Invention Application
- Patent Title: AIRCRAFT LOAD AND VIBRATION ATTENUATION
-
Application No.: US15418652Application Date: 2017-01-27
-
Publication No.: US20170334552A1Publication Date: 2017-11-23
- Inventor: Michael S. Seifert , Brett C. Howard , Thomas C. Parham, JR. , Martin Alex Peryea
- Applicant: Bell Helicopter Textron Inc.
- Main IPC: B64C27/00
- IPC: B64C27/00 ; B64C5/02 ; F16F7/01 ; B64C27/82 ; B64C27/06 ; 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
- US10647418B2 Aircraft load and vibration attenuation Public/Granted day:2020-05-12
Information query
