Turbine blades having alternating resonant frequencies

• US 4,878,810 A
• Filed: 05/20/1988
• Issued: 11/07/1989
• Est. Priority Date: 05/20/1988
• Status: Expired due to Term

• Current Assignee: Siemens Power Generation, Inc.
• Original Assignee: Westinghouse Electric Corporation (Paramount Global (f/k/a ViacomCBS Inc.))
• Inventors: Evans, David H.
• Primary Examiner(s): Powell Jr., Everette A.
• Application Number:
  US07/196,691
• Time in Patent Office: 536 Days
• Field of Search: 416/203, 416/228, 416/175, 416/500, 415/119, 415/172 A
• US Class Current: 416/203
• CPC Class Codes: F01D 5/16 for counteracting blade vibration
• CPC Class Codes: F01D 5/20 Specially-shaped blade tips to seal space between tips and stator F01D5/225 takes precedence
• CPC Class Codes: F05D 2260/961 by mistuning rotor blades or stator vanes with irregular interblade spacing, airfoil shape
• CPC Class Codes: Y10S 416/50 Vibration damping features

Abstract

Within a rotor blade row of a steam turbine, rotor blades having one resonant frequency alternate with rotor blades having a second, different resonant frequency. The two different resonant frequencies are achieved by profiling the tips of every other rotor blade.

Claims

1. A steam turbine rotor assembly comprising:

a rotor rotatable at a predetermined running speed,

a plurality of first free standing elongated, low aspect rotor blades, each having a first resonant frequency,

a plurality of second free standing elongated, low aspect rotor blades, each having a second resonant frequency, wherein the plurality of first and second rotor blades are alternatingly connected to the rotor in at least one row, and wherein adjacent blades of the at least one row have alternating first and second resonant frequencies, each of the plurality of first and second rotor blades having a base portion and an air foil portion including a leading edge, a trailing edge, a concave surface, a convex surface, and a tip, and the tips of the plurality of second rotor blades of the at least one row being profiled for increasing the resonant frequency thereof, said alternating first and second resonant frequencies providing means for preventing unstalled flutter in the at least one row at non-resonant frequencies wherein each profiled tip includes an L-shaped recess formed substantially longitudinally from the leading edge to the trailing edge in the concave surface of the airfoil portion of the blade at the tip, said L-shaped recess defining an extension running from the trailing edge along the top and terminating before the leading edge.

2. A turbine rotor assembly as recited in claim 1, wherein rotation of the rotor at the predetermined running speed produces a series of harmonics, and wherein the first and second resonant frequencies of the first and second rotor blades of the at least one row are in a frequency range approximately centered between two successive harmonics of the series of harmonics.

3. A turbine rotor assembly as recited in claim 1, wherein the at least one row of rotor blades comprises three rows of a low pressure steam turbine.

4. A turbine rotor assembly as recited in claim 3, wherein the plurality of first and second rotor blades are free standing blades.

5. A turbine rotor assembly as recited in claim 2, wherein the first and second resonant frequencies are first mode resonant frequencies in which vibrations occur in the plurality of first and second rotor blades in the direction of rotor rotation.

6. A turbine rotor assembly as recited in claim 1, wherein the predetermined running speed is substantially 3,600 r.p.m.