Turbulent flow

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CPC
F05D2210/33

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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 F05D2210/00Working fluids

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F05D2210/33Turbulent flow

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Patents Grantslast 30 patents

Information Patent Grant
Turbine blade including pin-fin array
- Patent number 11,313,238
- Issue date Apr 26, 2022
- Ki Baek Kim
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Jet engine, flying object, and operation method of jet engine
- Patent number 11,248,562
- Issue date Feb 15, 2022
- Mitsubishi Heavy Industries, Ltd.
- Mariko Hirokane
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Spray nozzle
- Patent number 11,181,272
- Issue date Nov 23, 2021
- Rolls-Royce PLC
- Luca Tentorio
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Propulsion system using large scale vortex generators for flow redi...
- Patent number 10,981,659
- Issue date Apr 20, 2021
- Gulfstream Aerospace Corporation
- Michael Rybalko
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Isentropic compression inlet for supersonic aircraft
- Patent number 10,731,556
- Issue date Aug 4, 2020
- Gulfstream Aerospace Corporation
- Timothy R. Conners
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Airfoil having internal hybrid cooling cavities
- Patent number 10,633,980
- Issue date Apr 28, 2020
- UNITED TECHNOLOGIES COPRORATION
- Tracy A. Propheter-Hinckley
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Cooling flow for leading panel in a gas turbine engine combustor
- Patent number 10,344,979
- Issue date Jul 9, 2019
- United Technologies Corporation
- Frank J. Cunha
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Flow outlet
- Patent number 9,964,114
- Issue date May 8, 2018
- Rolls-Royce PLC
- Oliver C Taylor-Tibbott
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Propulsion system using large scale vortex generators for flow redi...
- Patent number 9,884,688
- Issue date Feb 6, 2018
- Gulfstream Aerospace Corporation
- Michael Rybalko
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Blade tip
- Patent number 9,850,764
- Issue date Dec 26, 2017
- Rolls-Royce PLC
- Ian Colin Deuchar Care
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Gas turbine engine combustor with fluidic control of swirlers
- Patent number 9,513,010
- Issue date Dec 6, 2016
- Honeywell International Inc.
- Raymond R. Tseng
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Dual-vortical-flow hybrid rocket engine
- Patent number 9,458,796
- Issue date Oct 4, 2016
- National Applied Research Laboratories
- Yen-Sen Chen
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine airfoil vane with an impingement insert having a plurality...
- Patent number 9,347,324
- Issue date May 24, 2016
- Siemens Aktiengesellschaft
- Ching-Pang Lee
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Impeller
- Patent number 9,051,837
- Issue date Jun 9, 2015
- Delta Electronics, Inc.
- Chun-Lung Chiu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Serpentine cooling circuit with T-shaped partitions in a turbine ai...
- Patent number 9,017,025
- Issue date Apr 28, 2015
- SIEMENS ENERGY, INC.
- Ching-Pang Lee
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine blade tip with vortex generators
- Patent number 8,690,536
- Issue date Apr 8, 2014
- SIEMENS ENERGY, INC.
- Alexander R. Beeck
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Combustor liner assembly with enhanced cooling system
- Patent number 8,667,801
- Issue date Mar 11, 2014
- SIEMENS ENERGY, INC.
- Carlos Roldan-Posada
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Cooling system having reduced mass pin fins for components in a gas...
- Patent number 8,668,453
- Issue date Mar 11, 2014
- SIEMENS ENERGY, INC.
- Ching-Pang Lee
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
TURBINE BLADE INCLUDING PIN-FIN ARRAY
- Publication number 20200095870
- Publication date Mar 26, 2020
- Doosan Heavy Industries & Construction Co., Ltd.
- Ki Baek KIM
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
BLOWER WITH INDENTATIONS
- Publication number 20190154058
- Publication date May 23, 2019
- Black & Decker Inc.
- Oleksiy SERGYEYENKO
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
AIRFOIL HAVING INTERNAL HYBRID COOLING CAVITIES
- Publication number 20190101010
- Publication date Apr 4, 2019
- United Technologies Corporation
- Tracy A. Propheter-Hinckley
- B22 - CASTING POWDER METALLURGY
Information Patent Application
SPRAY NOZZLE
- Publication number 20190078784
- Publication date Mar 14, 2019
- Rolls-Royce plc
- Luca TENTORIO
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
JET ENGINE, FLYING OBJECT, AND OPERATION METHOD OF JET ENGINE
- Publication number 20190032602
- Publication date Jan 31, 2019
- Mitsubishi Heavy Industries, Ltd.
- Mariko HIROKANE
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
PROPULSION SYSTEM USING LARGE SCALE VORTEX GENERATORS FOR FLOW REDI...
- Publication number 20180127106
- Publication date May 10, 2018
- GULFSTREAM AEROSPACE CORPORATION
- Michael Rybalko
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Cooling Flow for Leading Panel in a Gas Turbine Engine Combustor
- Publication number 20160327273
- Publication date Nov 10, 2016
- United Technologies Corporation
- Frank J. Cunha
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ISENTROPIC COMPRESSION INLET FOR SUPERSONIC AIRCRAFT
- Publication number 20160265433
- Publication date Sep 15, 2016
- GULFSTREAM AEROSPACE CORPORATION
- Timothy R. Conners
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
BLADE TIP
- Publication number 20150247411
- Publication date Sep 3, 2015
- Rolls-Royce plc
- Ian Colin Deuchar CARE
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
GAS TURBINE ENGINE COMBUSTOR WITH FLUIDIC CONTROL OF SWIRLERS
- Publication number 20150040572
- Publication date Feb 12, 2015
- Honeywell International Inc.
- Raymond R. Tseng
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Dual-Vortical-Flow Hybrid Rocket Engine
- Publication number 20140352276
- Publication date Dec 4, 2014
- National Chiao Tung University
- Yen-Sen Chen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD FOR CREATING A CONNECTING ELEMENT POSITIONED BETWEEN TWO COM...
- Publication number 20140311161
- Publication date Oct 23, 2014
- SNECMA
- Francois Robert Bellabal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PROPULSION SYSTEM USING LARGE SCALE VORTEX GENERATORS FOR FLOW REDI...
- Publication number 20140224940
- Publication date Aug 14, 2014
- GULFSTREAM AEROSPACE CORPORATION
- Michael Rybalko
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOCHARGER ASSEMBLY
- Publication number 20140186174
- Publication date Jul 3, 2014
- Speed of Air, Inc.
- Joey A. Malfa
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBINE AIRFOIL VANE WITH AN IMPINGEMENT INSERT HAVING A PLURALITY...
- Publication number 20140105726
- Publication date Apr 17, 2014
- Ching-Pang Lee
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
EXHAUST SYSTEM FOR GAS TURBINES
- Publication number 20130327052
- Publication date Dec 12, 2013
- Chris O'NEILL
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SERPENTINE COOLING CIRCUIT WITH T-SHAPED PARTITIONS IN A TURBINE AI...
- Publication number 20120269648
- Publication date Oct 25, 2012
- Ching-Pang Lee
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBINE BLADE WITH IMPROVED TRAILING EDGE COOLING
- Publication number 20120269649
- Publication date Oct 25, 2012
- Christopher Rawlings
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
IMPELLER
- Publication number 20120251323
- Publication date Oct 4, 2012
- CHUN-LUNG CHIU
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
COOLING SYSTEM HAVING REDUCED MASS PIN FINS FOR COMPONENTS IN A GAS...
- Publication number 20120207591
- Publication date Aug 16, 2012
- Ching-Pang Lee
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBINE BLADE TIP WITH VORTEX GENERATORS
- Publication number 20120076653
- Publication date Mar 29, 2012
- Alexander R. Beeck
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBINE AIRFOIL VANE WITH AN IMPINGEMENT INSERT HAVING A PLURALITY...
- Publication number 20120070302
- Publication date Mar 22, 2012
- Ching-Pang Lee
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
COMBUSTOR LINER ASSEMBLY WITH ENHANCED COOLING SYSTEM
- Publication number 20120055165
- Publication date Mar 8, 2012
- Carlos Roldan-Posada
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES

Turbulent flow

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Turbine blade including pin-fin array

Jet engine, flying object, and operation method of jet engine

Spray nozzle

Propulsion system using large scale vortex generators for flow redi...

Isentropic compression inlet for supersonic aircraft

Airfoil having internal hybrid cooling cavities

Cooling flow for leading panel in a gas turbine engine combustor

Flow outlet

Propulsion system using large scale vortex generators for flow redi...

Blade tip

Gas turbine engine combustor with fluidic control of swirlers

Dual-vortical-flow hybrid rocket engine

Turbine airfoil vane with an impingement insert having a plurality...

Impeller

Serpentine cooling circuit with T-shaped partitions in a turbine ai...

Turbine blade tip with vortex generators

Combustor liner assembly with enhanced cooling system

Cooling system having reduced mass pin fins for components in a gas...

Patents Applicationslast 30 patents

TURBINE BLADE INCLUDING PIN-FIN ARRAY

BLOWER WITH INDENTATIONS

AIRFOIL HAVING INTERNAL HYBRID COOLING CAVITIES

SPRAY NOZZLE

JET ENGINE, FLYING OBJECT, AND OPERATION METHOD OF JET ENGINE

PROPULSION SYSTEM USING LARGE SCALE VORTEX GENERATORS FOR FLOW REDI...

Cooling Flow for Leading Panel in a Gas Turbine Engine Combustor

ISENTROPIC COMPRESSION INLET FOR SUPERSONIC AIRCRAFT

BLADE TIP

GAS TURBINE ENGINE COMBUSTOR WITH FLUIDIC CONTROL OF SWIRLERS

Dual-Vortical-Flow Hybrid Rocket Engine

METHOD FOR CREATING A CONNECTING ELEMENT POSITIONED BETWEEN TWO COM...

PROPULSION SYSTEM USING LARGE SCALE VORTEX GENERATORS FOR FLOW REDI...

TURBOCHARGER ASSEMBLY

TURBINE AIRFOIL VANE WITH AN IMPINGEMENT INSERT HAVING A PLURALITY...

EXHAUST SYSTEM FOR GAS TURBINES

SERPENTINE COOLING CIRCUIT WITH T-SHAPED PARTITIONS IN A TURBINE AI...

TURBINE BLADE WITH IMPROVED TRAILING EDGE COOLING

IMPELLER

COOLING SYSTEM HAVING REDUCED MASS PIN FINS FOR COMPONENTS IN A GAS...

TURBINE BLADE TIP WITH VORTEX GENERATORS

TURBINE AIRFOIL VANE WITH AN IMPINGEMENT INSERT HAVING A PLURALITY...

COMBUSTOR LINER ASSEMBLY WITH ENHANCED COOLING SYSTEM