Invention Grant
- Patent Title: Helicopter aircraft vehicle rotor damper
- Patent Title (中): 直升机飞机车辆转子阻尼器
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Application No.: US12203288Application Date: 2008-09-03
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Publication No.: US08167561B2Publication Date: 2012-05-01
- Inventor: Peter Jones
- Applicant: Peter Jones
- Applicant Address: US NC Cary
- Assignee: Lord Corporation
- Current Assignee: Lord Corporation
- Current Assignee Address: US NC Cary
- Agent Richard G. Miller
- Main IPC: B63H1/06
- IPC: B63H1/06 ; B63H5/125 ; B64C11/12 ; B64C11/28 ; F01D5/00

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.
Public/Granted literature
- US20090110555A1 HELICOPTER AIRCRAFT VEHICLE ROTOR DAMPER Public/Granted day:2009-04-30
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