Invention Grant
- Patent Title: Mechanically optimized liquid inertia vibration eliminator and aircraft pylon system
- Patent Title (中): 机械优化液体惯性消音器和飞机塔架系统
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Application No.: US14183711Application Date: 2014-02-19
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Publication No.: US09279471B2Publication Date: 2016-03-08
- Inventor: Maurice D. Griffin
- Applicant: Textron Innovations Inc.
- Applicant Address: US RI Providence
- Assignee: Textron Innovations Inc.
- Current Assignee: Textron Innovations Inc.
- Current Assignee Address: US RI Providence
- Agent James E. Walton
- Main IPC: B64C27/00
- IPC: B64C27/00 ; B63H7/02 ; F01D25/04 ; F03B11/04 ; F04D29/66 ; F16F13/08 ; F16F13/24 ; B64D27/26

Abstract:
A vibration isolator includes an upper housing and a lower housing; an upper reservoir housing defining a upper fluid chamber; a lower reservoir housing defining a lower fluid chamber; a piston spindle resiliently coupled to the upper housing with an upper elastomer member, the piston spindle being resiliently coupled to the lower housing with a lower elastomer member; an elongated portion having a tuning passage; and a tuning fluid 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. The vibration isolator is located between a pylon structure and a roof structure. The isolator includes a spherical bearing assembly that is located near a waterline location of a rotational axis of a drive shaft.
Public/Granted literature
- US20140217232A1 MECHANICALLY OPTIMIZED LIQUID INERTIA VIBRATION ELIMINATOR AND AIRCRAFT PYLON SYSTEM Public/Granted day:2014-08-07
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