by influencing fluid flow by heating using other means than combustion

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CPC
B64C2230/10

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

Current Industry

B64C2230/10by influencing fluid flow by heating using other means than combustion

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Patents Grantslast 30 patents

Information Patent Grant
Shock wave suppression device and aircraft
- Patent number 11,530,029
- Issue date Dec 20, 2022
- Mitsubishi Heavy Industries, Ltd.
- Mayuko Nagashiki
- 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
Control of hypersonic boundary layer transition
- Patent number 10,953,979
- Issue date Mar 23, 2021
- The Arizona Board of Regents on behalf of the University of Arizona
- Hermann F. Fasel
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
Leading edge ice-protection system
- Patent number 10,569,888
- Issue date Feb 25, 2020
- Airbus Operations GmbH
- Florian Lorenz
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Thermally controlled active flow control system
- Patent number 10,086,927
- Issue date Oct 2, 2018
- The Boeing Company
- Arvin Shmilovich
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Optical window system with aero-optical conductive blades
- Patent number 10,023,290
- Issue date Jul 17, 2018
- Raytheon Company
- David A. Vasquez
- F42 - AMMUNITION BLASTING
Information Patent Grant
Thermal actuation of riblets
- Patent number 9,764,824
- Issue date Sep 19, 2017
- The Boeing Company
- Weidong Song
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Grant
Method and apparatus for reducing turbulent skin friction
- Patent number 4,932,612
- Issue date Jun 12, 1990
- Ron F. Blackwelder
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
SHOCK WAVE SUPPRESSION DEVICE AND AIRCRAFT
- Publication number 20210253226
- Publication date Aug 19, 2021
- Mitsubishi Heavy Industries, Ltd.
- Mayuko NAGASHIKI
- 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
LEADING EDGE ICE-PROTECTION SYSTEM
- Publication number 20180170557
- Publication date Jun 21, 2018
- AIRBUS OPERATIONS GMBH
- Florian LORENZ
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
OPTICAL WINDOW SYSTEM WITH AERO-OPTICAL CONDUCTIVE BLADES
- Publication number 20170341726
- Publication date Nov 30, 2017
- Raytheon Company
- David A. Vasquez
- B32 - LAYERED PRODUCTS
Information Patent Application
Thermally Controlled Active Flow Control System
- Publication number 20170297680
- Publication date Oct 19, 2017
- The Boeing Company
- Arvin Shmilovich
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
BOUNDARY LAYER CONTROL ASSEMBLY FOR AN AIRCRAFT AIRFOIL AND METHOD...
- Publication number 20160221664
- Publication date Aug 4, 2016
- Hamilton Sundstrand Corporation
- Ray-Sing Lin
- B64 - AIRCRAFT AVIATION COSMONAUTICS

by influencing fluid flow by heating using other means than combustion

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Shock wave suppression device and aircraft

Thermally controlled active flow control system

Control of hypersonic boundary layer transition

Aircraft cabin noise reduction systems and methods

Leading edge ice-protection system

Thermally controlled active flow control system

Optical window system with aero-optical conductive blades

Thermal actuation of riblets

Method and apparatus for reducing turbulent skin friction

Patents Applicationslast 30 patents

SHOCK WAVE SUPPRESSION DEVICE AND AIRCRAFT

Thermally Controlled Active Flow Control System

LEADING EDGE ICE-PROTECTION SYSTEM

OPTICAL WINDOW SYSTEM WITH AERO-OPTICAL CONDUCTIVE BLADES

Thermally Controlled Active Flow Control System

BOUNDARY LAYER CONTROL ASSEMBLY FOR AN AIRCRAFT AIRFOIL AND METHOD...