| 发明名称 |
BRACKET FOR MOUNTING/REMOVAL OF ACTUATORS FOR ACTIVE VIBRATION CONTROL |
| 摘要 |
An active vibration control actuator mount including at least one actuator bracket having an actuator interface member configured to hold one or more active vibration element thereon in one or more predetermined orientations, and an engine mounting structure interface member connected to the actuator interface member, the engine mounting structure interface member being configured to couple the at least one actuator bracket to an engine mounting structure, wherein the at least one actuator bracket is configured for the installation and removal of a respective active vibration element to and from the actuator interface member while a respective one of the at least one actuator bracket remains coupled to the engine mounting structure. |
| 申请公布号 |
US2015198093(A1) |
申请公布日期 |
2015.07.16 |
| 申请号 |
US201414153238 |
申请日期 |
2014.01.13 |
| 申请人 |
The Boeing Company |
发明人 |
Jamshidiat Hamid;Jones Michael D.;Elias Laila M. |
| 分类号 |
F02C7/20;F01D25/04 |
主分类号 |
F02C7/20 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An active vibration control actuator mount comprising:
at least one actuator bracket including
an actuator interface member configured to hold one or more active vibration element thereon in one or more predetermined orientations, andan engine mounting structure interface member connected to the actuator interface member, the engine mounting structure interface member being configured to couple the at least one actuator bracket to an engine mounting structure; wherein the at least one actuator bracket is configured for the installation and removal of a respective active vibration element to and from the actuator interface member while a respective one of the at least one actuator bracket remains coupled to the engine mounting structure. |
| 地址 |
Chicago IL US |
