发明名称 |
APPARATUS AND METHOD FOR TUNING VIBRATORY RESPONSE OF ROTOR BLADE |
摘要 |
PROBLEM TO BE SOLVED: To provide a method and apparatus for reducing a vibratory response of a rotor blade by a desired amount.SOLUTION: Provided is a method and apparatus for reducing a vibratory response in a structure using a tuning object 312. A selected mass is identified for the tuning object. A plurality of channels are formed in a workpiece having a mass greater than the selected mass to form the tuning object having the selected mass. The tuning object is bonded to the structure using an adhesive bond to reduce the vibratory response of the structure. |
申请公布号 |
JP2014111986(A) |
申请公布日期 |
2014.06.19 |
申请号 |
JP20130233688 |
申请日期 |
2013.11.12 |
申请人 |
BOEING CO |
发明人 |
FRANK JOSEPH GILL III;RUSSELL EDDY FAY |
分类号 |
F16F15/02;B64C1/00;B64C27/473 |
主分类号 |
F16F15/02 |
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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