发明名称 |
A mechanically optimized liquid inertia vibration eliminator and aircraft pylon system |
摘要 |
<p>A vibration isolator (401) includes an upper housing (403) and a lower housing (405); an upper reservoir housing (427) defining a upper fluid chamber (407); a lower reservoir housing defining a lower fluid chamber (409); a piston spindle (411) resiliently coupled to the upper housing with an upper elastomer member (413), the piston spindle being resiliently coupled to the lower housing with a lower elastomer member (415); an elongated portion (419) having a tuning passage (421); and a tuning fluid (423) disposed there within. The vibration isolator cancels vibratory forces at an isolation frequency. The vibration isolator is utilized in a pylon system for mounting a transmission in an aircraft (11). The vibration isolator is located between a pylon structure (615) and a roof structure (603). The isolator includes a spherical bearing assembly that is located near a waterline location of a rotational axis (617) of a drive shaft.</p> |
申请公布号 |
EP2615027(A1) |
申请公布日期 |
2013.07.17 |
申请号 |
EP20120154479 |
申请日期 |
2012.02.08 |
申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
GRIFFIN, MAURICE D |
分类号 |
B64C27/00;F16F1/36;F16F7/10;F16F7/108;F16F9/34 |
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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