发明名称 |
Apparatus and method for tuning a vibratory response of a rotor blade |
摘要 |
A method and apparatus for reducing a vibratory response in a structure using a tuning object. A selected mass may be identified for the tuning object. A plurality of channels may be formed in a workpiece having a mass greater than the selected mass to form the tuning object having the selected mass. The tuning object may be bonded to the structure using an adhesive bond to reduce the vibratory response of the structure. |
申请公布号 |
EP2733067(A3) |
申请公布日期 |
2016.07.13 |
申请号 |
EP20130190176 |
申请日期 |
2013.10.25 |
申请人 |
THE BOEING COMPANY |
发明人 |
GILL, FRANK JOSEPH, III;FAY, RUSSELL EDDY |
分类号 |
B64C27/00;B64C27/473 |
主分类号 |
B64C27/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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