comprising boundary layer control means

Industry

CPC
B64D2033/0226

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Parent Industries

BPERFORMING OPERATIONS TRANSPORTING B64Aviation B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT

Current Industry

B64D2033/0226comprising boundary layer control means

Industries

Patents Grantslast 30 patents

Information Patent Grant
Aircraft with bifurcated air inlet
- Patent number 12,208,909
- Issue date Jan 28, 2025
- Textron Innovations Inc.
- Steven Ray Ivans
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Apparatus for ingesting boundary layer flow for an aircraft
- Patent number 12,168,506
- Issue date Dec 17, 2024
- JETZERO, INC.
- Mark Allan Page
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Cantilevered airfoils and methods of forming the same
- Patent number 12,104,501
- Issue date Oct 1, 2024
- General Electric Company
- Nicholas J. Kray
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Multiple intake distortion adaptive fan for gas turbine engine
- Patent number 12,065,258
- Issue date Aug 20, 2024
- Rolls-Royce North American Technologies Inc.
- Robert W. Heeter
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Streamline airframe with boundary ingestion fluidic propulsive elem...
- Patent number 12,037,104
- Issue date Jul 16, 2024
- JETOPTERA, INC.
- Andrei Evulet
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Drag recovery scheme using boundary layer ingestion
- Patent number 11,975,819
- Issue date May 7, 2024
- JETZERO, INC.
- Mark Allan Page
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Airfoil for a turbofan engine
- Patent number 11,965,425
- Issue date Apr 23, 2024
- General Electric Company
- Trevor Howard Wood
- G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information Patent Grant
Methods and apparatus to control air flow separation of an engine
- Patent number 11,828,237
- Issue date Nov 28, 2023
- General Electric Company
- Sai Venkata Kathik Saripella
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Aircraft engine nacelle with an aft end major axis substantially pa...
- Patent number 11,772,806
- Issue date Oct 3, 2023
- Airbus Operations Limited
- Geoffrey Richard Williams
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Propulsion system for an aircraft
- Patent number 11,686,246
- Issue date Jun 27, 2023
- Gulfstream Aerospace Corporation
- Shawn Bennett
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Inlet cowl for a turbine engine
- Patent number 11,555,449
- Issue date Jan 17, 2023
- General Electric Company
- Mustafa Dindar
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Adaptable flow control for engine nacelles
- Patent number 11,542,866
- Issue date Jan 3, 2023
- The Boeing Company
- Bradley J. Rafferty
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Active laminar flow control plenum panel arrangements and installat...
- Patent number 11,524,770
- Issue date Dec 13, 2022
- Rohr, Inc.
- Pablo T. Sanz Martinez
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Nacelle for an aircraft aft fan
- Patent number 11,518,499
- Issue date Dec 6, 2022
- General Electric Company
- Kishore Ramakrishnan
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Embedded engines in hybrid blended wing body
- Patent number 11,498,660
- Issue date Nov 15, 2022
- Raytheon Technologies Corporation
- Razvan Virgil Florea
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Deployable assembly for a propulsor
- Patent number 11,485,481
- Issue date Nov 1, 2022
- General Electric Company
- Lawrence Chih-Hui Cheung
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Flush fluid inlet designs for aero-acoustic tone mitigation of airc...
- Patent number 11,486,306
- Issue date Nov 1, 2022
- The Boeing Company
- Garrett D. Klovdahl
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft including a ducted rear thruster with an input stator havi...
- Patent number 11,485,506
- Issue date Nov 1, 2022
- SAFRAN AIRCRAFT ENGINES
- Nicolas Jérôme Jean Tantot
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Aft engine nacelle shape for an aircraft
- Patent number 11,447,259
- Issue date Sep 20, 2022
- General Electric Company
- Patrick Michael Marrinan
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Active laminar flow control plenum panel arrangement
- Patent number 11,414,203
- Issue date Aug 16, 2022
- Rohr, Inc.
- Pablo T. Sanz Martinez
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Drag recovery scheme using boundary layer ingestion
- Patent number 11,396,365
- Issue date Jul 26, 2022
- Blended Wing Aircraft, Inc.
- Mark Allan Page
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Active laminar flow control structural plenums fastened
- Patent number 11,396,366
- Issue date Jul 26, 2022
- Rohr, Inc.
- Pablo T. Sanz Martinez
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Systems and methods for hybrid electric gas turbine engines
- Patent number 11,377,219
- Issue date Jul 5, 2022
- Raytheon Technologies Corporation
- Daniel Kupratis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Flight vehicle engine with finned inlet
- Patent number 11,204,000
- Issue date Dec 21, 2021
- Raytheon Company
- Timothy F. O'Brien
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Electric propulsion engine for an aircraft
- Patent number 11,097,850
- Issue date Aug 24, 2021
- General Electric Company
- Daniel Alan Niergarth
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft incorporating a thrust recovery system using cabin air
- Patent number 11,085,312
- Issue date Aug 10, 2021
- Airbus Operations S.L.
- Javier Fraile Martin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Flight vehicle engine inlet with internal diverter, and method of c...
- Patent number 11,053,018
- Issue date Jul 6, 2021
- Raytheon Company
- Timothy F. O'Brien
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Thermally controlled active flow control system
- Patent number 10,988,240
- Issue date Apr 27, 2021
- The Boeing Company
- Arvin Shmilovich
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
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
Engine nacelle for an aircraft
- Patent number 10,974,813
- Issue date Apr 13, 2021
- General Electric Company
- Mustafa Dindar
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
DRAG RECOVERY SCHEME USING BOUNDARY LAYER INGESTION
- Publication number 20240417082
- Publication date Dec 19, 2024
- JETZERO, INC.
- Mark Allan Page
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
STREAMLINE AIRFRAME WITH BOUNDARY INGESTON FLUIDIC PROPULSIVE ELEMENTS
- Publication number 20240367777
- Publication date Nov 7, 2024
- JETOPTERA, INC.
- Andrei Evulet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRFOIL FOR A TURBOFAN ENGINE
- Publication number 20240263565
- Publication date Aug 8, 2024
- GENERAL ELECTRIC COMPANY
- Trevor Howard Wood
- G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information Patent Application
MULTIPLE INTAKE DISTORTION ADAPTIVE FAN FOR GAS TURBINE ENGINE
- Publication number 20240246688
- Publication date Jul 25, 2024
- Rolls-Royce North American Technologies Inc.
- Robert W. Heeter
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET
- Publication number 20230080020
- Publication date Mar 16, 2023
- Jose S. Alonso-Miralles
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DRAG RECOVERY SCHEME USING BOUNDARY LAYER INGESTION
- Publication number 20220348315
- Publication date Nov 3, 2022
- Blended Wing Aircraft, Inc.
- Mark Allan Page
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
DRAG RECOVERY SCHEME USING BOUNDARY LAYER INGESTION
- Publication number 20220033067
- Publication date Feb 3, 2022
- Blended Wing Aircraft, Inc.
- Mark Allan Page
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FLUSH FLUID INLET DESIGNS FOR AERO-ACOUSTIC TONE MITIGATION OF AIRC...
- Publication number 20210394917
- Publication date Dec 23, 2021
- The Boeing Company
- Garrett D. Klovdahl
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT ENGINE NACELLE
- Publication number 20210316871
- Publication date Oct 14, 2021
- AIRBUS OPERATIONS LIMITED
- Geoffrey Richard WILLIAMS
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
INLET COWL FOR A TURBINE ENGINE
- Publication number 20210231054
- Publication date Jul 29, 2021
- GENERAL ELECTRIC COMPANY
- Mustafa Dindar
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
NACELLE FOR AN AIRCRAFT AFT FAN
- Publication number 20210107631
- Publication date Apr 15, 2021
- GENERAL ELECTRIC COMPANY
- Kishore Ramakrishnan
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
TANDEM FAN FOR BOUNDARY LAYER INGESTION SYSTEMS
- Publication number 20200248560
- Publication date Aug 6, 2020
- United Technologies Corporation
- Michael M. Joly
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
NACELLE INLET AND SYSTEM AND METHOD FOR MAKING SAME
- Publication number 20200130856
- Publication date Apr 30, 2020
- SPIRIT AEROSYSTEMS, INC
- Randall Ray West
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
ACTIVE LAMINAR FLOW CONTROL STRUCTURAL PLENUMS FASTENED
- Publication number 20200102082
- Publication date Apr 2, 2020
- Rohr, Inc.
- PABLO T. SANZ MARTINEZ
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ACTIVE LAMINAR FLOW CONTROL PLENUM PANEL ARRANGEMENT
- Publication number 20200102083
- Publication date Apr 2, 2020
- Rohr, Inc.
- PABLO T. SANZ MARTINEZ
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ACTIVE LAMINAR FLOW CONTROL PLENUM PANEL ARRANGEMENTS AND INSTALLAT...
- Publication number 20200102084
- Publication date Apr 2, 2020
- Rohr, Inc.
- PABLO T. SANZ MARTINEZ
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
PREDICTION OF INLET DISTORTION OF BOUNDARY LAYER INGESTING PROPULSI...
- Publication number 20200080477
- Publication date Mar 12, 2020
- United Technologies Corporation
- Michael Joseph Murphy
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Aft Engine Nacelle Shape for an Aircraft
- Publication number 20190329896
- Publication date Oct 31, 2019
- GENERAL ELECTRIC COMPANY
- Patrick Michael Marrinan
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METHODS AND APPARATUS TO MONITOR A SHOCK WAVE PROXIMATE A TRANSONIC...
- Publication number 20190291884
- Publication date Sep 26, 2019
- The Boeing Company
- Steve G. Mackin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
INLET DIFFUSERS FOR JET ENGINES, JET ENGINES, JET AIRCRAFT, AND MET...
- Publication number 20190284996
- Publication date Sep 19, 2019
- The Boeing Company
- Thuy Huynh
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Inlet Assembly for an Aircraft Aft Fan
- Publication number 20190234242
- Publication date Aug 1, 2019
- GENERAL ELECTRIC COMPANY
- Kishore Ramakrishnan
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
EMBEDDED ENGINES IN HYBRID BLENDED WING BODY
- Publication number 20190055006
- Publication date Feb 21, 2019
- United Technologies Corporation
- Razvan Virgil Florea
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
VARIABLE AND ADAPTABLE DIVERTERLESS BUMP INLET
- Publication number 20180354639
- Publication date Dec 13, 2018
- AIRBUS DEFENCE AND SPACE GMBH
- Thomas BERENS
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AFT FAN COUNTER-ROTATING TURBINE ENGINE
- Publication number 20180354637
- Publication date Dec 13, 2018
- United Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Thermally Controlled Active Flow Control System
- Publication number 20180346101
- Publication date Dec 6, 2018
- The Boeing Company
- Arvin Shmilovich
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
VARIABLE-GEOMETRY BOUNDARY LAYER DIVERTER
- Publication number 20180298829
- Publication date Oct 18, 2018
- United Technologies Corporation
- Wesley K. Lord
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
FLIGHT VEHICLE ENGINE WITH FINNED INLET
- Publication number 20180274486
- Publication date Sep 27, 2018
- Raytheon Company
- Timothy F. O'Brien
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
EMERGENCY POWER GENERATION VIA ELECTRICALLY DRIVEN TAIL CONE BOUNDA...
- Publication number 20180265213
- Publication date Sep 20, 2018
- HAMILTON SUNDSTRAND CORPORATION
- Richard A. Himmelmann
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIR INTAKE STRUCTURE AND AIRFLOW CONTROL SYSTEM
- Publication number 20180265208
- Publication date Sep 20, 2018
- Hani M. Saeed Yousef
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT INCLUDING A STREAMLINED REAR THRUSTER WITH AN INPUT STATOR...
- Publication number 20180209445
- Publication date Jul 26, 2018
- SAFRAN AIRCRAFT ENGINES
- Nicolas Jérôme Jean Tantot
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

comprising boundary layer control means

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Aircraft with bifurcated air inlet

Apparatus for ingesting boundary layer flow for an aircraft

Cantilevered airfoils and methods of forming the same

Multiple intake distortion adaptive fan for gas turbine engine

Streamline airframe with boundary ingestion fluidic propulsive elem...

Drag recovery scheme using boundary layer ingestion

Airfoil for a turbofan engine

Methods and apparatus to control air flow separation of an engine

Aircraft engine nacelle with an aft end major axis substantially pa...

Propulsion system for an aircraft

Inlet cowl for a turbine engine

Adaptable flow control for engine nacelles

Active laminar flow control plenum panel arrangements and installat...

Nacelle for an aircraft aft fan

Embedded engines in hybrid blended wing body

Deployable assembly for a propulsor

Flush fluid inlet designs for aero-acoustic tone mitigation of airc...

Aircraft including a ducted rear thruster with an input stator havi...

Aft engine nacelle shape for an aircraft

Active laminar flow control plenum panel arrangement

Drag recovery scheme using boundary layer ingestion

Active laminar flow control structural plenums fastened

Systems and methods for hybrid electric gas turbine engines

Flight vehicle engine with finned inlet

Electric propulsion engine for an aircraft

Aircraft incorporating a thrust recovery system using cabin air

Flight vehicle engine inlet with internal diverter, and method of c...

Thermally controlled active flow control system

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

Engine nacelle for an aircraft

Patents Applicationslast 30 patents

DRAG RECOVERY SCHEME USING BOUNDARY LAYER INGESTION

STREAMLINE AIRFRAME WITH BOUNDARY INGESTON FLUIDIC PROPULSIVE ELEMENTS

AIRFOIL FOR A TURBOFAN ENGINE

MULTIPLE INTAKE DISTORTION ADAPTIVE FAN FOR GAS TURBINE ENGINE

AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET

DRAG RECOVERY SCHEME USING BOUNDARY LAYER INGESTION

DRAG RECOVERY SCHEME USING BOUNDARY LAYER INGESTION

FLUSH FLUID INLET DESIGNS FOR AERO-ACOUSTIC TONE MITIGATION OF AIRC...

AIRCRAFT ENGINE NACELLE

INLET COWL FOR A TURBINE ENGINE

NACELLE FOR AN AIRCRAFT AFT FAN

TANDEM FAN FOR BOUNDARY LAYER INGESTION SYSTEMS

NACELLE INLET AND SYSTEM AND METHOD FOR MAKING SAME

ACTIVE LAMINAR FLOW CONTROL STRUCTURAL PLENUMS FASTENED

ACTIVE LAMINAR FLOW CONTROL PLENUM PANEL ARRANGEMENT

ACTIVE LAMINAR FLOW CONTROL PLENUM PANEL ARRANGEMENTS AND INSTALLAT...

PREDICTION OF INLET DISTORTION OF BOUNDARY LAYER INGESTING PROPULSI...

Aft Engine Nacelle Shape for an Aircraft

METHODS AND APPARATUS TO MONITOR A SHOCK WAVE PROXIMATE A TRANSONIC...

INLET DIFFUSERS FOR JET ENGINES, JET ENGINES, JET AIRCRAFT, AND MET...

Inlet Assembly for an Aircraft Aft Fan

EMBEDDED ENGINES IN HYBRID BLENDED WING BODY

VARIABLE AND ADAPTABLE DIVERTERLESS BUMP INLET

AFT FAN COUNTER-ROTATING TURBINE ENGINE

Thermally Controlled Active Flow Control System

VARIABLE-GEOMETRY BOUNDARY LAYER DIVERTER

FLIGHT VEHICLE ENGINE WITH FINNED INLET

EMERGENCY POWER GENERATION VIA ELECTRICALLY DRIVEN TAIL CONE BOUNDA...

AIR INTAKE STRUCTURE AND AIRFLOW CONTROL SYSTEM

AIRCRAFT INCLUDING A STREAMLINED REAR THRUSTER WITH AN INPUT STATOR...