of the piezoelectric type

Industry

CPC
B64C2027/7283

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Parent Industries

BPERFORMING OPERATIONS TRANSPORTING B64Aviation B64CAEROPLANES HELICOPTERS

Current Industry

B64C2027/7283of the piezoelectric type

Industries

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Patents Grantslast 30 patents

Information Patent Grant
Flap drive device and blades of rotary-wing aircraft
- Patent number 11,667,378
- Issue date Jun 6, 2023
- Seoul National University R&DB Foundation
- Sang Joon Shin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Actuator arrangement and control surface arrangement, especially fo...
- Patent number 9,631,711
- Issue date Apr 25, 2017
- EADS Deutschland GmbH
- Stefan Storm
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Electric circuit with power amplifier for piezoelectric actuators
- Patent number 9,484,843
- Issue date Nov 1, 2016
- Airbus Helicopters Deutschland GmbH
- Boris Grohmann
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Grant
Rotor blade with control flap
- Patent number 9,415,868
- Issue date Aug 16, 2016
- Airbus Helicopters Deutschland GmbH
- Rupert Pfaller
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Drive system for helicopters
- Patent number 9,004,395
- Issue date Apr 14, 2015
- EADS Deutschland GmbH
- Jean Botti
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Hybrid device for vibration control
- Patent number 8,210,469
- Issue date Jul 3, 2012
- Fred Nitzsche
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Elongated, torsion-deformable aerodynamic element
- Patent number 8,205,840
- Issue date Jun 26, 2012
- Office National d'Etudes et de Recherches Aerospatiales
- Hugues Mercier des Rochettes
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rotor blade for a rotary wing aircraft
- Patent number 8,162,607
- Issue date Apr 24, 2012
- Eurocopter Deutschland GmbH
- Boris Grohmann
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Sandwich-structure flat actuator and application to structural torsion
- Patent number 7,726,603
- Issue date Jun 1, 2010
- Onera (Office National D'Etudes et de Recherches Aerospatiales)
- Hugues Mercier Des Rochettes
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Deformable aerodynamic profile
- Patent number 7,717,373
- Issue date May 18, 2010
- EADS Deutschland GmbH
- Peter Jaenker
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Piezoelectric extension actuator
- Patent number 7,453,185
- Issue date Nov 18, 2008
- EADS Deutschland GmbH
- Marius Bebesel
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Composite structural member having an integrated electrical circuit
- Patent number 7,391,622
- Issue date Jun 24, 2008
- The Boeing Company
- Joseph A. Marshall
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Grant
Method of manufacturing a composite structural member having an int...
- Patent number 7,281,318
- Issue date Oct 16, 2007
- The Boeing Company
- Joseph A. Marshall
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Grant
Piezoelectric actuating device for controlling the flaps on the rot...
- Patent number 6,717,333
- Issue date Apr 6, 2004
- EADS Deutschland GmbH
- Frank Hermle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method and control arrangement for adjusting a flap that is pivotal...
- Patent number 6,648,599
- Issue date Nov 18, 2003
- Eurocopter Deutschland GmbH
- Dieter Preissler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Piezoelectric actuators for circulation controlled rotorcraft
- Patent number 6,425,553
- Issue date Jul 30, 2002
- West Virginia University
- James E. Smith
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aerodynamic component with a leading edge flap
- Patent number 6,371,415
- Issue date Apr 16, 2002
- DaimlerChrysler AG
- Thomas Lorkowski
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rotor blade flap driving apparatus
- Patent number 6,273,681
- Issue date Aug 14, 2001
- Advanced Technology Institute of Commuter-Helicopter, Ltd.
- Eiichi Yamakawa
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Active flaperon assembly
- Patent number 6,247,670
- Issue date Jun 19, 2001
- Ramot University Authority for Applied Research and Industrial Development Ltd.
- Shaul Eliahou-Niv
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Airfoil member with a piezoelectrically actuated servo-flap
- Patent number 6,231,013
- Issue date May 15, 2001
- DaimlerChrysler AG
- Peter Jaenker
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method for producing a composite structure including a piezoelectri...
- Patent number 6,162,313
- Issue date Dec 19, 2000
- Eurocopter Deutschland GmbH
- Horst Bansemir
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Helicopter rotor blade flap actuator government interest
- Patent number 6,135,713
- Issue date Oct 24, 2000
- The McDonnell Douglas Helicopter Company
- David B. Domzalski
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Profile edge of an aerodynamic profile
- Patent number 6,076,776
- Issue date Jun 20, 2000
- Deutsches Zentrum fur Luft-und Raumfahrt E.V.
- Elmar J. Breitbach
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
High-efficiency, large stroke electromechanical actuator
- Patent number 5,907,211
- Issue date May 25, 1999
- Massachusetts Institute of Technology
- Steven R. Hall
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Thermostatic metal actuator for nozzle actuation
- Patent number 5,788,181
- Issue date Aug 4, 1998
- McDonnell Douglas Helicopter Co.
- John C. Wilson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rotor blade
- Patent number 5,730,581
- Issue date Mar 24, 1998
- Deutsche Forschungsanstalt fur Luft-und Raumfahrt e.V.
- Andreas Buter
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Piezoelectric actuator
- Patent number 5,626,312
- Issue date May 6, 1997
- McDonnell Douglas Corporation
- Robert E. Head
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method and apparatus for structural, actuation and sensing in a des...
- Patent number 5,440,193
- Issue date Aug 8, 1995
- University of Maryland
- Ronald M. Barrett
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Piezoelectric helicopter blade flap actuator
- Patent number 5,224,826
- Issue date Jul 6, 1993
- Massachusetts Institute of Technology
- Steven R. Hall
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
FLAP DRIVE DEVICE AND BLADES OF ROTARY-WING AIRCRAFT
- Publication number 20220024570
- Publication date Jan 27, 2022
- Seoul National University R&DB Foundation
- Sang Joon SHIN
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
High Authority Stability and Control Augmentation System
- Publication number 20180157275
- Publication date Jun 7, 2018
- BELL HELICOPTER TEXTRON INC.
- Brady G. Atkins
- G05 - CONTROLLING REGULATING
Information Patent Application
ROTOR BLADE WITH CONTROL FLAP
- Publication number 20140234104
- Publication date Aug 21, 2014
- AIRBUS HELICOPTERS DEUTSCHLAND GMBH
- Rupert PFALLER
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ACTUATOR ARRANGEMENT AND CONTROL SURFACE ARRANGEMENT, ESPECIALLY FO...
- Publication number 20140217235
- Publication date Aug 7, 2014
- EADS Deutschland GmbH
- Stefan Storm
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ELECTRIC CIRCUIT WITH POWER AMPLIFIER FOR PIEZOELETRIC ACTUATORS
- Publication number 20140132113
- Publication date May 15, 2014
- EADS DEUTSCHLAND GMBH
- Boris Grohmann
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
DRIVE SYSTEM FOR HELICOPTERS
- Publication number 20130119185
- Publication date May 16, 2013
- Eurocopter Deutschland GmbH
- Jean Botti
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ELONGATED, TORSION-DEFORMABLE AERODYNAMIC ELEMENT
- Publication number 20100258680
- Publication date Oct 14, 2010
- ONERA (Office National d'Etudes et de Recherches Aérospatiales)
- Hugues Mercier Des Rochettes
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
ROTOR BLADE FOR A ROTARY WING AIRCRAFT
- Publication number 20100181415
- Publication date Jul 22, 2010
- Eurocopter Deutschland GmbH
- Andree Altmikus
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
HYBRID DEVICE FOR VIBRATION CONTROL
- Publication number 20090321555
- Publication date Dec 31, 2009
- Fred NITZSCHE
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
ROTOR BLADE FOR A ROTARY WING AIRCRAFT
- Publication number 20090269198
- Publication date Oct 29, 2009
- Eurocopter Deutschland GmbH
- Boris Grohmann
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Composite structural member having an integrated electrical circuit
- Publication number 20070298663
- Publication date Dec 27, 2007
- The Boeing Company
- Joseph A. Marshall
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Application
Sandwich-structure flat actuator and application to structural torsion
- Publication number 20070205332
- Publication date Sep 6, 2007
- ONERA
- Hugues Mercier Des Rochettes
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Deformable aerodynamic profile
- Publication number 20060214065
- Publication date Sep 28, 2006
- EADS Deutschland GmbH
- Peter Jaenker
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Apparatus and methods for structurally-integrated conductive condui...
- Publication number 20060049302
- Publication date Mar 9, 2006
- Dennis K. Kennedy
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Structurally integrated circuit and associated method
- Publication number 20050257956
- Publication date Nov 24, 2005
- The Boeing Company
- Joseph A. Marshall
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Application
Piezoelectric extension actuator
- Publication number 20040070311
- Publication date Apr 15, 2004
- Marius Bebesel
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Piezoelectric actuating device for controlling the flaps on the rot...
- Publication number 20030137218
- Publication date Jul 24, 2003
- Frank Hermle
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Method and control arrangement for adjusting a flap that is pivotal...
- Publication number 20020141867
- Publication date Oct 3, 2002
- Eurocopter Deutschland GmbH
- Dieter Preissler
- B64 - AIRCRAFT AVIATION COSMONAUTICS

of the piezoelectric type

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Flap drive device and blades of rotary-wing aircraft

Actuator arrangement and control surface arrangement, especially fo...

Electric circuit with power amplifier for piezoelectric actuators

Rotor blade with control flap

Drive system for helicopters

Hybrid device for vibration control

Elongated, torsion-deformable aerodynamic element

Rotor blade for a rotary wing aircraft

Sandwich-structure flat actuator and application to structural torsion

Deformable aerodynamic profile

Piezoelectric extension actuator

Composite structural member having an integrated electrical circuit

Method of manufacturing a composite structural member having an int...

Piezoelectric actuating device for controlling the flaps on the rot...

Method and control arrangement for adjusting a flap that is pivotal...

Piezoelectric actuators for circulation controlled rotorcraft

Aerodynamic component with a leading edge flap

Rotor blade flap driving apparatus

Active flaperon assembly

Airfoil member with a piezoelectrically actuated servo-flap

Method for producing a composite structure including a piezoelectri...

Helicopter rotor blade flap actuator government interest

Profile edge of an aerodynamic profile

High-efficiency, large stroke electromechanical actuator

Thermostatic metal actuator for nozzle actuation

Rotor blade

Piezoelectric actuator

Method and apparatus for structural, actuation and sensing in a des...

Piezoelectric helicopter blade flap actuator

Patents Applicationslast 30 patents

FLAP DRIVE DEVICE AND BLADES OF ROTARY-WING AIRCRAFT

High Authority Stability and Control Augmentation System

ROTOR BLADE WITH CONTROL FLAP

ACTUATOR ARRANGEMENT AND CONTROL SURFACE ARRANGEMENT, ESPECIALLY FO...

ELECTRIC CIRCUIT WITH POWER AMPLIFIER FOR PIEZOELETRIC ACTUATORS

DRIVE SYSTEM FOR HELICOPTERS

ELONGATED, TORSION-DEFORMABLE AERODYNAMIC ELEMENT

ROTOR BLADE FOR A ROTARY WING AIRCRAFT

HYBRID DEVICE FOR VIBRATION CONTROL

ROTOR BLADE FOR A ROTARY WING AIRCRAFT

Composite structural member having an integrated electrical circuit

Sandwich-structure flat actuator and application to structural torsion

Deformable aerodynamic profile

Apparatus and methods for structurally-integrated conductive condui...

Structurally integrated circuit and associated method

Piezoelectric extension actuator

Piezoelectric actuating device for controlling the flaps on the rot...

Method and control arrangement for adjusting a flap that is pivotal...