using one actuator per blade

Industry

CPC
B64C2027/7216

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Parent Industries

BPERFORMING OPERATIONS TRANSPORTING B64Aviation B64CAEROPLANES HELICOPTERS

Current Industry

B64C2027/7216using one actuator per blade

Industries

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Patents Grantslast 30 patents

Information Patent Grant
Helicopter with coaxial counter-rotating roller driven rotors
- Patent number 11,866,161
- Issue date Jan 9, 2024
- Charles Douglas Pope
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
System for reducing vibrations or stresses in a rotor blade system
- Patent number 11,702,195
- Issue date Jul 18, 2023
- AIRBUS HELICOPTERS TECHNIK GMBH
- Andre Hausberg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
System for reducing vibrations or stresses in a rotor blade system
- Patent number 11,091,253
- Issue date Aug 17, 2021
- ZF Friedrichshafen AG
- Andre Hausberg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Adjustment of track and balance of a multi-blade rotor
- Patent number 10,870,484
- Issue date Dec 22, 2020
- Airbus Helicopters Deutschland GmbH
- Moritz Buesing
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Active counterweight for main rotor
- Patent number 10,752,349
- Issue date Aug 25, 2020
- Bell Helicopter Textron Inc.
- Andrew Paul Haldeman
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Adaptable rotor control system for a variable number of blades
- Patent number 10,625,846
- Issue date Apr 21, 2020
- Bell Helicopter Textron Inc.
- Gary Miller
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Active rotor damping system
- Patent number 10,577,095
- Issue date Mar 3, 2020
- Sikorsky Aircraft Corporation
- James Orbon
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method of manufacturing a control cuff for a rotor blade of a hinge...
- Patent number 10,532,811
- Issue date Jan 14, 2020
- Airbus Helicopters Deutschland GmbH
- Joerg Radekopf
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Adaptable rotor control system for a variable number of blades
- Patent number 10,358,207
- Issue date Jul 23, 2019
- Bell Helicopter Textron Inc.
- Gary Miller
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Vibration control of a swashplateless coaxial rotor
- Patent number 10,351,233
- Issue date Jul 16, 2019
- Sikorsky Aircraft Corporation
- Bryan D. Mayrides
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rotor hub for a rotorcraft
- Patent number 9,896,199
- Issue date Feb 20, 2018
- Bell Helicopter Textron Inc.
- Christopher Foskey
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Individual blade control utilizing pneumatic muscles
- Patent number 9,751,624
- Issue date Sep 5, 2017
- Bell Helicopter Textron Inc.
- Troy Schank
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Controlling rotor blades of a swashplateless rotor
- Patent number 9,682,771
- Issue date Jun 20, 2017
- Sikorsky Aircraft Corporation
- John Knag
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Swashplateless active blade pitch control with a mechanical delta-3...
- Patent number 9,476,312
- Issue date Oct 25, 2016
- Bell Helicopter Textron Inc.
- Christopher E. Foskey
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Integration of rotary electrical actuator for swashplateless indivi...
- Patent number 9,452,831
- Issue date Sep 27, 2016
- Sikorsky Aircraft Corporation
- Bryan D. Mayrides
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Radial fluid device with variable phase and amplitude
- Patent number 9,376,205
- Issue date Jun 28, 2016
- Bell Helicopter Textron Inc.
- Carlos A. Fenny
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rotary wing blade, rotor comprising at least two of such blades and...
- Patent number 9,334,050
- Issue date May 10, 2016
- ONERA (Office National d'Etudes et de Recherches Aérospatliales)
- Hugues Mercier Des Rochettes
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Swashplateless coaxial rotary wing aircraft
- Patent number 9,248,909
- Issue date Feb 2, 2016
- Sikorsky Aircraft Corporation
- Erez Eller
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Radial fluid device with multi-harmonic output
- Patent number 9,162,760
- Issue date Oct 20, 2015
- Bell Helicopter Textron Inc.
- Carlos A. Fenny
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Independent blade control system with rotary blade actuator
- Patent number 9,061,760
- Issue date Jun 23, 2015
- Bell Helicopter Textron Inc.
- Carlos A. Fenny
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Independent blade control system with hydraulic cyclic control
- Patent number 8,973,864
- Issue date Mar 10, 2015
- Bell Helicopter Textron Inc.
- Carlos A. Fenny
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Independent blade control system with hydraulic pitch link
- Patent number 8,857,757
- Issue date Oct 14, 2014
- Bell Helicopter Textron Inc.
- Carlos A. Fenny
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Helicopter rotor control system
- Patent number 8,858,179
- Issue date Oct 14, 2014
- Sikorsky Aircraft Corporation
- Devon Cowles
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
System and method for magnetically and aerodynamically optimized co...
- Patent number 8,845,290
- Issue date Sep 30, 2014
- Sonic Blue Aerospace, Inc.
- Richard H. Lugg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Adaptive twist system for a rotor blade
- Patent number 8,662,843
- Issue date Mar 4, 2014
- Textron Innovations Inc.
- John E. Brunken
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Swashplateless rotorcraft with fault tolerant linear electric actuator
- Patent number 8,235,667
- Issue date Aug 7, 2012
- Karem Aircraft, Inc.
- William Martin Waide
- 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
Helicopter rotor control system with individual blade control
- Patent number 8,201,771
- Issue date Jun 19, 2012
- ZF Friedrichshafen AG
- Christoph Kessler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Swashplateless helicopter blade actuation system
- Patent number 8,197,205
- Issue date Jun 12, 2012
- The Boeing Company
- Frank M. Rudley
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Helicopter rotor control system with individual blade control
- Patent number 7,900,869
- Issue date Mar 8, 2011
- ZF Friedrichshafen AG
- Christoph Keβler
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
Cable Tilt Actuator for an Aircraft
- Publication number 20240002049
- Publication date Jan 4, 2024
- Overair, Inc.
- William Martin Waide
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
MAST DAMPENER FOR A ROTORCRAFT
- Publication number 20230192284
- Publication date Jun 22, 2023
- Jaunt Air Mobility, LLC
- Jay W. CARTER
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METHOD AND DEVICE FOR DETERMINING A STATE OF A ROTORCRAFT ROTOR
- Publication number 20210362846
- Publication date Nov 25, 2021
- AIRBUS HELICOPTERS
- Jean-Paul PETILLON
- G05 - CONTROLLING REGULATING
Information Patent Application
SYSTEM FOR REDUCING VIBRATIONS OR STRESSES IN A ROTOR BLADE SYSTEM
- Publication number 20210347471
- Publication date Nov 11, 2021
- ZF Friedrichshafen AG
- Andre Hausberg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ACTIVE COUNTERWEIGHT FOR MAIN ROTOR
- Publication number 20200130823
- Publication date Apr 30, 2020
- BELL HELICOPTER TEXTRON INC.
- Andrew Paul HALDEMAN
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Mast Dampener and Collective Pitch for a Rotocraft
- Publication number 20200102073
- Publication date Apr 2, 2020
- Carter Aviation Technologies, LLC
- Jay W. Carter
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
ADAPTABLE ROTOR CONTROL SYSTEM FOR A VARIABLE NUMBER OF BLADES
- Publication number 20190263502
- Publication date Aug 29, 2019
- BELL HELICOPTER TEXTRON INC.
- Gary Miller
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ADJUSTMENT OF TRACK AND BALANCE OF A MULTI-BLADE ROTOR
- Publication number 20180072412
- Publication date Mar 15, 2018
- AIRBUS HELICOPTERS DEUTSCHLAND GMBH
- Moritz BUESING
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ACTIVE ROTOR DAMPING SYSTEM
- Publication number 20180022448
- Publication date Jan 25, 2018
- SIKORSKY AIRCRAFT CORPORATION
- James Orbon
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METHOD OF MANUFACTURING A CONTROL CUFF FOR A ROTOR BLADE OF A HINGE...
- Publication number 20170283051
- Publication date Oct 5, 2017
- AIRBUS HELICOPTERS DEUTSCHLAND GMBH
- Joerg RADEKOPF
- B32 - LAYERED PRODUCTS
Information Patent Application
ROTOR HUB FOR A ROTORCRAFT
- Publication number 20150175259
- Publication date Jun 25, 2015
- BELL HELICOPTER TEXTRON INC.
- Christopher Foskey
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
INTEGRATION OF ROTARY ELECTRICAL ACTUATOR FOR SWASHPLATELESS INDIVI...
- Publication number 20140314573
- Publication date Oct 23, 2014
- SIKORSKY AIRCRAFT CORPORATION
- Bryan D. Mayrides
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
VIBRATION CONTROL OF A SWASHPLATELESS COAXIAL ROTOR
- Publication number 20140314563
- Publication date Oct 23, 2014
- SIKORSKY AIRCRAFT CORPORATION
- Bryan D. Mayrides
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Swashplateless Active Blade Pitch Control with a Mechanical Delta-3...
- Publication number 20140271203
- Publication date Sep 18, 2014
- BELL HELICOPTER TEXTRON INC.
- Christopher E. Foskey
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ACTUATOR CONFIGURATION FOR A ROTARY DRIVE
- Publication number 20140265649
- Publication date Sep 18, 2014
- Timothy A. Fofonoff
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
RADIAL FLUID DEVICE WITH VARIABLE PHASE AND AMPLITUDE
- Publication number 20140234102
- Publication date Aug 21, 2014
- BELL HELICOPTER TEXTRON INC.
- Carlos A. Fenny
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
RADIAL FLUID DEVICE WITH MULTI-HARMONIC OUTPUT
- Publication number 20140231579
- Publication date Aug 21, 2014
- BELL HELICOPTER TEXTRON INC.
- Carlos A. Fenny
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
HELICOPTER WITH ROTOR BLADE LOAD CONTROL METHOD AND DEVICE
- Publication number 20140169967
- Publication date Jun 19, 2014
- Bluebirds Technology LLC
- John Anthony Wilkins
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
INDEPENDENT BLADE CONTROL SYSTEM WITH HYDRAULIC PITCH LINK
- Publication number 20140034777
- Publication date Feb 6, 2014
- BELL HELICOPTER TEXTRON INC.
- Carlos A. Fenny
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
INDEPENDENT BLADE CONTROL SYSTEM WITH ROTARY BLADE ACTUATOR
- Publication number 20140034778
- Publication date Feb 6, 2014
- BELL HELICOPTER TEXTRON INC.
- Carlos A. Fenny
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
INDEPENDENT BLADE CONTROL SYSTEM WITH HYDRAULIC CYCLIC CONTROL
- Publication number 20140034779
- Publication date Feb 6, 2014
- BELL HELICOPTER TEXTRON INC.
- Carlos A. Fenny
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
ADAPTIVE TWIST SYSTEM FOR A ROTOR BLADE
- Publication number 20130089422
- Publication date Apr 11, 2013
- BELL HELICOPTER TEXTRON INC.
- John E. Brunken
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ROTARY WING BLADE, ROTOR COMPRISING AT LEAST TWO OF SUCH BLADES AND...
- Publication number 20120263590
- Publication date Oct 18, 2012
- ONERA (Office National d'Etudes et de Recherches Aerospatiales)
- Hugues Mercier Des Rochettes
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
HELICOPTER ROTOR CONTROL SYSTEM
- Publication number 20120156033
- Publication date Jun 21, 2012
- SIKORSKY AIRCRAFT CORPORATION
- Devon Cowles
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
HELICOPTER ROTOR CONTROL SYSTEM WITH INDIVIDUAL BLADE CONTROL
- Publication number 20120068005
- Publication date Mar 22, 2012
- ZF Friedrichshafen AG
- Christoph Kessler
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Swashplateless rotorcraft with fault tolerant linear electric actuator
- Publication number 20100150719
- Publication date Jun 17, 2010
- Karem Aircraft, Inc.
- William Martin Waide
- 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
SWASHPLATELESS HELICOPTER BLADE ACTUATION SYSTEM
- Publication number 20090269199
- Publication date Oct 29, 2009
- THE BOEING COMPANY
- Frank M. Rudley
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Helicopter Rotor Control System with Individual Blade Control
- Publication number 20080279685
- Publication date Nov 13, 2008
- ZF Friedrichshafen AG
- Christoph Kessler
- 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...

using one actuator per blade

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Helicopter with coaxial counter-rotating roller driven rotors

System for reducing vibrations or stresses in a rotor blade system

System for reducing vibrations or stresses in a rotor blade system

Adjustment of track and balance of a multi-blade rotor

Active counterweight for main rotor

Adaptable rotor control system for a variable number of blades

Active rotor damping system

Method of manufacturing a control cuff for a rotor blade of a hinge...

Adaptable rotor control system for a variable number of blades

Vibration control of a swashplateless coaxial rotor

Rotor hub for a rotorcraft

Individual blade control utilizing pneumatic muscles

Controlling rotor blades of a swashplateless rotor

Swashplateless active blade pitch control with a mechanical delta-3...

Integration of rotary electrical actuator for swashplateless indivi...

Radial fluid device with variable phase and amplitude

Rotary wing blade, rotor comprising at least two of such blades and...

Swashplateless coaxial rotary wing aircraft

Radial fluid device with multi-harmonic output

Independent blade control system with rotary blade actuator

Independent blade control system with hydraulic cyclic control

Independent blade control system with hydraulic pitch link

Helicopter rotor control system

System and method for magnetically and aerodynamically optimized co...

Adaptive twist system for a rotor blade

Swashplateless rotorcraft with fault tolerant linear electric actuator

Hybrid device for vibration control

Helicopter rotor control system with individual blade control

Swashplateless helicopter blade actuation system

Helicopter rotor control system with individual blade control

Patents Applicationslast 30 patents

Cable Tilt Actuator for an Aircraft

MAST DAMPENER FOR A ROTORCRAFT

METHOD AND DEVICE FOR DETERMINING A STATE OF A ROTORCRAFT ROTOR

SYSTEM FOR REDUCING VIBRATIONS OR STRESSES IN A ROTOR BLADE SYSTEM

ACTIVE COUNTERWEIGHT FOR MAIN ROTOR

Mast Dampener and Collective Pitch for a Rotocraft

ADAPTABLE ROTOR CONTROL SYSTEM FOR A VARIABLE NUMBER OF BLADES

ADJUSTMENT OF TRACK AND BALANCE OF A MULTI-BLADE ROTOR

ACTIVE ROTOR DAMPING SYSTEM

METHOD OF MANUFACTURING A CONTROL CUFF FOR A ROTOR BLADE OF A HINGE...

ROTOR HUB FOR A ROTORCRAFT

INTEGRATION OF ROTARY ELECTRICAL ACTUATOR FOR SWASHPLATELESS INDIVI...

VIBRATION CONTROL OF A SWASHPLATELESS COAXIAL ROTOR

Swashplateless Active Blade Pitch Control with a Mechanical Delta-3...

ACTUATOR CONFIGURATION FOR A ROTARY DRIVE

RADIAL FLUID DEVICE WITH VARIABLE PHASE AND AMPLITUDE

RADIAL FLUID DEVICE WITH MULTI-HARMONIC OUTPUT

HELICOPTER WITH ROTOR BLADE LOAD CONTROL METHOD AND DEVICE

INDEPENDENT BLADE CONTROL SYSTEM WITH HYDRAULIC PITCH LINK

INDEPENDENT BLADE CONTROL SYSTEM WITH ROTARY BLADE ACTUATOR

INDEPENDENT BLADE CONTROL SYSTEM WITH HYDRAULIC CYCLIC CONTROL

ADAPTIVE TWIST SYSTEM FOR A ROTOR BLADE

ROTARY WING BLADE, ROTOR COMPRISING AT LEAST TWO OF SUCH BLADES AND...

HELICOPTER ROTOR CONTROL SYSTEM

HELICOPTER ROTOR CONTROL SYSTEM WITH INDIVIDUAL BLADE CONTROL

Swashplateless rotorcraft with fault tolerant linear electric actuator

HYBRID DEVICE FOR VIBRATION CONTROL

SWASHPLATELESS HELICOPTER BLADE ACTUATION SYSTEM

Helicopter Rotor Control System with Individual Blade Control

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