by using a surface having multiple apertures of relatively small openings other than slots

Industry

CPC
B64C2230/22

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Parent Industries

BPERFORMING OPERATIONS TRANSPORTING B64Aviation B64CAEROPLANES HELICOPTERS B64C2230/00Boundary layer controls

Current Industry

B64C2230/22by using a surface having multiple apertures of relatively small openings other than slots

Industries

Patents Grantslast 30 patents

Information Patent Grant
Active drag control system for an aircraft
- Patent number 12,129,018
- Issue date Oct 29, 2024
- Airbus Operations Limited
- Henry Edwards
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Flow body for a vehicle and method for manufacturing a flow body
- Patent number 11,866,172
- Issue date Jan 9, 2024
- Airbus Defence and Space GmbH
- Florian Mayer
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Grant
Performance evaluation system of an aircraft component
- Patent number 11,845,538
- Issue date Dec 19, 2023
- Airbus Defence and Space GmbH
- Christian Herrles
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Apparatus and method for heating an aircraft structure
- Patent number 11,667,388
- Issue date Jun 6, 2023
- Airbus Operations Limited
- Henry Edwards
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Ice protection and boundary layer suction system for an aircraft ae...
- Patent number 11,667,387
- Issue date Jun 6, 2023
- Sonaca S.A.
- Said Elmouden
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Noise attenuation panel
- Patent number 11,591,065
- Issue date Feb 28, 2023
- Fokker Aerostructures B.V.
- Marcel Roggeveen
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Vertical tail unit for flow control
- Patent number 11,565,795
- Issue date Jan 31, 2023
- Airbus Operations GmbH
- Thomas Heuer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft structure for flow control
- Patent number 11,541,991
- Issue date Jan 3, 2023
- Airbus Operations GmbH
- Dort Daandels
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
Active control flow system and method of cooling and providing acti...
- Patent number 11,525,388
- Issue date Dec 13, 2022
- Pratt & Whitney Canada Corp.
- Jean Thomassin
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Aerofoil leading edge structures
- Patent number 11,453,481
- Issue date Sep 27, 2022
- Airbus Operations Limited
- David Andrew Phipps
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Active laminar flow control system with composite panel
- Patent number 11,433,990
- Issue date Sep 6, 2022
- Rohr, Inc.
- Pablo T. Sanz Martinez
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
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
Flow guide body for an aircraft
- Patent number 11,358,707
- Issue date Jun 14, 2022
- Airbus Operations GmbH
- Bruno Stefes
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Leading edge structure for a flow control system of an aircraft
- Patent number 11,220,345
- Issue date Jan 11, 2022
- Airbus Operations GmbH
- Christian Heck
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aerodynamic body having perforated skin
- Patent number 11,186,358
- Issue date Nov 30, 2021
- Airbus Operations Limited
- Ching-Yu Hui
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Apparatus and method for heating an aircraft structure
- Patent number 11,174,032
- Issue date Nov 16, 2021
- Airbus Operations Limited
- Henry Edwards
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Leading edge structure for a flow control system of an aircraft
- Patent number 11,155,342
- Issue date Oct 26, 2021
- Airbus Operations GmbH
- Alexander Büscher
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Apparatus for laminar flow control
- Patent number 11,142,296
- Issue date Oct 12, 2021
- Airbus Operations Limited
- Vernon Holmes
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Grant
Leading edge structure for a flow control system of an aircraft
- Patent number 11,040,769
- Issue date Jun 22, 2021
- Airbus Operations GmbH
- Geza Schrauf
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Vertical tail unit for flow control
- Patent number 10,974,817
- Issue date Apr 13, 2021
- Airbus Operations GmbH
- Thomas Heuer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Vertical tail unit for flow control
- Patent number 10,967,955
- Issue date Apr 6, 2021
- Airbus Operations GmbH
- Thomas Heuer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Flow body, method for manufacturing a flow body and aircraft having...
- Patent number 10,814,962
- Issue date Oct 27, 2020
- Airbus Operations GmbH
- Martin Gerber
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Boundary-layer-influencing aerodynamic part and method for producin...
- Patent number 10,723,443
- Issue date Jul 28, 2020
- Airbus Operations GmbH
- Bernd Ruppert
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Simplified fluidic oscillator for controlling aerodynamics of an ai...
- Patent number 10,717,519
- Issue date Jul 21, 2020
- The Boeing Company
- Matthew T. Lakebrink
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Heat exchanger for laminar-flow aircraft
- Patent number 10,618,636
- Issue date Apr 14, 2020
- Parker-Hannifin Corporation
- Carsten Ralf Mehring
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Grant
Aircraft cabin noise reduction systems and methods
- Patent number 10,611,458
- Issue date Apr 7, 2020
- The Boeing Company
- Brian J. Tillotson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Laminar flow panel
- Patent number 10,556,670
- Issue date Feb 11, 2020
- The Boeing Company
- Henry J. Koppelman
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Tile assembly
- Patent number 10,556,671
- Issue date Feb 11, 2020
- BAE Systems plc
- Clyde Warsop
- B63 - SHIPS OR OTHER WATERBORNE VESSELS RELATED EQUIPMENT

Patents Applicationslast 30 patents

Information Patent Application
MOVABLE AERODYNAMIC SURFACE FOR AN AIRCRAFT
- Publication number 20220306273
- Publication date Sep 29, 2022
- AIRBUS OPERATIONS GMBH
- Alexander BÜSCHER
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ACTIVE DRAG CONTROL SYSTEM FOR AN AIRCRAFT
- Publication number 20220274688
- Publication date Sep 1, 2022
- AIRBUS OPERATIONS LIMITED
- Henry Edwards
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
PERFORMANCE EVALUATION SYSTEM OF AN AIRCRAFT COMPONENT
- Publication number 20220097829
- Publication date Mar 31, 2022
- Christian HERRLES
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
APPARATUS AND METHOD FOR HEATING AN AIRCRAFT STRUCTURE
- Publication number 20220041289
- Publication date Feb 10, 2022
- AIRBUS OPERATIONS LIMITED
- Henry EDWARDS
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
VERTICAL TAIL UNIT FOR FLOW CONTROL
- Publication number 20210214072
- Publication date Jul 15, 2021
- AIRBUS OPERATIONS GMBH
- Thomas Heuer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT STRUCTURE FOR FLOW CONTROL
- Publication number 20200290730
- Publication date Sep 17, 2020
- AIRBUS OPERATIONS GMBH
- Dort DAANDELS
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AEROFOIL LEADING EDGE STRUCTURES
- Publication number 20200283158
- Publication date Sep 10, 2020
- AIRBUS OPERATIONS LIMITED
- David Andrew PHIPPS
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
Flow Guide Body For An Aircraft
- Publication number 20200102066
- Publication date Apr 2, 2020
- AIRBUS OPERATIONS GMBH
- Bruno Stefes
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Application
AERODYNAMIC BODY
- Publication number 20200055591
- Publication date Feb 20, 2020
- AIRBUS OPERATIONS LIMITED
- Ching-Yu HUI
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Wave-Shaped Acoustic Insert and Core
- Publication number 20190185171
- Publication date Jun 20, 2019
- The Boeing Company
- Kanika Gakhar
- B32 - LAYERED PRODUCTS
Information Patent Application
SIMPLIFIED FLUIDIC OSCILLATOR FOR CONTROLING AERODYNAMICS OF AN AIR...
- Publication number 20190152584
- Publication date May 23, 2019
- The Boeing Company
- Matthew T. Lakebrink
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
APPARATUS FOR LAMINAR FLOW CONTROL
- Publication number 20190118923
- Publication date Apr 25, 2019
- AIRBUS OPERATIONS LIMITED
- Vernon HOLMES
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
VERTICAL TAIL UNIT FOR FLOW CONTROL
- Publication number 20190106202
- Publication date Apr 11, 2019
- AIRBUS OPERATIONS GMBH
- Thomas Heuer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ACTIVE CONTROL FLOW SYSTEM AND METHOD OF COOLING AND PROVIDING ACTI...
- Publication number 20190107039
- Publication date Apr 11, 2019
- Pratt & Whitney Canada Corp.
- Jean THOMASSIN
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
VERTICAL TAIL UNIT FOR FLOW CONTROL
- Publication number 20190106201
- Publication date Apr 11, 2019
- AIRBUS OPERATIONS GMBH
- Thomas Heuer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
DUCTS FOR LAMINAR FLOW CONTROL SYSTEMS
- Publication number 20190092456
- Publication date Mar 28, 2019
- AIRBUS OPERATIONS LIMITED
- David Michael SAWYERS
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
LEADING EDGE STRUCTURE FOR A FLOW CONTROL SYSTEM OF AN AIRCRAFT
- Publication number 20190016444
- Publication date Jan 17, 2019
- AIRBUS OPERATIONS GMBH
- Geza SCHRAUF
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
CONTROL SURFACE COMPONENT FOR A HIGH-LIFT DEVICE OF AN AIRCRAFT AND...
- Publication number 20180148163
- Publication date May 31, 2018
- AIRBUS DEFENCE AND SPACE GMBH
- Michael Bauer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
NACELLE AND METHOD FOR INFLUENCING FLUID FLOWS IN A NACELLE
- Publication number 20180010518
- Publication date Jan 11, 2018
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Jens ORTMANNS
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
BOUNDARY-LAYER-INFLUENCING AERODYNAMIC PART AND METHOD FOR PRODUCIN...
- Publication number 20170267332
- Publication date Sep 21, 2017
- AIRBUS OPERATIONS GMBH
- Bernd RUPPERT
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
TILE ASSEMBLY
- Publication number 20170001715
- Publication date Jan 5, 2017
- BAE Systems plc
- Clyde WARSOP
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
HEAT EXCHANGER FOR LAMINAR-FLOW AIRCRAFT
- Publication number 20160332724
- Publication date Nov 17, 2016
- Parker-Hannifin Corporation
- Carsten Ralf Mehring
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
OPTIMIZED NACELLE PROFILE AND PLENUM SHAPE FOR BOUNDARY LAYER INGES...
- Publication number 20160311520
- Publication date Oct 27, 2016
- Rohr, Inc.
- Ann E. Khidekel
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
HIGH-LIFT DEVICE OF FLIGHT VEHICLE
- Publication number 20160194073
- Publication date Jul 7, 2016
- The society of Japanese Aerospace Companies
- Kazuhide Isotani
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Laminar Flow Panel
- Publication number 20160159465
- Publication date Jun 9, 2016
- The Boeing Company
- Henry J. Koppelman
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Laminar Flow Panel
- Publication number 20140326834
- Publication date Nov 6, 2014
- Henry J. Koppelman
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
PROFILE PLATE PORTION FOR USE AS AN OUTER WALL OF A FLOW BODY, METH...
- Publication number 20140021304
- Publication date Jan 23, 2014
- AIRBUS OPERATIONS GMBH
- Martin Gerber
- B64 - AIRCRAFT AVIATION COSMONAUTICS

by using a surface having multiple apertures of relatively small openings other than slots

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Active drag control system for an aircraft

Flow body for a vehicle and method for manufacturing a flow body

Performance evaluation system of an aircraft component

Apparatus and method for heating an aircraft structure

Ice protection and boundary layer suction system for an aircraft ae...

Noise attenuation panel

Vertical tail unit for flow control

Aircraft structure for flow control

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

Active control flow system and method of cooling and providing acti...

Aerofoil leading edge structures

Active laminar flow control system with composite panel

Active laminar flow control plenum panel arrangement

Active laminar flow control structural plenums fastened

Flow guide body for an aircraft

Leading edge structure for a flow control system of an aircraft

Aerodynamic body having perforated skin

Apparatus and method for heating an aircraft structure

Leading edge structure for a flow control system of an aircraft

Apparatus for laminar flow control

Leading edge structure for a flow control system of an aircraft

Vertical tail unit for flow control

Vertical tail unit for flow control

Flow body, method for manufacturing a flow body and aircraft having...

Boundary-layer-influencing aerodynamic part and method for producin...

Simplified fluidic oscillator for controlling aerodynamics of an ai...

Heat exchanger for laminar-flow aircraft

Aircraft cabin noise reduction systems and methods

Laminar flow panel

Tile assembly

Patents Applicationslast 30 patents

MOVABLE AERODYNAMIC SURFACE FOR AN AIRCRAFT

ACTIVE DRAG CONTROL SYSTEM FOR AN AIRCRAFT

PERFORMANCE EVALUATION SYSTEM OF AN AIRCRAFT COMPONENT

APPARATUS AND METHOD FOR HEATING AN AIRCRAFT STRUCTURE

VERTICAL TAIL UNIT FOR FLOW CONTROL

AIRCRAFT STRUCTURE FOR FLOW CONTROL

AEROFOIL LEADING EDGE STRUCTURES

ACTIVE LAMINAR FLOW CONTROL STRUCTURAL PLENUMS FASTENED

ACTIVE LAMINAR FLOW CONTROL PLENUM PANEL ARRANGEMENT

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

Flow Guide Body For An Aircraft

AERODYNAMIC BODY

Wave-Shaped Acoustic Insert and Core

SIMPLIFIED FLUIDIC OSCILLATOR FOR CONTROLING AERODYNAMICS OF AN AIR...

APPARATUS FOR LAMINAR FLOW CONTROL

VERTICAL TAIL UNIT FOR FLOW CONTROL

ACTIVE CONTROL FLOW SYSTEM AND METHOD OF COOLING AND PROVIDING ACTI...

VERTICAL TAIL UNIT FOR FLOW CONTROL

DUCTS FOR LAMINAR FLOW CONTROL SYSTEMS

LEADING EDGE STRUCTURE FOR A FLOW CONTROL SYSTEM OF AN AIRCRAFT

CONTROL SURFACE COMPONENT FOR A HIGH-LIFT DEVICE OF AN AIRCRAFT AND...

NACELLE AND METHOD FOR INFLUENCING FLUID FLOWS IN A NACELLE

BOUNDARY-LAYER-INFLUENCING AERODYNAMIC PART AND METHOD FOR PRODUCIN...

TILE ASSEMBLY

HEAT EXCHANGER FOR LAMINAR-FLOW AIRCRAFT

OPTIMIZED NACELLE PROFILE AND PLENUM SHAPE FOR BOUNDARY LAYER INGES...

HIGH-LIFT DEVICE OF FLIGHT VEHICLE

Laminar Flow Panel

Laminar Flow Panel

PROFILE PLATE PORTION FOR USE AS AN OUTER WALL OF A FLOW BODY, METH...