NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Concepts and effects of damping in isolatorsA series of innovative designs and inventions which led to the solution of many aerospace vibration and shock problems through damping techniques is presented. The design of damped airborne structures has presented a need for such creative innovation. The primary concern was to discover what concepts were necessary for good structural damping. Once these concepts are determined and converted into basic principles, the design of hardware follows. The following hardware and techniques were developed in support of aerospace program requirements: shipping containers, alignment cables for precision mechanisms, isolation of small components such as relays and flight instruments, isolation for heavy flight equipment, coupling devices, universal joints, use of wire mesh to replace cable, isolation of 16-dB, 5000 lb horn, and compound damping devices to get better isolation from shock and vibration in a high steady environment.
Document ID
19860012420
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kerley, J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 12, 2013
Publication Date
November 1, 1984
Publication Information
Publication: AFWAL Vibration Damping 1984 Workshop Proceedings
Subject Category
Structural Mechanics
Accession Number
86N21891
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available