Rotors with mistuned blades

Fluid reaction surfaces (i.e. – impellers) – Unsymmetrical impeller or dissimilar working members

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Details

416203, 416175, 416241R, 416500, 416223, 415119, 298891, 2988921, 29404, 2940701, 364578, 36446803, 36446804, B64C 2746, F01D 514, F03B 312

Patent

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059931612

ABSTRACT:
A method for designing a mistuned rotor with improved stability and forced response.

REFERENCES:
patent: 4097192 (1978-06-01), Kulina
patent: 5388956 (1995-02-01), Pla et al.
patent: 5391053 (1995-02-01), Pla et al.
patent: 5566907 (1996-10-01), Marze et al.
patent: 5620300 (1997-04-01), Knuijt
patent: 5620303 (1997-04-01), Moffitt et al.
Chi et al., Some Recent Advances in the Understanding and Prediction of Turbomachine Subsonic Stall Flutter, Transactions of the ASME, vol. 107 pp. 408-417 (Apr. 1985).
Srinivasan et al., Effects of Mistuning on Resonant Stresses of Turbine Blades, The Winter Annual Meeting of The American Society of Mechanical Engineers, pp. 57-71 (Dec. 5-10, 1976).
Whitehead, D.S., Effect of Mistuning on the Vibration of Turbomachine Blades induced by Wakes, Journal Mechanical Engineering Science, vol. 8 No. 1 1966, pp. 15-21 (1966).

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