ROCKET ENGINE WITH EXTENDABLE DIVERGENT
- Publication number 20120167575
- Publication date Jul 5, 2012
- SNECMA
- Olivier Dobek
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEPLOYABLE DIVERGENT NOZZLE FOR A PROPULSIVE UNIT
- Publication number 20120067052
- Publication date Mar 22, 2012
- Olivier Condaminet
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
FASTENER FITTING BETWEEN THE MOVABLE PORTION OF A DEPLOYABLE DIVERG...
- Publication number 20120060467
- Publication date Mar 15, 2012
- Michel Fiolek
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXTENDIBLE EXHAUST NOZZLE BELL FOR A ROCKET ENGINE
- Publication number 20090178415
- Publication date Jul 16, 2009
- EADS Astrium GmbH
- Joachim Kretschmer
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Extendible exhaust nozzle bell for a rocket engine
- Publication number 20050016179
- Publication date Jan 27, 2005
- EADS Astrium GmbH
- Martin Roth
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Method for extending a nozzle and extended nozzle for rocket drives
- Publication number 20040231316
- Publication date Nov 25, 2004
- Gerald Hagemann
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Engine with a central spike for a space launcher
- Publication number 20030217552
- Publication date Nov 27, 2003
- Max Calabro
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Nozzle extension
- Publication number 20030136128
- Publication date Jul 24, 2003
- Josef Groeber
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Deployable nozzles

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Multi-pulse rocket propulsion motor

Device for modulating a gas ejection section

Fragmenting nozzle system

Fragmenting nozzle system

Spacecraft nozzle comprising an improved deployment system

Expandable exhaust cone

Spring-assisted deployment of a pivotable rocket motor

Launcher stage comprising a temporary support structure for tempora...

Threaded rod for system for deploying a deployable divergent segmen...

System for reducing the dynamic behavior of the movable segment of...

Extendable nozzle for rocket engine

Convex thermal shield for rocket engine with extendable divergent n...

Fastener fitting between the movable portion of a deployable diverg...

Rocket nozzle assembly

Deployable divergent nozzle for a propulsive unit

Extendible exhaust nozzle bell for a rocket engine

Extendible exhaust nozzle bell for a rocket engine

Method for extending a nozzle and extended nozzle for rocket drives

Engine with a central spike for a space launcher

Nozzle extension

Aerospike augmentation of microthruster impulse

Deployable diverging part for a thruster

Extendable divergent tail pipe propulsion unit

Expandable nozzle mechanism for a rocket engine

Rocket nozzle for a rocket engine

Self-locking and reversible mechanism for deploying the diverging p...

Extendible nozzle

Diverging portion of discontinuous curvature for a rocket engine no...

Rocket motor extendible nozzle exit cone

Spring apparatus

Patents Applicationslast 30 patents

EXPANDABLE EXHAUST CONE

SPACECRAFT NOZZLE COMPRISING AN IMPROVED DEPLOYMENT SYSTEM

LAUNCHER STAGE COMPRISING A TEMPORARY SUPPORT STRUCTURE FOR TEMPORA...

ROCKET NOZZLE ASSEMBLY

SYSTEM FOR REDUCING THE DYNAMIC BEHAVIOR OF THE MOVABLE SEGMENT OF...

THREADED ROD FOR SYSTEM FOR DEPLOYING A DEPLOYABLE DIVERGENT SEGMEN...

ROCKET ENGINE WITH EXTENDABLE DIVERGENT

DEPLOYABLE DIVERGENT NOZZLE FOR A PROPULSIVE UNIT

FASTENER FITTING BETWEEN THE MOVABLE PORTION OF A DEPLOYABLE DIVERG...

EXTENDIBLE EXHAUST NOZZLE BELL FOR A ROCKET ENGINE

Extendible exhaust nozzle bell for a rocket engine

Method for extending a nozzle and extended nozzle for rocket drives

Engine with a central spike for a space launcher

Nozzle extension