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MOMENT OF INERTIA INSTRUMENTS
The GB series Moment Of Inertia (MOI) instruments are designed to measure large mechanical components such as re-entry vehicles, spacecraft, automobile engine parts, and complex structures. Standard models are available for measurement of test objects weighing up to 15,000 pounds (6,800Kg) with an accuracy of +/-0.1 percent. In addition to their use as a design tool, these instruments are fast enough for use on production lines for manufacturing quality analysis. Most rotating machinery and all space vehicles require the calculation of Moment of Inertia of components and complete assemblies. While these calculations have become faster and more accurate through the use of computers, the exact value and extent of manufacturing variations cannot be known without making measurements. Space Electronics GB Series instruments measure the MOI of any object regardless of its size or shape in a fraction of the time required for the MOI calculation and permit rapid accumulation of data for variation analysis. GB Series instruments use a flat gas thrust bearing to support the test part weight, a cylindrical gas bearing for precise centering, and a torsion rod as a rotational spring. The lower end of the rod is attached to a flexure which prevents changes in torsion stiffness as a function of small variations in gas bearing gap and thermal expansion of the machine frame. The instrument operates on the principal of an inverted torsion pendulum. To measure
MOI, the test table is rotated through a small angle and held against a fixed stop. When
released, the table will oscillate freely since the load is supported and centered by
nearly frictionless gas bearings. A digital timer on the instrument determines the period
of oscillation. This procedure is first carried out with the bare table and any necessary
locating fixture, and then again with the test part mounted. A simple computation using
the tare period, the period with test part, and a calibration constant, converts this data
into moment of inertia of the test part.
Choosing a Location - Care should be exercised in choosing the proper site for the instrument in order to achieve full rated accuracy. The foundation on which the instrument is mounted must be rigid enough to support the total weight of the instrument and test part without altering the level condition of the instrument. A means must be provided for gently lowering the heavy payloads in place without damaging the instrument. For maximum accuracy, short term temperature variations should be less than +/- 2o F (1oC). Drafts should be avoided. These instruments are supplied with calibration weights, a calibration weight locating system (beam or table with calibration holes), a 6 digit period counter with crystal controlled time base, and a pocket calculator. Computer Interfacing Option - This an IBM style computer, VGA color monitor, printer, RS232 interface, and operating software. The software provides prompts to the operator for calibration, tare, and part measurement procedures, reads timer data, averages period readings, calculates MOI, and generates a report. SPECIAL INSTRUMENTS In addition to our standard line of instruments, we have designed and manufactured special instruments for test parts in excess of 25,000 lbs. and have achieved accuracy as great as 0.01%. These machines can also be fully automated to meet special needs. Contact our sales department, if a standard instrument will not meet your requirements. |
| Space Electronics LLC - 81 Fuller Way - Berlin, CT 06037 (USA) - Phone: +1 860 829 0001 - Fax: +1 860 829 0005 - Email: sales@space-electronics.com |