Abstract




 
   

IJE TRANSACTIONS B: Applications Vol. 21, No. 3 (October 2008) 281-290   

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  AN INVESTIGATION ON THE CAUSES OF A ROTOR BENDING AND ITS THERMAL STRAIGHTENING (TECHNICAL NOTE)
 
 
E. Poursaeidi*

Department of Mechanical Engineering, Zanjan University
P. O. Box 313, Zanjan, Iran
Iran Power Plant Repair Company, Research and Laboratories
P. O. Box 31585/1137, Karaj,
Iranepsaeidi@yahoo.com - epsaeidi@znu.ac.ir
 
A. R. Razavi

Iran Power Plant Repair Company, Research and Laboratories
P. O. Box 31585/1137, Karaj, Iran
arazavi110@yahoo.com
 
*Corresponding Author
 
 
( Received: October 09, 2007 – Accepted in Revised Form: May 09, 2008 )
 
 

Abstract    Distortion or bend in a turbine rotor (especially HIP rotors) may be caused by a number of factors, either singularly or in combination. In general, the causes of rotor bend can be classified invariably in two categories: Rapidly forming permanent rotor bends and/or Slower forming rotor bends, which could trip the turbines’ emergency stop. One of the major modifying solutions for rapid repairing of bent rotors is hot spotting. For this purpose, after the initial tests (visual inspection, chemical analysis, nondestructive hardness), the hot spotting was performed seven consecutive times. The results of experimental investigations and experiences with different temperatures and times showed that, the 690 ± 20˚C and 210 S. are as an optimum temperature and time respectively, for hot spotting which can provide a noticeable straightening in bent areas, in addition to having no affects on mechanical properties. Also, this results were simulated by F.E.M in view of heat distribution in different temperatures in three states (without insulation, with moisture and dry insulation), in order to find out the optimum restraint effects around hot spot area.

 

Keywords    Thermal Straightening, Rotor Bending, Hot Spotting

 

References   

1. Gestel, R. V., “Rotor Repair”, Presented at the International Gas Turbines, ASME, Netherlands, No. 94-JT-351, (June 13-16, 1994).

2. Jones, G. T. and Gunning, J., “Causes for and Methods of Straightening Bent Turbine Rotors”, ERA Technology, U.K., (1988).

3. Harrison, H. L., “Straightening Structural Members in Place”, Welding Journal, Vol. 31, (May 1952), 2575-2625.

4. Holt, R. E., “Primary Concepts for Flame Bending”, Welding Journal, Vol. 76, (1971), 416424.

5. Holt, R. E., “Flame Straightening Basics”, Welding Engineering, Vol. 12, (1965), 49-53.

6. Amit, H., “Varma, Keith Kowalkowski”, Effects of Multiple Damage-Heat Straightening Repairs on the Structural Properties of Bridge Stddls, Michigan State University Report, Michigan, U.S.A., No. Rc1456, (November 14, 2004).

7. Pattee, H. E., Evans, R. M., and Monreo, R. E., “Flame Straightening and its Effect on Base Metal Properties, Battelle Memorial Institute Columbus, Ohio, U.S.A., (August 1969).

8. Morris, J., “Controlled Distortion-an aid to Metal Working”, Welding Journal, (November 1949), 1080-1082.

9. Gatewood, B. E., “Thermal Stresses with Applications to Airplanes, Missiles, Turbines and Nuclear Reactors”, McGraw-Hill, New York, U.S.A., (1957).

10. Rothman, R. l., “Flame Straightening Quenched and Tempered Steels in Ship Construction”, Ship Structures Committee, Battelle Columbus Labs Ohio, U.S.A., Report No. 335, (1974).

11. Avent, R. R, Mukai, D. J., Robinson, “Effect of Heat Straightening on Material Properties of Steel”, Journal of Materials in Civil Engineering, ASME, Vol. 12, No. 3, (2000), 188-195.

12. Ministry of Defence, U.K., “Shafting Systems and Propulsors, Requirements for Repair of Main Propulsion Shafting”, No. DEF STAN 02-304, Part 4, Issue 2, U.K. Defence Standardization, U.K., (September 2002).





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