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Class Information
Number: 416/141
Name: Fluid reaction surfaces (i.e., impellers) > Articulated, resiliently mounted or self-shifting impeller or working member > Plural articulation
Description: Apparatus wherein the impeller or working member is supported for movement about plural pivots or for universal movement about one pivot.


Patents under this class:
1 2 3 4

Patent Number Title Of Patent Date Issued
7607892 Rotorcraft rotor with blades hinged in flap and in lag Oct. 27, 2009
7604460 Rotorcraft rotors having twistable blades Oct. 20, 2009
7393180 Wind turbine in parked position Jul. 1, 2008
7207778 Rotor as well as rotary-wing aircraft with a rotor Apr. 24, 2007
7100866 Control system for a flying vehicle Sep. 5, 2006
7040863 Variable pitch rotor blade for shrouded rotors, in particular helicopter rotors May. 9, 2006
6986642 Extreme mu rotor Jan. 17, 2006
6971853 Elastomeric bearing system Dec. 6, 2005
6848886 Snubber Feb. 1, 2005
6783327 Helicopter blade folding with blade droop Aug. 31, 2004
6375426 Protective edge members for composite flexures Apr. 23, 2002
6296444 Prop rotor hub Oct. 2, 2001
6280141 Swash-plates system for control of the pitch of rotor blades with rotating plate driver Aug. 28, 2001
6260676 Magnetic particle damper apparatus Jul. 17, 2001
6152696 Swash-plate device for controlling the pitch of rotor blades with non-rotating plate articulated on a central ball joint Nov. 28, 2000
6149386 Swash-plate device for controlling the pitch of rotor blades with non-rotating plate articulated by cotters on a central ball joint Nov. 21, 2000
6102659 Swash-plate device for controlling the pitch of rotor blades with cylindrical runners sliding on non-rotating pillars Aug. 15, 2000
6074168 Swash-plate device for controlling the pitch of the blades of a rotor with rotary guided parts on slides translated along the rotor axis Jun. 13, 2000
6050778 Semi-articulated rotor system Apr. 18, 2000
6039538 Multi-blade rotor for a helicopter Mar. 21, 2000
6033182 Swash-plate device for controlling the pitch of rotor blades with non rotating plate stop track and pin Mar. 7, 2000
5980206 Monolithic structure having improved flaw tolerance Nov. 9, 1999
5906476 Main rotor system for helicopters May. 25, 1999
5853145 Rotor head for rotary wing aircraft Dec. 29, 1998
5826822 System and method for providing cyclic and collective pitch control in a rotary wing aircraft Oct. 27, 1998
5788462 Hingeless rotor with intermediate pitch-control rings Aug. 4, 1998
5769606 De-icing connection installation for rotorcraft rotor Jun. 23, 1998
5716193 Installation for affording electrical continuity for rotorcraft rotor Feb. 10, 1998
5645400 Composite cuff structure for helicopter rotors Jul. 8, 1997
5511947 Cyclic pitch control having torsion spring system Apr. 30, 1996
5474424 Rotorcraft rotor head, which is rigid in drag and articulated in pitch and flapping Dec. 12, 1995
5466124 Device for generating an inversion-kinematic movement Nov. 14, 1995
5460487 Pitch adjustment assembly for bearingless main rotors Oct. 24, 1995
5364230 Rotor blade subassembly for a rotor assembly having ducted, coaxial counter-rotating rotors Nov. 15, 1994
5340279 Snubber assembly for a rotor assembly having ducted, coaxial counter-rotating rotors Aug. 23, 1994
5316442 Articulated rotor head for gyroplanes May. 31, 1994
5286167 Spar-to-hub joint for a flexbeam helicopter rotor Feb. 15, 1994
5242266 Gyrocraft articulated rotor head with intermediate sleeves between hub and blades Sep. 7, 1993
5228834 Hub structure for a rotary wing aircraft Jul. 20, 1993
5181829 Helicopter blade Jan. 26, 1993
5165853 Main helicopter rotor Nov. 24, 1992
5156527 Main helicopter rotor Oct. 20, 1992
5145321 Helicopter rotors with elastomeric bearings Sep. 8, 1992
5135357 Main helicopter rotor Aug. 4, 1992
5110260 Articulated helicopter rotor within an improved blade-to-hub connection May. 5, 1992
5110259 Pitch change bearing system May. 5, 1992
5096380 Composite flexbeam for a bearingless helicopter rotor Mar. 17, 1992
5092738 Flexbeam helicopter rotor with improved snubber-vibration damper between the torque tube and the flexible spar member Mar. 3, 1992
5074753 Rotor blade Dec. 24, 1991
5059094 Rotor redundant force retention system for VTOL and VSTOL aircraft Oct. 22, 1991

1 2 3 4


 
 
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