B64C2027/7266 - CPC Classification Index

ClassID:

72159 ⎘

B64C2027/7266 - CPC Classification

Classification description:

Rotorcraft; Rotors peculiar thereto; Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement; Means acting on blades on each blade individually, e.g. individual blade control [IBC] with flaps actuated by actuators

Sub-classes:

B64C2027/7272 » {of the electro-hydraulic type} 14
B64C2027/7277 » {of the magnetostrictive type} 5
B64C2027/7283 » {of the piezoelectric type} 15
B64C2027/7288 » {of the memory shape type} 18

Recent Application in this class:

20230303241

2023-09-28

Rotor blade using adaptive trailing edge assembly

20210114722

2021-04-22

Linear actuator

20190088244

2019-03-21

Noise reduction device, flight vehicle, power generation device, and noise reduction method

20180162515

2018-06-14

Gurney flap

20170341744

2017-11-30

Main rotor trim tab retention system, an aircraft employing same and a method of replacing a trim tab assembly from blade housing

20170183089

2017-06-29

Rotor blade system

20160221673

2016-08-04

Electro-hydraulic on-blade actuation system

20160053620

2016-02-25

Actuator lock

20150298802

2015-10-22

Blade with reduced torsional rigidity, and rotor equipped with such a blade

#10

20150104307

2015-04-16

Actuation system for an active blade element of a rotor blade

#11

20150010401

2015-01-08

Flexbeam hinge for helicopter blade active trailing edge flap

#12

20140083216

2014-03-27

Dry lubricated rotary actuator for in blade rotor control

#13

20140064965

2014-03-06

Actuation system for an active element in a rotor blade

#14

20140064962

2014-03-06

Electromechanical linear actuator for in blade rotor control

#15

20140064960

2014-03-06

Actuation system for an active element in a rotor blade

#16

20140060249

2014-03-06

Actuation system for an active element in a rotor blade

#17

20130327879

2013-12-12

High speed compound rotary wing aircraft

#18

20130320782

2013-12-05

Electromechanical rotary actuator and method

#19

20130294914

2013-11-07

Multi-element rotor blade

#20

20130259681

2013-10-03

Enhanced performance rotorcraft rotor blade

#21

20130058793

2013-03-07

System for heat dissipation from an internal actuator in a rotor blade

#22

20120308384

2012-12-06

Twist mechanism for twisting a rotor blade for a rotorcraft, and a blade

#23

20120305698

2012-12-06

Method and apparatus for actively manipulating aerodynamic surfaces

#24

20120261519

2012-10-18

Active gurney flap

#25

20120261518

2012-10-18

Active gurney flap

#26

20120261508

2012-10-18

Active gurney flap

#27

20120116612

2012-05-10

Implementation of Kalman filter linear state estimator for actuator equalization

#28

20110164979

2011-07-07

Mechanical system for high acceleration environments

#29

20110164976

2011-07-07

Active rotor blade control effector system for a rotary-wing aircraft

#30

20100178167

2010-07-15

Method and device for controlling a rotary wing aircraft

#31

20100047067

2010-02-25

System and methods for adaptive blade control surface adjustment

#32

20100044505

2010-02-25

HELICOPTER BLADE VORTEX INTERACTION NOISE REDUCING METHOD AND DEVICE

#33

20090302168

2009-12-10

Compliant structure design of varying surface contours

#34

20080237395

2008-10-02

Helicopter blade vortex interaction noise reducing method and device

#35

20080203222

2008-08-28

Yaw control system and method

#36

20080138203

2008-06-12

Self-lubricated actuator for on-blade rotor control

#37

20080101931

2008-05-01

Brushless direct current (BLDC) motor based linear or rotary actuator for helicopter rotor control

#38

20080035798

2008-02-14

Fluid-driven artificial muscles as mechanisms for controlled actuation

#39

20080035788

2008-02-14

Cellular support structures used for controlled actuation of fluid contact surfaces

#40

20070131820

2007-06-14

Rotorcraft control system and method of using

#41

20070098553

2007-05-03

Rotorcraft blade provided with a flap that is tiltable with the help of at least one main ball joint having a first shaft that is secured to said flap

#42