| 摘要 |
<p>A method for attaching a component to an internal portion of an aircraft fuselage is disclosed herein. The method includes, but is not limited to, mounting a vibration isolator assembly to the internal portion of the aircraft fuselage. The vibration isolator assembly has a protruding engagement portion having a flange. The method further includes, but is not limited to defining an opening in a vibration-deadening body. The method further includes, but is not limited to positioning the vibration-deadening body over the vibration isolator such that the protruding engagement portion is received within the opening. The method further includes, but is not limited to pressing a retaining member onto the protruding engagement portion such that the retaining member engages the flange.</p> |
