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FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F05Engines, pumps F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS F05D2250/00Geometry

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F05D2250/41with one degree of freedom

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Patents Grantslast 30 patents

Information Patent Grant
System for cooling an aircraft turbojet engine
- Patent number 11,994,069
- Issue date May 28, 2024
- SAFRAN NACELLES
- Julien Corbin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
System and method for reconfiguring a bleed system
- Patent number 11,808,215
- Issue date Nov 7, 2023
- General Electric Company
- Jorge Mario Rochin Machado
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Two-dimensional supersonic nozzle thrust vectoring using staggered...
- Patent number 11,614,050
- Issue date Mar 28, 2023
- The Regents of the University of California
- Carlos F. Montes
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbofan comprising a system comprising a screen for closing off th...
- Patent number 11,519,362
- Issue date Dec 6, 2022
- Airbus Operations SAS
- Lionel Czapla
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Wastegate for turbine
- Patent number 11,441,478
- Issue date Sep 13, 2022
- Cummins Ltd.
- Matthew J. Purdey
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine compressor radial door bleed valve
- Patent number 11,428,234
- Issue date Aug 30, 2022
- Raytheon Technologies Corporation
- Jonathan D. Little
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Divided volute turbocharger having vane ring with plurality of vane...
- Patent number 11,333,071
- Issue date May 17, 2022
- BorgWarner Inc.
- Greg Williams
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust reverser for an aircraft engine nacelle, comprising a panel...
- Patent number 11,293,378
- Issue date Apr 5, 2022
- SAFRAN NACELLES
- Alexis Tabouret
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Self retained linkage and system including the self retained linkag...
- Patent number 11,149,580
- Issue date Oct 19, 2021
- Raytheon Technologies Corporation
- Jacob Fassett
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Dual-mode plug nozzle
- Patent number 11,143,052
- Issue date Oct 12, 2021
- General Electric Company
- Trevor Andrew Tersmette
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Fan drive gear system mechanical controller
- Patent number 11,143,111
- Issue date Oct 12, 2021
- Raytheon Technologies Corporation
- John R. Otto
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Turbine with adjusting ring
- Patent number 11,118,500
- Issue date Sep 14, 2021
- BorgWarner Inc.
- Sascha Karstadt
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Dual function air diverter and variable area fan nozzle
- Patent number 11,028,776
- Issue date Jun 8, 2021
- Raytheon Technologies Corporation
- Richard Alan Weiner
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Aero loading shroud sealing
- Patent number 11,015,613
- Issue date May 25, 2021
- General Electric Company
- Daniel Patrick Kerns
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Non-contact seal assembly for rotational equipment
- Patent number 10,975,715
- Issue date Apr 13, 2021
- Raytheon Technologies Corporation
- William K. Ackermann
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Axial flow turbine having a diaphragm split in two halves at a hori...
- Patent number 10,934,892
- Issue date Mar 2, 2021
- General Electric Technology GmbH
- Julien Lemaire
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Aircraft engine rotor repaired with microstructural enhancement
- Patent number 10,865,644
- Issue date Dec 15, 2020
- KEYSTONE SYNERGISTIC ENTERPRISES, INC.
- Bryant Walker
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Turbofan comprising a series of rotatable blades for blocking off t...
- Patent number 10,830,089
- Issue date Nov 10, 2020
- Airbus Operations SAS
- Pascal Gardes
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbojet engine with thrust take-up means on the inter-compressor case
- Patent number 10,815,892
- Issue date Oct 27, 2020
- SAFRAN AIRCRAFT ENGINES
- Michel Gilbert Roland Brault
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Bleed valve system
- Patent number 10,794,217
- Issue date Oct 6, 2020
- Raytheon Technologies Corporation
- Anthony R. Bifulco
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Composite piston ring seal for axially and circumferentially transl...
- Patent number 10,760,500
- Issue date Sep 1, 2020
- Raytheon Technologies Corporation
- Steven D. Porter
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Variable diffuser having a respective penny for each vane
- Patent number 10,753,369
- Issue date Aug 25, 2020
- Rolls-Royce Corporation
- Christopher Hall
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Floating support assembly for compensating for axial thermal expansion
- Patent number 10,746,055
- Issue date Aug 18, 2020
- ANSALDO ENERGIA SWITZERLAND AG
- Meisam Sistaninia
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Mount structure for an aircraft ancillary engine unit
- Patent number 10,731,567
- Issue date Aug 4, 2020
- Rolls-Royce plc
- Rong Yang
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Solenoid actuated tine lock
- Patent number 10,677,194
- Issue date Jun 9, 2020
- Goodrich Actuation Systems Limited
- Andrew Hawksworth
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Discourager for discouraging flow through flow path gaps
- Patent number 10,669,874
- Issue date Jun 2, 2020
- General Electric Company
- Sergio Filippi
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable vane apparatus
- Patent number 10,655,629
- Issue date May 19, 2020
- HANWHA AEROSPACE CO., LTD
- Jong Goo Kim
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Gas turbine engine having section with thermally isolated area
- Patent number 10,634,055
- Issue date Apr 28, 2020
- United Technologies Corporation
- Brian D. Merry
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine accessory architecture
- Patent number 10,634,061
- Issue date Apr 28, 2020
- United Technologies Corporation
- Ryan K. Snyder
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Oil tank mount arrangement on a geared turbofan engine
- Patent number 10,577,979
- Issue date Mar 3, 2020
- United Technologies Corporation
- Todd A. Davis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
THRUST REVERSER FOR TURBOFAN PROPULSION SYSTEM OF AN AIRCRAFT AND T...
- Publication number 20230089038
- Publication date Mar 23, 2023
- LEONARDO S.P.A.
- Massimo POLI
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEM FOR COOLING AN AIRCRAFT TURBOJET ENGINE
- Publication number 20220186665
- Publication date Jun 16, 2022
- SAFRAN NACELLES
- Julien CORBIN
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
DIVIDED VOLUTE TURBOCHARGER HAVING VANE RING WITH PLURALITY OF VANE...
- Publication number 20210140366
- Publication date May 13, 2021
- BorgWarner Inc.
- Greg Williams
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
THRUST REVERSER FOR AN AIRCRAFT ENGINE NACELLE, COMPRISING A PANEL...
- Publication number 20200291894
- Publication date Sep 17, 2020
- SAFRAN NACELLES
- Alexis TABOURET
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DUAL-MODE PLUG NOZZLE
- Publication number 20200025022
- Publication date Jan 23, 2020
- GENERAL ELECTRIC COMPANY
- Trevor Andrew Tersmette
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
FAN DRIVE GEAR SYSTEM MECHANICAL CONTROLLER
- Publication number 20190368425
- Publication date Dec 5, 2019
- United Technologies Corporation
- John R. Otto
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
VARIABLE DIFFUSER HAVING A RESPECTIVE PENNY FOR EACH VANE
- Publication number 20190345839
- Publication date Nov 14, 2019
- Rolls-Royce Corporation
- Christopher Hall
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
TWO-DIMENSIONAL SUPERSONIC NOZZLE THRUST VECTORING USING STAGGERED...
- Publication number 20190195169
- Publication date Jun 27, 2019
- The Regents of the University of California
- Carlos F. Montes
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
DUAL FUNCTION AIR DIVERTER AND VARIABLE AREA FAN NOZZLE
- Publication number 20190101055
- Publication date Apr 4, 2019
- United Technologies Corporation
- Richard Alan Weiner
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
NON-CONTACT SEAL ASSEMBLY FOR ROTATIONAL EQUIPMENT
- Publication number 20190003327
- Publication date Jan 3, 2019
- United Technologies Corporation
- William K. Ackermann
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
OIL TANK MOUNT ARRANGEMENT ON A GEARED TURBOFAN ENGINE
- Publication number 20180245484
- Publication date Aug 30, 2018
- United Technologies Corporation
- Todd A. Davis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
COMPOSITE PISTON RING SEAL FOR AXIALLY AND CIRCUMFERENTIALLY TRAN...
- Publication number 20180238240
- Publication date Aug 23, 2018
- United Technologies Corproation
- Steven D. Porter
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
A DEVICE FOR MODULATING A GAS EJECTION SECTION
- Publication number 20180202393
- Publication date Jul 19, 2018
- ARIANEGROUP SAS
- Pascal CAUBET
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
RETRACTABLE ROCKET MOTOR IGNITER
- Publication number 20180187631
- Publication date Jul 5, 2018
- ARIANEGROUP SAS
- Gérard ROZ
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
VARIABLE VANE APPARATUS
- Publication number 20180163735
- Publication date Jun 14, 2018
- HANWHA TECHWIN CO., LTD.
- Jong Goo KIM
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
PARTICLE SEPARATOR
- Publication number 20180058323
- Publication date Mar 1, 2018
- Rolls-Royce North American Technologies, Inc.
- Crawford F. Smith
- B07 - SEPARATING SOLIDS FROM SOLIDS SORTING
Information Patent Application
AIRCRAFT ENGINE ROTOR REPAIRED WITH MICROSTRUCTURAL ENHANCEMENT
- Publication number 20170298735
- Publication date Oct 19, 2017
- KEYSTONE SYNERGISTIC ENTERPRISES, INC.
- Bryant Walker
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
CHEVRON NOZZLE
- Publication number 20170130672
- Publication date May 11, 2017
- RUDOLF GANZ
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Turbocharger With Turbine Nozzle Vanes And An Annular Rotary Bypass...
- Publication number 20150267605
- Publication date Sep 24, 2015
- Honeywell International Inc.
- Alain Lombard
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DUAL FUNCTION AIR DIVERTER AND VARIABLE AREA FAN NOZZLE
- Publication number 20150198092
- Publication date Jul 16, 2015
- United Technologies Corporation
- Richard Alan Weiner
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
APPARATUS FOR MOVING TURBINE SHELL
- Publication number 20140356152
- Publication date Dec 4, 2014
- Andrew Thomas Hynous
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
THREE STREAM, VARIABLE AREA FIXED APERTURE NOZZLE WITH PNEUMATIC AC...
- Publication number 20140263737
- Publication date Sep 18, 2014
- Rolls-Royce North American Technologies, Inc.
- Anthony F. Pierluissi
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOMACHINE GEARED ARCHITECTURE SUPPORT ASSEMBLY
- Publication number 20140219774
- Publication date Aug 7, 2014
- United Technologies Corporation
- John R. Otto
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEVICE FOR PIVOTING A ROTOR OF A TURBOMACHINE FROM A FIRST POSITION...
- Publication number 20140208584
- Publication date Jul 31, 2014
- Siemens Aktiengesellschaft
- Carsten Foerster
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
Metal Joining And Strengthening Methods Utilizing Microstructural E...
- Publication number 20140161618
- Publication date Jun 12, 2014
- Keystone Synergistic Enterprises, Inc.
- Bryant Walker
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
METHODS AND SYSTEMS FOR OPERATING AN INTEGRATED ACTUATOR
- Publication number 20140077116
- Publication date Mar 20, 2014
- GENERAL ELECTRIC COMPANY
- Gabriel Walker Santiago
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBOPROP ENGINE WITH COMPRESSOR TURBINE SHROUD
- Publication number 20140069107
- Publication date Mar 13, 2014
- Ian Alexander Macfarlane
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
STATIONARY BLADE RING, ASSEMBLY METHOD AND TURBOMACHINE
- Publication number 20140044526
- Publication date Feb 13, 2014
- MTU Aero Engines AG
- Werner Humhauser
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Thrust Reverser System
- Publication number 20130313337
- Publication date Nov 28, 2013
- The Boeing Company
- Eric D. Bol
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INNER TURBINE SHELL AXIAL MOVEMENT
- Publication number 20130302147
- Publication date Nov 14, 2013
- GENERAL ELECTRIC COMPANY
- Kenneth BLACK
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

with one degree of freedom

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

System for cooling an aircraft turbojet engine

System and method for reconfiguring a bleed system

Two-dimensional supersonic nozzle thrust vectoring using staggered...

Turbofan comprising a system comprising a screen for closing off th...

Wastegate for turbine

Gas turbine compressor radial door bleed valve

Divided volute turbocharger having vane ring with plurality of vane...

Thrust reverser for an aircraft engine nacelle, comprising a panel...

Self retained linkage and system including the self retained linkag...

Dual-mode plug nozzle

Fan drive gear system mechanical controller

Turbine with adjusting ring

Dual function air diverter and variable area fan nozzle

Aero loading shroud sealing

Non-contact seal assembly for rotational equipment

Axial flow turbine having a diaphragm split in two halves at a hori...

Aircraft engine rotor repaired with microstructural enhancement

Turbofan comprising a series of rotatable blades for blocking off t...

Turbojet engine with thrust take-up means on the inter-compressor case

Bleed valve system

Composite piston ring seal for axially and circumferentially transl...

Variable diffuser having a respective penny for each vane

Floating support assembly for compensating for axial thermal expansion

Mount structure for an aircraft ancillary engine unit

Solenoid actuated tine lock

Discourager for discouraging flow through flow path gaps

Variable vane apparatus

Gas turbine engine having section with thermally isolated area

Gas turbine engine accessory architecture

Oil tank mount arrangement on a geared turbofan engine

Patents Applicationslast 30 patents

THRUST REVERSER FOR TURBOFAN PROPULSION SYSTEM OF AN AIRCRAFT AND T...

SYSTEM FOR COOLING AN AIRCRAFT TURBOJET ENGINE

DIVIDED VOLUTE TURBOCHARGER HAVING VANE RING WITH PLURALITY OF VANE...

THRUST REVERSER FOR AN AIRCRAFT ENGINE NACELLE, COMPRISING A PANEL...

DUAL-MODE PLUG NOZZLE

FAN DRIVE GEAR SYSTEM MECHANICAL CONTROLLER

VARIABLE DIFFUSER HAVING A RESPECTIVE PENNY FOR EACH VANE

TWO-DIMENSIONAL SUPERSONIC NOZZLE THRUST VECTORING USING STAGGERED...

DUAL FUNCTION AIR DIVERTER AND VARIABLE AREA FAN NOZZLE

NON-CONTACT SEAL ASSEMBLY FOR ROTATIONAL EQUIPMENT

OIL TANK MOUNT ARRANGEMENT ON A GEARED TURBOFAN ENGINE

COMPOSITE PISTON RING SEAL FOR AXIALLY AND CIRCUMFERENTIALLY TRAN...

A DEVICE FOR MODULATING A GAS EJECTION SECTION

RETRACTABLE ROCKET MOTOR IGNITER

VARIABLE VANE APPARATUS

PARTICLE SEPARATOR

AIRCRAFT ENGINE ROTOR REPAIRED WITH MICROSTRUCTURAL ENHANCEMENT

CHEVRON NOZZLE

Turbocharger With Turbine Nozzle Vanes And An Annular Rotary Bypass...

DUAL FUNCTION AIR DIVERTER AND VARIABLE AREA FAN NOZZLE

APPARATUS FOR MOVING TURBINE SHELL

THREE STREAM, VARIABLE AREA FIXED APERTURE NOZZLE WITH PNEUMATIC AC...

TURBOMACHINE GEARED ARCHITECTURE SUPPORT ASSEMBLY

DEVICE FOR PIVOTING A ROTOR OF A TURBOMACHINE FROM A FIRST POSITION...

Metal Joining And Strengthening Methods Utilizing Microstructural E...

METHODS AND SYSTEMS FOR OPERATING AN INTEGRATED ACTUATOR

TURBOPROP ENGINE WITH COMPRESSOR TURBINE SHROUD

STATIONARY BLADE RING, ASSEMBLY METHOD AND TURBOMACHINE

Thrust Reverser System

INNER TURBINE SHELL AXIAL MOVEMENT