Reversing at least one flow in relation to at least one other flow in a plural- flow engine

Industry

CPC
F02K1/74

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

F02K1/74Reversing at least one flow in relation to at least one other flow in a plural- flow engine

Industries

Patents Grantslast 30 patents

Information Patent Grant
Track beam with composite lug
- Patent number 11,674,540
- Issue date Jun 13, 2023
- Rohr, Inc.
- Christian Soria
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbofan engine comprising a set of rotatable blades for blocking o...
- Patent number 11,486,335
- Issue date Nov 1, 2022
- Airbus Operations SAS
- Fabien Menou
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine with reversible heat exchanger
- Patent number 11,286,881
- Issue date Mar 29, 2022
- Rolls-Royce North American Technologies Inc.
- Douglas Boyd
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft propulsion assembly comprising a thrust reverser
- Patent number 11,136,937
- Issue date Oct 5, 2021
- SAFRAN AIRCRAFT ENGINES
- Nicolas Jérôme Jean Tantot
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Track beam with composite lug
- Patent number 10,352,273
- Issue date Jul 16, 2019
- Rohr, Inc.
- Christian Soria
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Dielectric elastomer device to fill steps or gaps in a thrust reverser
- Patent number 9,920,709
- Issue date Mar 20, 2018
- Rohr, Inc.
- Joel H. Frank
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Core cowl thrust reverser system and apparatus
- Patent number 9,650,992
- Issue date May 16, 2017
- Rohr, Inc.
- Michael Aten
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rotary hydraulic motor driven hybrid thrust reverser actuation syst...
- Patent number 9,650,993
- Issue date May 16, 2017
- Honeywell International Inc.
- Kevin K. Chakkera
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Device and method for assembling a fixed thrust reverser structure...
- Patent number 9,518,533
- Issue date Dec 13, 2016
- Aircelle
- Xavier Holay
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
By-pass turbojet including a thrust reverser
- Patent number 8,468,796
- Issue date Jun 25, 2013
- SNECMA
- Yves Emprin
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Pivoting door thrust reverser with controlled bypass through the re...
- Patent number 5,937,636
- Issue date Aug 17, 1999
- Societe Hispano-Suiza
- Patrick Gonidec
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Blockerless thrust reverser
- Patent number 5,904,320
- Issue date May 18, 1999
- Northrop Gunman Corporation
- Runyon H. Tindell
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Fluid flow control devices and methods
- Patent number 5,720,453
- Issue date Feb 24, 1998
- British Aerospace Plc
- John T. Platt
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Multi axis thrust vectoring for turbo fan engines
- Patent number 5,706,649
- Issue date Jan 13, 1998
- Boeing North American, Inc.
- Michael R. Robinson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Jet propulsion powerplants
- Patent number 5,271,222
- Issue date Dec 21, 1993
- British Aerospace Public Limited Company
- Ronald Coe
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas ejection nozzle for a jet engine and a jet engine fitted with t...
- Patent number 5,211,008
- Issue date May 18, 1993
- Conception Aeronautique du Sud Ouest
- Etienne Fage
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust reversing system for high bypass fan engines
- Patent number 5,142,862
- Issue date Sep 1, 1992
- The Boeing Company
- Robert B. Brown
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust reversing system and method
- Patent number 5,103,634
- Issue date Apr 14, 1992
- The Boeing Company
- Geoffrey E. Harrison
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust reversing system for high bypass fan engines
- Patent number 4,922,711
- Issue date May 8, 1990
- The Boeing Company
- Robert B. Brown
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Double flow turbine engine equipped with a central mixing nozzle an...
- Patent number 4,581,890
- Issue date Apr 15, 1986
- Pierre Giraud
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Mounting for gas turbine powerplant
- Patent number 4,326,682
- Issue date Apr 27, 1982
- Rolls-Royce Limited
- Douglas J. Nightingale
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Ducted fan gas turbine engine
- Patent number 4,228,651
- Issue date Oct 21, 1980
- Rolls-Royce Limited
- John A. Mullins
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust reverser nozzle
- Patent number 4,147,027
- Issue date Apr 3, 1979
- Grumman Aerospace Corporation
- William K. Greathouse
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Combination primary and fan air thrust reversal control systems for...
- Patent number 4,073,440
- Issue date Feb 14, 1978
- The Boeing Company
- Donald W. Hapke
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust reverser for by-pass gas turbine engine
- Patent number 4,069,663
- Issue date Jan 24, 1978
- Rolls-Royce (1971) Limited
- Leslie Richard Harper
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
3824784
- Patent number 3,824,784
- Issue date Jul 23, 1974
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
3684183
- Patent number 3,684,183
- Issue date Aug 15, 1972
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
3660982
- Patent number 3,660,982
- Issue date May 9, 1972
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
3618323
- Patent number 3,618,323
- Issue date Nov 9, 1971
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
3616648
- Patent number 3,616,648
- Issue date Nov 2, 1971
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
AIRCRAFT DUAL-FLOW TURBINE ENGINE ASSEMBLY, THE ASSEMBLY BEING EQUI...
- Publication number 20230407797
- Publication date Dec 21, 2023
- SAFRAN AIRCRAFT ENGINES
- Eva Julie LEBEAULT
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TRACK BEAM WITH COMPOSITE LUG
- Publication number 20210088001
- Publication date Mar 25, 2021
- Rohr, Inc.
- Christian Soria
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
BY-PASS TURBOJET INCLUDING A THRUST REVERSER
- Publication number 20080250770
- Publication date Oct 16, 2008
- SNECMA
- Yves EMPRIN
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Thrust vectoring
- Publication number 20070018034
- Publication date Jan 25, 2007
- John Eugene Dickau
- F42 - AMMUNITION BLASTING

Reversing at least one flow in relation to at least one other flow in a plural- flow engine

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Track beam with composite lug

Turbofan engine comprising a set of rotatable blades for blocking o...

Gas turbine engine with reversible heat exchanger

Aircraft propulsion assembly comprising a thrust reverser

Track beam with composite lug

Dielectric elastomer device to fill steps or gaps in a thrust reverser

Core cowl thrust reverser system and apparatus

Rotary hydraulic motor driven hybrid thrust reverser actuation syst...

Device and method for assembling a fixed thrust reverser structure...

By-pass turbojet including a thrust reverser

Pivoting door thrust reverser with controlled bypass through the re...

Blockerless thrust reverser

Fluid flow control devices and methods

Multi axis thrust vectoring for turbo fan engines

Jet propulsion powerplants

Gas ejection nozzle for a jet engine and a jet engine fitted with t...

Thrust reversing system for high bypass fan engines

Thrust reversing system and method

Thrust reversing system for high bypass fan engines

Double flow turbine engine equipped with a central mixing nozzle an...

Mounting for gas turbine powerplant

Ducted fan gas turbine engine

Thrust reverser nozzle

Combination primary and fan air thrust reversal control systems for...

Thrust reverser for by-pass gas turbine engine

3824784

3684183

3660982

3618323

3616648

Patents Applicationslast 30 patents

AIRCRAFT DUAL-FLOW TURBINE ENGINE ASSEMBLY, THE ASSEMBLY BEING EQUI...

TRACK BEAM WITH COMPOSITE LUG

BY-PASS TURBOJET INCLUDING A THRUST REVERSER

Thrust vectoring