Invention Grant
- Patent Title: Aircraft load and vibration attenuation
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Application No.: US15418652Application Date: 2017-01-27
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Publication No.: US10647418B2Publication Date: 2020-05-12
- Inventor: Michael S. Seifert , Brett C. Howard , Thomas C. Parham, Jr. , Martin Alex Peryea
- Applicant: Bell Helicopter Textron Inc.
- Applicant Address: US TX Fort Worth
- Assignee: BELL HELICOPTER TEXTRON INC.
- Current Assignee: BELL HELICOPTER TEXTRON INC.
- Current Assignee Address: US TX Fort Worth
- Agency: Patent Capital Group
- Main IPC: F16F15/02
- IPC: F16F15/02 ; B64C27/00 ; B64C5/02 ; B64C27/04 ; F16F7/01 ; B64C27/82 ; B64C29/00
Abstract:
In one embodiment, an apparatus comprises a particle damper for damping a component when the particle damper is attached to the component. The particle damper comprises a plurality of pockets configured to hold a plurality of particles, and the particle damper also comprises an attachment fitting for coupling the particle damper to the component.
Public/Granted literature
- US20170334552A1 AIRCRAFT LOAD AND VIBRATION ATTENUATION Public/Granted day:2017-11-23
Information query
