characterised by using a nozzle provided with at least a deflector mounted within the nozzle

Industry

CPC
F42B10/665

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 F42Ammunition F42BEXPLOSIVE CHARGES F42B10/00Means for influencing

Current Industry

F42B10/665characterised by using a nozzle provided with at least a deflector mounted within the nozzle

Industries

Patents Grantslast 30 patents

Information Patent Grant
Method for reducing jet tab exposure during thrust vectoring
- Patent number 11,879,416
- Issue date Jan 23, 2024
- Raytheon Company
- Brandon J. Napier
- F42 - AMMUNITION BLASTING
Information Patent Grant
Steering system with power take-off from actuators
- Patent number 11,733,011
- Issue date Aug 22, 2023
- Raytheon Company
- John Bugge
- F42 - AMMUNITION BLASTING
Information Patent Grant
Thrust vectoring apparatus, thrust vectoring method, and flying body
- Patent number 10,088,284
- Issue date Oct 2, 2018
- Mitsubishi Heavy Industries, Ltd.
- Fuminori Fujisawa
- F42 - AMMUNITION BLASTING
Information Patent Grant
Thrust vectoring apparatus and flying object having thrust vectorin...
- Patent number 9,663,222
- Issue date May 30, 2017
- Mitsubishi Heavy Industries, Ltd.
- Fuminori Fujisawa
- F42 - AMMUNITION BLASTING
Information Patent Grant
System for steering, about its axes of rotation, a moving body prop...
- Patent number 9,080,843
- Issue date Jul 14, 2015
- MBDA France
- Lionel Mazenq
- F42 - AMMUNITION BLASTING
Information Patent Grant
Flying object
- Patent number 8,561,385
- Issue date Oct 22, 2013
- Deutsches Zentrum fuer Luft -und Raumfahrt e.V.
- Helmut Ciezki
- F42 - AMMUNITION BLASTING
Information Patent Grant
Integral thrust vector and roll control system
- Patent number 8,387,360
- Issue date Mar 5, 2013
- Raytheon Company
- Lloyd E. Kinsey
- F42 - AMMUNITION BLASTING
Information Patent Grant
Actuation assembly
- Patent number 8,338,768
- Issue date Dec 25, 2012
- Honeywell International Inc.
- Casey Hanlon
- F42 - AMMUNITION BLASTING
Information Patent Grant
Component for use in streams of hot gas
- Patent number 8,268,438
- Issue date Sep 18, 2012
- Deutsches Zentrum fuer Luft -und Raumfahrt e.V.
- Martin Friess
- F42 - AMMUNITION BLASTING
Information Patent Grant
Jet vane and method for manufacturing a jet vane
- Patent number 8,147,206
- Issue date Apr 3, 2012
- Deutsches Zentrum fuer Luft -und Raumfahrt e.V.
- Bernhard Heidenreich
- F42 - AMMUNITION BLASTING
Information Patent Grant
Propulsion system with canted multinozzle grid
- Patent number 7,856,806
- Issue date Dec 28, 2010
- Raytheon Company
- Daniel Chasman
- F42 - AMMUNITION BLASTING
Information Patent Grant
Exhaust assembly for missile system, and method
- Patent number 7,728,266
- Issue date Jun 1, 2010
- Raytheon Company
- Edgar R. Melkers
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Retractable thrust vector control vane system and method
- Patent number 7,434,762
- Issue date Oct 14, 2008
- Raytheon Company
- William M. Hatalsky
- F42 - AMMUNITION BLASTING
Information Patent Grant
Jet vane thrust vector control system
- Patent number 7,313,910
- Issue date Jan 1, 2008
- Agency for Defense Development
- Won-Hoon Kim
- F42 - AMMUNITION BLASTING
Information Patent Grant
Multi-function actuator, and method of operating same
- Patent number 6,726,147
- Issue date Apr 27, 2004
- Moog Inc.
- Richard J. Perini
- F42 - AMMUNITION BLASTING
Information Patent Grant
Method and apparatus for planar actuation of a flared surface to co...
- Patent number 6,723,972
- Issue date Apr 20, 2004
- Lockheed Martin Corporation
- Wayne K. Schroeder
- F42 - AMMUNITION BLASTING
Information Patent Grant
Dissolvable thrust vector control vane
- Patent number 6,548,794
- Issue date Apr 15, 2003
- Raytheon Company
- Andrew B. Facciano
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Apparatus and method for controlling the motion of a solid body or...
- Patent number 6,250,586
- Issue date Jun 26, 2001
- Ramot University Authority for Applied Research and Industrial Development Ltd.
- Avi Seifert
- F42 - AMMUNITION BLASTING
Information Patent Grant
Method and apparatus for non-propulsive fin control in an air or se...
- Patent number 6,247,666
- Issue date Jun 19, 2001
- Lockheed Martin Corporation
- Brian C. Baker
- F42 - AMMUNITION BLASTING
Information Patent Grant
Variable configuration final nozzle assembly for a combined rocket/...
- Patent number 5,970,705
- Issue date Oct 26, 1999
- Rolls Royce, Limited
- Harold Alan Scrace
- F42 - AMMUNITION BLASTING
Information Patent Grant
Missile jet vane control system and method
- Patent number 5,806,791
- Issue date Sep 15, 1998
- Raytheon Company
- William M. Hatalsky
- F42 - AMMUNITION BLASTING
Information Patent Grant
Vectorable nozzle having jet vanes
- Patent number 5,511,745
- Issue date Apr 30, 1996
- Thiokol Corporation
- Lawrence C. Faupell
- F42 - AMMUNITION BLASTING
Information Patent Grant
Vane-type nozzle(s) for varying the magnitude and direction of a th...
- Patent number 5,110,047
- Issue date May 5, 1992
- Moog Inc.
- Hans G. Toews
- F42 - AMMUNITION BLASTING
Information Patent Grant
Droppable jet vane TVC
- Patent number 5,082,202
- Issue date Jan 21, 1992
- The United States of America as represented by the Secretary of the Navy
- Michael D. Jacobson
- F42 - AMMUNITION BLASTING
Information Patent Grant
Combination actuator and coolant supply for missile and rocket vect...
- Patent number 5,072,891
- Issue date Dec 17, 1991
- Applied Technology Associates
- Robert J. Cavalleri
- F42 - AMMUNITION BLASTING
Information Patent Grant
Propulsion, monitoring and control unit particularly for ballistic...
- Patent number 4,892,268
- Issue date Jan 9, 1990
- A.R.I.S.S.p.A.
- Claudio Peretti
- F42 - AMMUNITION BLASTING
Information Patent Grant
Control vanes for thrust vector control nozzle
- Patent number 4,754,927
- Issue date Jul 5, 1988
- Colt Industries Inc.
- Robert E. Fitzgerald
- F42 - AMMUNITION BLASTING
Information Patent Grant
Procedure for steering a low-speed missile, weapon system and missi...
- Patent number 4,645,139
- Issue date Feb 24, 1987
- Societe Nationale Industrielle Aeropatiale
- Jean Guillot
- F42 - AMMUNITION BLASTING
Information Patent Grant
Thrust vectoring apparatus for maneuvering missile in flight
- Patent number 4,627,586
- Issue date Dec 9, 1986
- The United States of America as represented by the Secretary of the Navy
- Maigonis V. Krumins
- F42 - AMMUNITION BLASTING
Information Patent Grant
Rocket vehicle
- Patent number 4,562,980
- Issue date Jan 7, 1986
- The Commonwealth of Australia
- Arnold L. Deans
- F42 - AMMUNITION BLASTING

Patents Applicationslast 30 patents

Information Patent Application
FIN CONTROL ACTUATION SYSTEM
- Publication number 20230375317
- Publication date Nov 23, 2023
- RAFAEL ADVANCED DEFENSE SYSTEMS LTD.
- Alexander Vainshtein
- F42 - AMMUNITION BLASTING
Information Patent Application
STEERING SYSTEM WITH POWER TAKE-OFF FROM ACTUATORS
- Publication number 20220163302
- Publication date May 26, 2022
- Raytheon Company
- John Bugge
- F42 - AMMUNITION BLASTING
Information Patent Application
THRUST VECTORING APPARATUS, THRUST VECTORING METHOD, AND FLYING BODY
- Publication number 20160108851
- Publication date Apr 21, 2016
- Mitsubishi Heavy Industries, Ltd.
- Fuminori FUJISAWA
- F42 - AMMUNITION BLASTING
Information Patent Application
SYSTEM FOR STEERING, ABOUT ITS AXES OF ROTATION, A MOVING BODY PROP...
- Publication number 20140110524
- Publication date Apr 24, 2014
- MBDA FRANCE
- Lionel Mazenq
- F42 - AMMUNITION BLASTING
Information Patent Application
ACTUATION ASSEMBLY
- Publication number 20120181372
- Publication date Jul 19, 2012
- Honeywell International Inc.
- Casey Hanlon
- F42 - AMMUNITION BLASTING
Information Patent Application
FLYING OBJECT
- Publication number 20110083418
- Publication date Apr 14, 2011
- Deutsches Zentrum fuer Luft- Und Raumfahrt e.V.
- Helmut Ciezki
- F42 - AMMUNITION BLASTING
Information Patent Application
PROPULSION SYSTEM WITH CANTED MULTINOZZLE GRID
- Publication number 20100313544
- Publication date Dec 16, 2010
- Daniel Chasman
- F42 - AMMUNITION BLASTING
Information Patent Application
Jet vane and method for manufacturing a jet vane
- Publication number 20100272577
- Publication date Oct 28, 2010
- Deutsches Zentrum fuer Luft-und Raumfahrt e.V.
- Bernhard Heidenreich
- F42 - AMMUNITION BLASTING
Information Patent Application
COMPONENT FOR USE IN STREAMS OF HOT GAS
- Publication number 20100223906
- Publication date Sep 9, 2010
- Deutsches Zentrum fuer Luft- Und Raumfahrt e.V.
- Martin Friess
- F42 - AMMUNITION BLASTING
Information Patent Application
INTEGRAL THRUST VECTOR AND ROLL CONTROL SYSTEM
- Publication number 20090288389
- Publication date Nov 26, 2009
- Lloyd E. Kinsey
- F42 - AMMUNITION BLASTING
Information Patent Application
RETRACTABLE THRUST VECTOR CONTROL VANE SYSTEM AND METHOD
- Publication number 20080179449
- Publication date Jul 31, 2008
- Raytheon Company
- William M. Hatalsky
- F42 - AMMUNITION BLASTING
Information Patent Application
Exhaust assembly for mass ejection drive system
- Publication number 20070152097
- Publication date Jul 5, 2007
- Edgar R. Melkers
- F42 - AMMUNITION BLASTING
Information Patent Application
Thrust vectoring
- Publication number 20070018034
- Publication date Jan 25, 2007
- John Eugene Dickau
- F42 - AMMUNITION BLASTING
Information Patent Application
Jet vane thrust vector control system
- Publication number 20050178878
- Publication date Aug 18, 2005
- AGENCY FOR DEFENSE DEVELOPMENT
- Won-Hoon Kim
- F42 - AMMUNITION BLASTING
Information Patent Application
Dissolvable thrust vector control vane
- Publication number 20020130216
- Publication date Sep 19, 2002
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Application
Method and apparatus for planar actuation of a flared surface to co...
- Publication number 20020079404
- Publication date Jun 27, 2002
- Wayne K. Schroeder
- F42 - AMMUNITION BLASTING

characterised by using a nozzle provided with at least a deflector mounted within the nozzle

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Method for reducing jet tab exposure during thrust vectoring

Steering system with power take-off from actuators

Thrust vectoring apparatus, thrust vectoring method, and flying body

Thrust vectoring apparatus and flying object having thrust vectorin...

System for steering, about its axes of rotation, a moving body prop...

Flying object

Integral thrust vector and roll control system

Actuation assembly

Component for use in streams of hot gas

Jet vane and method for manufacturing a jet vane

Propulsion system with canted multinozzle grid

Exhaust assembly for missile system, and method

Retractable thrust vector control vane system and method

Jet vane thrust vector control system

Multi-function actuator, and method of operating same

Method and apparatus for planar actuation of a flared surface to co...

Dissolvable thrust vector control vane

Apparatus and method for controlling the motion of a solid body or...

Method and apparatus for non-propulsive fin control in an air or se...

Variable configuration final nozzle assembly for a combined rocket/...

Missile jet vane control system and method

Vectorable nozzle having jet vanes

Vane-type nozzle(s) for varying the magnitude and direction of a th...

Droppable jet vane TVC

Combination actuator and coolant supply for missile and rocket vect...

Propulsion, monitoring and control unit particularly for ballistic...

Control vanes for thrust vector control nozzle

Procedure for steering a low-speed missile, weapon system and missi...

Thrust vectoring apparatus for maneuvering missile in flight

Rocket vehicle

Patents Applicationslast 30 patents

FIN CONTROL ACTUATION SYSTEM

STEERING SYSTEM WITH POWER TAKE-OFF FROM ACTUATORS

THRUST VECTORING APPARATUS, THRUST VECTORING METHOD, AND FLYING BODY

SYSTEM FOR STEERING, ABOUT ITS AXES OF ROTATION, A MOVING BODY PROP...

ACTUATION ASSEMBLY

FLYING OBJECT

PROPULSION SYSTEM WITH CANTED MULTINOZZLE GRID

Jet vane and method for manufacturing a jet vane

COMPONENT FOR USE IN STREAMS OF HOT GAS

INTEGRAL THRUST VECTOR AND ROLL CONTROL SYSTEM

RETRACTABLE THRUST VECTOR CONTROL VANE SYSTEM AND METHOD

Exhaust assembly for mass ejection drive system

Thrust vectoring

Jet vane thrust vector control system

Dissolvable thrust vector control vane

Method and apparatus for planar actuation of a flared surface to co...