HELICOPTER AIRCRAFT VEHICLE ROTOR DAMPER
First Claim
1. A helicopter rotor damper system for damping a motion of a helicopter blade relative to a helicopter rotor, said helicopter rotor damper system including:
- a torsional damper with a damper centering bearing providing a damper center of rotation axis,at least a first elastomeric torsional damper, said first elastomeric torsional damper having a first elastomeric torsional damper torsional elastomer bonded between a first elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a first elastomeric torsional damper second torsional damper nonelastomeric bonding surface,at least a second elastomeric torsional damper, said second elastomeric torsional damper having a second elastomeric torsional damper torsional elastomer bonded between a second elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a second elastomeric torsional damper second torsional damper nonelastomeric bonding surface,and a damper link, said damper link linked with said torsional damper, wherein said torsional damper and said damper link are connected between said helicopter blade and said helicopter rotor with said first elastomeric torsional damper first torsional damper nonelastomeric bonding surface rotating relative to said first elastomeric torsional damper second torsional damper nonelastomeric bonding surface,and said second elastomeric torsional damper first torsional damper nonelastomeric bonding surface rotating relative to said second elastomeric torsional damper second torsional damper nonelastomeric bonding surface.
1 Assignment
0 Petitions
Accused Products
Abstract
A helicopter rotor damper system including a torsional damper with a damper centering bearing providing a damper center of rotation axis, a first elastomeric torsional damper with a first elastomeric torsional damper torsional elastomer bonded between a first elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a first elastomeric torsional damper second torsional damper nonelastomeric bonding surface, and a second elastomeric torsional damper with a second elastomeric torsional damper torsional elastomer bonded between a second elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a second elastomeric torsional damper second torsional damper nonelastomeric bonding surface. The helicopter rotor damper system includes a damper link linked with the torsional damper, with the torsional damper and the damper link connected between a helicopter blade and a helicopter rotor with the elastomeric torsional damper nonelastomeric bonding surfaces relatively rotating.
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Citations
56 Claims
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1. A helicopter rotor damper system for damping a motion of a helicopter blade relative to a helicopter rotor, said helicopter rotor damper system including:
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a torsional damper with a damper centering bearing providing a damper center of rotation axis, at least a first elastomeric torsional damper, said first elastomeric torsional damper having a first elastomeric torsional damper torsional elastomer bonded between a first elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a first elastomeric torsional damper second torsional damper nonelastomeric bonding surface, at least a second elastomeric torsional damper, said second elastomeric torsional damper having a second elastomeric torsional damper torsional elastomer bonded between a second elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a second elastomeric torsional damper second torsional damper nonelastomeric bonding surface, and a damper link, said damper link linked with said torsional damper, wherein said torsional damper and said damper link are connected between said helicopter blade and said helicopter rotor with said first elastomeric torsional damper first torsional damper nonelastomeric bonding surface rotating relative to said first elastomeric torsional damper second torsional damper nonelastomeric bonding surface, and said second elastomeric torsional damper first torsional damper nonelastomeric bonding surface rotating relative to said second elastomeric torsional damper second torsional damper nonelastomeric bonding surface. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15)
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16. A damper including a damper centering bearing providing a damper center of rotation axis,
at least a first elastomeric torsional damper, said first elastomeric torsional damper having a first elastomeric torsional damper torsional elastomer bonded between a first elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a first elastomeric torsional damper second torsional damper nonelastomeric bonding surface, at least a second elastomeric torsional damper, said second elastomeric torsional damper having a second elastomeric torsional damper torsional elastomer bonded between a second elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a second elastomeric torsional damper second torsional damper nonelastomeric bonding surface, wherein said first elastomeric torsional damper first torsional damper nonelastomeric bonding surface rotate relative to said first elastomeric torsional damper second torsional damper nonelastomeric bonding surface, and said second elastomeric torsional damper first torsional damper nonelastomeric bonding surface rotate relative to said second elastomeric torsional damper second torsional damper nonelastomeric bonding surface.
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26. An aircraft link system, said aircraft link system including:
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a longitudinally extending link, said longitudinally extending link having a longitudinal link axis with said link having a first linkend and a distal second linkend, said first linkend is comprised of a nonelastomeric outer link housing member, said first linkend having a linkend cavity with a linkend cavity inner circumferential bonding surface, and a linkend nonelastomeric inner member contained in said linkend cavity, said linkend nonelastomeric inner member having a linkend outer circumferential bonding surface, and a linkend elastomeric intermediate having an outer circumferential elastomeric bonding surface and an inner circumferential elastomeric bonding surface, said outer circumferential elastomeric bonding surface bonded to said linkend cavity inner circumferential bonding surface and said inner circumferential elastomeric bonding surface bonded to said linkend outer circumferential bonding surface, said elastomeric intermediate containing a plurality of bonded nonelastomeric shims, and a first cantilever connector providing a cantileved connection between said first linkend nonelastomeric inner member and a first aircraft member. - View Dependent Claims (27, 28, 29)
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30. A method of making a damper system, said method including:
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providing a damper centering bearing providing a damper center of rotation axis, providing at least a first elastomeric torsional damper, said first elastomeric torsional damper having a first elastomeric torsional damper torsional elastomer bonded between a first elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a first elastomeric torsional damper second torsional damper nonelastomeric bonding surface, providing at least a second elastomeric torsional damper, said second elastomeric torsional damper having a second elastomeric torsional damper torsional elastomer bonded between a second elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a second elastomeric torsional damper second torsional damper nonelastomeric bonding surface, centering said at least a first elastomeric torsional damper and said at least a second elastomeric torsional damper to rotate about said damper center of rotation axis, providing a damper link, connecting said damper link with said at least first elastomeric torsional damper and said at least second elastomeric torsional damper, and said second elastomeric torsional damper first torsional damper nonelastomeric bonding surface rotating relative to said second elastomeric torsional damper second torsional damper nonelastomeric bonding surface. - View Dependent Claims (31, 32, 33, 34, 35, 36, 37, 38, 39, 40, 41, 42)
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43. A method of controlling a motion, said method including:
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providing a damper, said damper including a damper centering bearing providing a damper center of rotation axis, at least a first elastomeric torsional damper, said first elastomeric torsional damper having a first elastomeric torsional damper torsional elastomer bonded between a first elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a first elastomeric torsional damper second torsional damper nonelastomeric bonding surface, and at least a second elastomeric torsional damper, said second elastomeric torsional damper having a second elastomeric torsional damper torsional elastomer bonded between a second elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a second elastomeric torsional damper second torsional damper nonelastomeric bonding surface, said at least first elastomeric torsional damper and said at least second elastomeric torsional damper rotating about said damper center of rotation axis, providing a damper link, connecting said damper link with said damper wherein said first elastomeric torsional damper first torsional damper nonelastomeric bonding surface rotates relative to said first elastomeric torsional damper second torsional damper nonelastomeric bonding surface about said damper center of rotation axis, and said second elastomeric torsional damper first torsional damper nonelastomeric bonding surface rotates relative to said second elastomeric torsional damper second torsional damper nonelastomeric bonding surface about said damper center of rotation axis. - View Dependent Claims (44, 45, 46, 47, 48, 49, 50, 51, 52, 53, 54, 55)
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56. A damper system for damping a motion of a moving member, said damper system including:
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a torsional damper with a means for providing a damper center of rotation axis, at least a first elastomeric torsional damper, said first elastomeric torsional damper having a first elastomeric torsional damper torsional elastomer bonded between a first elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a first elastomeric torsional damper second torsional damper nonelastomeric bonding surface, at least a second elastomeric torsional damper, said second elastomeric torsional damper having a second elastomeric torsional damper torsional elastomer bonded between a second elastomeric torsional damper first torsional damper nonelastomeric bonding surface and a second elastomeric torsional damper second torsional damper nonelastomeric bonding surface, and a means for linking said torsional damper with said moving member, wherein said torsional damper is connected with said moving member with said first elastomeric torsional damper first torsional damper nonelastomeric bonding surface rotating relative to said first elastomeric torsional damper second torsional damper nonelastomeric bonding surface, and said second elastomeric torsional damper first torsional damper nonelastomeric bonding surface rotating relative to said second elastomeric torsional damper second torsional damper nonelastomeric bonding surface.
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Specification