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US4732532A Expired / Lapsed US ⏱️ 0.0 years remaining

Arrangement for minimizing buzz saw noise in bladed rotors

Assignee: Rolls Royce PLC
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Filing: 1982-11-12
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Granted: 1988-03-22
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Expires: 2002-11-12
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Abstract

Abstract The invention minimizes selected tones present in buzz-saw noise, otherwise known as multiple pure tone noise. This noise arises from the production of unequal shockwaves during the rotation at sonic or supersonic velocities of a bladed rotor, the dimensional characteristics of whose blades are subject to manufacturing tolerances. Minimization of selected buzz-saw noise tones is achieved by arranging the blades around the rotor in a sequence which minimizes selected Fourier coefficients of the shockwave strengths; alternatively, the blades are arranged to minimize selected Fourier coefficients of the dimensional characteristics of the blades, such as thickness, t, stagger angle θ, and camber. The invention is particularly applicable to the fan propulsors of turbofan aeroengines.

Inventors

  • 👤 Peter J. G. Schwaller
  • 👤 David R. Newby

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 08:38
CPC Classifications
B; B64; B64D; B64D33/00; B64D33/02; F; F02; F02C; F02C7/00; F02C7/04; F02C7/045; F04; F04D; F04D29/00; F04D29/66; F04D29/661; F04D29/663; F04D29/666; B64D2033/0206; B64D2033/0266; B64D2033/0286; Y; Y02; Y02T; Y02T50/00; Y02T50/60; Y10; Y10S; Y10S416/00; Y10S416/50

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 280 words
A rotor including a plurality of rotor blades, said rotor being adapted for rotation within a duct under conditions in which at least radially outer portions of said rotor blades attain at least sonic velocity thereby producing shockwaves within said duct, said blades being subject to manufacturing tolerances manifested in blade-to-blade variations of at least one selected dimensional characteristic of said blades, which dimensional characteristic has a significant effect on shockwave strengths, whereby said blades generate shockwaves which vary in strength from blade to blade around said rotor thereby causing buzz saw noise within said duct, said rotor being produced by a process in which the blades are arranged in a sequence which minimizes the intensity of at least one selected buzz saw noise tone, said process comprising the steps of: (a) measuring said at least one selected dimensional characteristic of each blade to be assembled into said rotor; (b) notionally arranging said blades around said rotor in a chosen sequence; (c) evaluating the shockwave strength at each said blade as arranged in sequence; (d) calculating at least one Fourier coefficient of said shockwave strengths for said sequence, said at least one Fourier coefficient being selected to correspond to said at least one selected buzz saw noise tone; (e) rearranging said blades around said rotor in further sequences and repeating steps (c) and (d) for each such sequence to determine which one of said sequences produces an acceptable minimum value of said at least one Fourier coefficient; and (f) assembling said blades into said rotor such that they are arranged in that one of said sequences for which said minimum value of said at least one Fourier coefficient is obtained.
Claim 2
Dependent Claim 280 words
A rotor including a plurality of rotor blades, said rotor being adapted for rotation within a duct under conditions in which at least radially outer portions of said rotor blades attain at least sonic velocity thereby producing shockwaves within said duct, said blades being subject to manufacturing tolerances manifested in blade-to-blade variations of at least one selected dimensional characteristic of said blades, which dimensional characteristic has a significant effect on shockwave strengths, whereby said blades generate shockwaves which vary in strength from blade to blade around said rotor thereby causing buzz saw noise within said duct, said rotor being produced by a process in which the blades are arranged in a sequence which minimizes the intensity of at least one selected buzz saw noise tone, said process comprising the steps of: (a) measuring said at least one selected dimensional characteristic of each blade to be assembled into said rotor; (b) notionally arranging said blades around said rotor in a chosen sequence; (c) evaluating the shockwave strength at each said blade as arranged in sequence; (d) calculating at least one Fourier coefficient of said shockwave strengths for said sequence, said at least one Fourier coefficient being selected to correspond to said at least one selected buzz saw noise tone; (e) rearranging said blades around said rotor in further sequences and repeating steps (c) and (d) for each such sequence to determine which one of said sequences produces an acceptable minimum value of said at least one Fourier coefficient; and (f) assembling said blades into said rotor such that they are arranged in that one of said sequences for which said minimum value of said at least one Fourier coefficient is obtained.
Claim 3
Dependent Claim 55 words
A rotor according to claim 1 wherein its process steps of production further include the step of: arranging the blades with respect to each other such that differences between the stagger angles of neighboring blades are not more than a predetermined value, thereby minimizing buzz saw noise tones at frequencies other than rotor rotational frequency.
Claim 4
Dependent Claim 41 words
A rotor according to claim 1 wherein its process steps of production further include the step of: arranging the blades with respect to each other such that the moment weight imbalance of the rotor is not more than a predetermined value.
Claim 5
Dependent Claim 16 words
A rotor according to claim 1 wherein said rotor is the fan of a turbofan aeroengine.

References Cited (Backward Citations)

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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1991-03-22 1991-09-21 1992-03-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1995-03-22 1995-09-21 1996-03-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1999-03-22 1999-09-21 2000-03-22 $7700.00 Window Closed / Lapsed

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