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The spin test, of course, is the primary proof of the material, fabrication, and design Although it will not ordinarily answer questions of fatigue or cycled loads, a destructive spin test gives the best indication of the true safety margin Long-term cyclic life tests are very helpful if a realistic load cycle can be devised A third way to reduce the necessary factor of safety is to reduce the physical and financial harm that would be caused by a flywheel failure No matter what material is used, any flywheel will break if it is rotated fast enough If this failure can be controlled in some way, the design speed of the flywheel can be closer to the failure speed without undue risk Standard steel rim-type and disk flywheels usually burst into three to six pieces at failure; each piece travels with quite a bit of kinetic energy.

One method to control failure is therefore to force a breakup into smaller pieces;.

Downloaded from Digital Engineering Library @ McGraw-Hill (www.digitalengineeringlibrary.com) Copyright 2004 The McGraw-Hill Companies. All rights reserved. Any use is subject to the Terms of Use as given at the website.

many composite flywheels shred, for example. Another method used with the energy-storage flywheel relies on centrifugal force to separate the outer circular sections of the flywheel from the spokes or inner hub section before the material begins to fail. If a benign failure mode cannot be introduced into the design, a heavier containment enclosure could serve the same purpose, lessening the consequence of a flywheel failure.

Listing 12-1

- (id) init { self = [super init]; if (self != nil) { [self preload]; } return self; }

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7.1 1980 Flywheel Technology Symposium, October 1980, Scottsdale, Arizona, University of California Lawrence Livermore National Laboratory, Livermore, Calif., NTIS CONF801022. 7.2 Rowland S. Benson and N. D. Whitehouse, Internal Combustion Engines, Pergamon, New York, 1979. 7.3 C. W. Bert and G. Ramunujam, Design Guide for Composite-Material Flywheels: Rotor Dynamic Considerations, Part I, University of Oklahoma, Norman, Okla., September 1981, UCRL-15420. 7.4 J. P. Den Hartog, Advanced Strength of Materials, McGraw-Hill, New York, 1952. 7.5 R. R. Gilbert, et al., Flywheel Feasibility Study and Demonstration, Lockheed Missiles and Space Company, Sunnyvale, Calif., April 1971, NTIS PB-200143. 7.6 Edward B. Haugen, Probabilistic Approaches to Design, John Wiley & Sons, New York, 1968. 7.7 Charles R. Mischke, Elements of Mechanical Analysis, Addison-Wesley, Reading, Mass., 1963. 7.8 R. P. Nimmer, K. Torossian, and W. W. Wilkening, Laminated Composite Disk Flywheel Development, General Electric Company, Schenectady, N.Y., UCRL-15383. 7.9 M. Saraph, A. Midha, and J. C. Wambold, Automated Stress Analysis of Mechanical Sheaves and Pulleys, Computers in Mechanical Engineering, pp. 34 42, October 1982. 7.10 Joseph E. Shigley and Charles R. Mischke, Mechanical Engineering Design, 5th ed., McGraw-Hill, New York, 1989. 7.11 Joseph Edward Shigley and John Joseph Uicker, Jr., Theory of Machines and Mechanisms, 2d ed. McGraw-Hill, New York, 1995.

Downloaded from Digital Engineering Library @ McGraw-Hill (www.digitalengineeringlibrary.com) Copyright 2004 The McGraw-Hill Companies. All rights reserved. Any use is subject to the Terms of Use as given at the website.

Downloaded from Digital Engineering Library @ McGraw-Hill (www.digitalengineeringlibrary.com) Copyright 2004 The McGraw-Hill Companies. All rights reserved. Any use is subject to the Terms of Use as given at the website.

Morse code keyer program (Continued).

8.1 TYPES, USES, ADVANTAGES, AND CHARACTERISTICS / 8.4 8.2 TORQUE AND ENERGY CONSIDERATIONS / 8.14 8.3 TEMPERATURE CONSIDERATIONS / 8.21 8.4 FRICTION MATERIALS / 8.23 8.5 TORQUE AND FORCE ANALYSIS OF RIM CLUTCHES AND BRAKES / 8.25 8.6 BAND AND CONE BRAKES AND CLUTCHES / 8.34 8.7 DISK CLUTCHES AND BRAKES / 8.40 8.8 ELECTROMAGNETIC TYPES / 8.45 8.9 ACTUATION PROBLEMS / 8.48 REFERENCES / 8.50 SUGGESTED READING / 8.50

That was a simple init method. Basically, you just call preload, which is where you, well, preload all your particles and memory allocations:

a a a A b b c C C d D D Dmax e E f fv Vehicle deceleration, ft/s2 (m/s2) Location of shoe pivot, in (m) Lever arm for larger band force, in (m) Area, in2 (m2) Percentage of grade Width of band, shoe, or web, in (m) Lever arm for smaller band force, in (m) Center of pressure Specific heat, Btu/(lbm F) [J/(kg C)] Inside disk diameter, in (m) Outside disk diameter, in (m) Pitch diameter of gear, in (m) Maximum roll diameter, in (m) Radius to center of circular brake pad, in (m) Total energy dissipated, ft lb or Btu (J) Coefficient of friction Ventilation factor

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