NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Variable-Tension-Cord Suspension/Vibration-Isolation SystemA system for mechanical suspension and vibration isolation of a machine or instrument is based on the use of Kevlar (or equivalent aromatic polyamide) cord held in variable tension between the machine or instrument and a surrounding frame. The basic concept of such a tensioned-cord suspension system (including one in which the cords are made of aromatic polyamide fibers) is not new by itself; what is new here is the additional provision for adjusting the tension during operation to optimize vibration- isolation properties. In the original application for which this system was conceived, the objective is to suspend a reciprocating cryocooler aboard a space shuttle and to prevent both (1) transmission of launch vibrations to the cryocooler and (2) transmission of vibrations from the cryocooler to samples in a chamber cooled by the cryocooler. The basic mechanical principle of this system can also be expected to be applicable to a variety of other systems in which there are requirements for cord suspension and vibration isolation. The reciprocating cryocooler of the original application is a generally axisymmetric object, and the surrounding frame is a generally axisymmetric object with windows (see figure). Two cords are threaded into a spoke-like pattern between attachment rings on the cryocooler, holes in the cage, and cord-tension- adjusting assemblies. Initially, the cord tensions are adjusted to at least the level necessary to suspend the cryocooler against gravitation. Accelerometers for measuring vibrations are mounted (1) on the cold tip of the cryocooler and (2) adjacent to the cage, on a structure that supports the cage. During operation, a technician observes the accelerometer outputs on an oscilloscope while manually adjusting the cord tensions in an effort to minimize the amount of vibration transmitted to and/or from the cryocooler. A contemplated future version of the system would include a microprocessor-based control subsystem that would include cord-tension actuators. This control subsystem would continually adjust the cord tension in response to accelerometer feedback to optimize vibration-isolation properties as required for various operating conditions. The control system could also adjust cord tensions (including setting the two cords to different tensions) to suppress resonances. Other future enhancements could include optimizing the cord material, thickness, and braid; optimizing the spoke patterns; and adding longitudinal cords for applications in which longitudinal stiffness and vibration suppression are required.
Document ID
20110014146
Acquisition Source
Johnson Space Center
Document Type
Other - NASA Tech Brief
Authors
Villemarette, Mark L.
(NASA Johnson Space Center Houston, TX, United States)
Boston, Joshua
(NASA Johnson Space Center Houston, TX, United States)
RInks, Judith
(NASA Johnson Space Center Houston, TX, United States)
Felice, Pat
(NASA Johnson Space Center Houston, TX, United States)
Stein, Tim
(NASA Johnson Space Center Houston, TX, United States)
Payne, Patrick
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
November 1, 2006
Publication Information
Publication: NASA Tech Briefs, November 2006
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MSC-23993
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available