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CPC
F05D2250/22

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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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F05D2250/22parallelepipedal

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Patents Grantslast 30 patents

Information Patent Grant
Inlet filter housing having components including portions of filter...
- Patent number 11,988,142
- Issue date May 21, 2024
- GE INFRASTRUCTURE TECHNOLOGY LLC
- Laxmikant Merchant
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Ducted inlet for reducing flow oscillations
- Patent number 11,988,113
- Issue date May 21, 2024
- The Boeing Company
- Zachariah B. VanDeMark
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbomachine hollow blade
- Patent number 11,808,179
- Issue date Nov 7, 2023
- SAFRAN HELICOPTER ENGINES
- Laurence Vial
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Grant
Centralized oil distribution system
- Patent number 11,732,647
- Issue date Aug 22, 2023
- Daniella Sladen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Double walled stator housing
- Patent number 11,466,593
- Issue date Oct 11, 2022
- Raytheon Technologies Corporation
- Lawrence A. Binek
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Grant
Thermal insulation features for gas turbine engines
- Patent number 11,268,404
- Issue date Mar 8, 2022
- Raytheon Technologies Corporation
- David W. Morganson
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Grant
Gas turbine blade
- Patent number 11,015,452
- Issue date May 25, 2021
- Doosan Heavy Industries Construction Co., Ltd.
- Jong Hoon Park
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Blade ring segment for turbine section, turbine section having the...
- Patent number 10,947,862
- Issue date Mar 16, 2021
- Doosan Heavy Industries Construction Co., Ltd.
- Inkyom Kim
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbine airfoil with biased trailing edge cooling arrangement
- Patent number 10,900,361
- Issue date Jan 26, 2021
- Jan H. Marsh
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbomachine blade assembly
- Patent number 10,526,901
- Issue date Jan 7, 2020
- MTU Aero Engines AG
- Markus Schlemmer
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Blade, cut-back of blade or vane and gas turbine having the same
- Patent number 10,443,394
- Issue date Oct 15, 2019
- Doosan Heavy Industries Construction Co., Ltd.
- Mu Hyoung Lee
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Angled impingement inserts with cooling features
- Patent number 10,422,235
- Issue date Sep 24, 2019
- General Electric Company
- Ronald Scott Bunker
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Hollow blade having internal damper
- Patent number 10,316,670
- Issue date Jun 11, 2019
- United Technologies Corporation
- Robert J. Morris
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Shroud assembly for a turbine engine
- Patent number 10,280,785
- Issue date May 7, 2019
- General Electric Company
- Robert David Briggs
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Steam turbine rotor seal key member, related assembly and steam tur...
- Patent number 10,036,270
- Issue date Jul 31, 2018
- General Electric Company
- Steven Sebastian Burdgick
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Reversible blade rotor seal
- Patent number 10,030,530
- Issue date Jul 24, 2018
- United Technologies Corporation
- Daniel A. Snyder
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Brush seal
- Patent number 9,920,838
- Issue date Mar 20, 2018
- MTU Aero Engines AG
- Stephan Klaen
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Brush seal
- Patent number 9,598,970
- Issue date Mar 21, 2017
- Eagle Industry Co., Ltd.
- Hideyuki Inoue
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method for producing an acoustic treatment panel
- Patent number 8,733,501
- Issue date May 27, 2014
- Airbus Operations SAS
- Alain Porte
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Tailorable design configuration topologies for aircraft engine mid-...
- Patent number 8,707,710
- Issue date Apr 29, 2014
- United Technologies Corporation
- Nagendra Somanath
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Abrasive coated preform for a turbine blade tip
- Patent number 8,616,847
- Issue date Dec 31, 2013
- SIEMENS ENERGY, INC.
- David B. Allen
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Propulsion unit for aircraft with heat exchanger having front inlet...
- Patent number 8,522,529
- Issue date Sep 3, 2013
- Airbus Operations SAS
- Jean-Marc Martinou
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Double padded finger seal
- Patent number 7,735,833
- Issue date Jun 15, 2010
- The University of Akron
- Minel J. Braun
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Thermal erosion test device and method for testing thermal protecti...
- Patent number 7,628,534
- Issue date Dec 8, 2009
- SNECMA Propulsion Solide
- Jean-Marc Deoclezian
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Tailorable design configuration topologies for aircraft engine mid-...
- Patent number 7,610,763
- Issue date Nov 3, 2009
- United Technologies Corporation
- Nagendra Somanath
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine blade turbulator cooling design
- Patent number 7,347,671
- Issue date Mar 25, 2008
- Kevin Dorling
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Mounting for variably settable stator blades in a compressor
- Patent number 5,061,152
- Issue date Oct 29, 1991
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation
- Daniel J. Marey
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Fan blade axial locking device
- Patent number 4,502,841
- Issue date Mar 5, 1985
- SNECMA
- Georges Kebedjis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Device to lock the blades of a turboblower and to fasten the front...
- Patent number 4,405,285
- Issue date Sep 20, 1983
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation, "S.N.E.C....
- Jean M. Surdi
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Annular three-dimensional structure usable in particular as reinfor...
- Patent number 4,254,599
- Issue date Mar 10, 1981
- Societe Europeenne de Propulsion
- Michel Maistre
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL

Patents Applicationslast 30 patents

Information Patent Application
DAMPER RING FOR REDUCING UNWANTED VIBRATIONS OF A BLISK, AS WELL AS...
- Publication number 20240240563
- Publication date Jul 18, 2024
- MTU Aero Engines AG
- Andreas HARTUNG
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
INLET FILTER HOUSING HAVING COMPONENTS INCLUDING PORTIONS OF FILTER...
- Publication number 20230193825
- Publication date Jun 22, 2023
- GENERAL ELECTRIC COMPANY
- Laxmikant Merchant
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DUCTED INLET FOR REDUCING FLOW OSCILLATIONS
- Publication number 20220195878
- Publication date Jun 23, 2022
- The Boeing Company
- Zachariah B. VanDeMark
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
CENTRALIZED OIL DISTRIBUTION SYSTEM
- Publication number 20220178304
- Publication date Jun 9, 2022
- Daniella Sladen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INLET FILTER HOUSING HAVING COMPONENTS INCLUDING PORTIONS OF FILTER...
- Publication number 20220082051
- Publication date Mar 17, 2022
- GENERAL ELECTRIC COMPANY
- Laxmikant Merchant
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES
- Publication number 20200024987
- Publication date Jan 23, 2020
- GENERAL ELECTRIC COMPANY
- Ronald Scott Bunker
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
TURBOMACHINE BLADE ASSEMBLY
- Publication number 20170335695
- Publication date Nov 23, 2017
- MTU Aero Engines AG
- Markus Schlemmer
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
SEAL-PLATE ANTI-ROTATION IN A STAGE OF A GAS TURBINE ENGINE
- Publication number 20170191370
- Publication date Jul 6, 2017
- Rolls-Royce plc
- John DAWSON
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
METHOD FOR PRODUCING AN ACOUSTIC TREATMENT PANEL
- Publication number 20130146393
- Publication date Jun 13, 2013
- Airbus Operations SAS
- Alain Porte
- B32 - LAYERED PRODUCTS
Information Patent Application
ABRASIVE COATED PREFORM FOR A TURBINE BLADE TIP
- Publication number 20120051934
- Publication date Mar 1, 2012
- David B. Allen
- C25 - ELECTROLYTIC OR ELECTROPHORETIC PROCESSES APPARATUS THEREFOR
Information Patent Application
TAILORABLE DESIGN CONFIGURATION TOPOLOGIES FOR AIRCRAFT ENGINE MID-...
- Publication number 20100008765
- Publication date Jan 14, 2010
- United Technologies Corporation
- Somanath Nagendra
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
ARTICLE HAVING A PROTECTIVE COATING AND METHODS
- Publication number 20090324401
- Publication date Dec 31, 2009
- GENERAL ELECTRIC COMPANY
- Eklavya Calla
- C23 - COATING METALLIC MATERIAL COATING MATERIAL WITH METALLIC MATERIAL CHEMI...
Information Patent Application
PROPULSION UNIT FOR AIRCRAFT AND AIRCRAFT COMPRISING AT LEAST ONE S...
- Publication number 20090025366
- Publication date Jan 29, 2009
- AIRBUS FRANCE
- Jean-Marc Martinou
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Thermal erosion test device and method for testing thermal protecti...
- Publication number 20080192799
- Publication date Aug 14, 2008
- SNECMA PROPULSION SOLIDE
- Jean-Marc Deoclezian
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Double Padded Finger Seal
- Publication number 20080122183
- Publication date May 29, 2008
- Minel J. BRAUN
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Tailorable design configuration topologies for aircraft engine mid-...
- Publication number 20070261411
- Publication date Nov 15, 2007
- United Technologies Corporation
- Somanath Nagendra
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turbine blade turbulator cooling design
- Publication number 20060120868
- Publication date Jun 8, 2006
- Kevin Dorling
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

parallelepipedal

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Inlet filter housing having components including portions of filter...

Ducted inlet for reducing flow oscillations

Turbomachine hollow blade

Centralized oil distribution system

Double walled stator housing

Thermal insulation features for gas turbine engines

Gas turbine blade

Blade ring segment for turbine section, turbine section having the...

Turbine airfoil with biased trailing edge cooling arrangement

Turbomachine blade assembly

Blade, cut-back of blade or vane and gas turbine having the same

Angled impingement inserts with cooling features

Hollow blade having internal damper

Shroud assembly for a turbine engine

Steam turbine rotor seal key member, related assembly and steam tur...

Reversible blade rotor seal

Brush seal

Brush seal

Method for producing an acoustic treatment panel

Tailorable design configuration topologies for aircraft engine mid-...

Abrasive coated preform for a turbine blade tip

Propulsion unit for aircraft with heat exchanger having front inlet...

Double padded finger seal

Thermal erosion test device and method for testing thermal protecti...

Tailorable design configuration topologies for aircraft engine mid-...

Turbine blade turbulator cooling design

Mounting for variably settable stator blades in a compressor

Fan blade axial locking device

Device to lock the blades of a turboblower and to fasten the front...

Annular three-dimensional structure usable in particular as reinfor...

Patents Applicationslast 30 patents

DAMPER RING FOR REDUCING UNWANTED VIBRATIONS OF A BLISK, AS WELL AS...

INLET FILTER HOUSING HAVING COMPONENTS INCLUDING PORTIONS OF FILTER...

DUCTED INLET FOR REDUCING FLOW OSCILLATIONS

CENTRALIZED OIL DISTRIBUTION SYSTEM

INLET FILTER HOUSING HAVING COMPONENTS INCLUDING PORTIONS OF FILTER...

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

TURBOMACHINE BLADE ASSEMBLY

SEAL-PLATE ANTI-ROTATION IN A STAGE OF A GAS TURBINE ENGINE

METHOD FOR PRODUCING AN ACOUSTIC TREATMENT PANEL

ABRASIVE COATED PREFORM FOR A TURBINE BLADE TIP

TAILORABLE DESIGN CONFIGURATION TOPOLOGIES FOR AIRCRAFT ENGINE MID-...

ARTICLE HAVING A PROTECTIVE COATING AND METHODS

PROPULSION UNIT FOR AIRCRAFT AND AIRCRAFT COMPRISING AT LEAST ONE S...

Thermal erosion test device and method for testing thermal protecti...

Double Padded Finger Seal

Tailorable design configuration topologies for aircraft engine mid-...

Turbine blade turbulator cooling design