US5382134A
Expired / Lapsed
US
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Active noise control using noise source having adaptive resonant frequency tuning through stiffness variation
Assignee: General Electric Co
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Filing: 1993-11-01
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Granted: 1995-01-17
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Expires: 2013-11-01
Abstract
Abstract A noise source for an aircraft engine active noise cancellation system in which the resonant frequency of a noise radiating element is tuned to permit noise cancellation over a wide range of frequencies. The resonant frequency of the noise radiating element is tuned by a plurality of force transmitting mechanisms which contact the noise radiating element. Each one of the force transmitting mechanisms includes an expandable element and a spring in contact with the noise radiating element so that excitation of the element varies the spring force applied to the noise radiating element. The elements are actuated by a controller which receives input of a signal proportional to displacement of the noise radiating element and a signal corresponding to the blade passage frequency of the engine's fan. In response, the controller determines a control signal which is sent to the elements and causes the spring force applied to the noise radiating element to be varied. The force transmitting mechanisms can be arranged to either produce bending or linear stiffness variations in the noise radiating element.
Inventors
- 👤 Frederic G. Pla
- 👤 Harindra Rajiyah
- 👤 Anthony A. Renshaw
- 👤 Robert A. Hedeen
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 19:45
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/04; F02C7/045; B; B64; B64C; B64C11/00; G; G10; G10K; G10K11/00; G10K11/16; G10K11/175; G10K11/178; G10K11/1785; G10K11/17853; G10K11/17854; G10K11/17857; G10K11/1787; G10K11/17879; G10K11/17883; F05; F05D; F05D2260/00; F05D2260/96; F05D2260/962; G10K2210/00; G10K2210/10; G10K2210/107; G10K2210/121; G10K2210/128; G10K2210/1281; G10K2210/30; G10K2210/321; G10K2210/3212; G10K2210/3227; G10K2210/32271; G10K2210/3229; G10K2210/32291; G10K2210/50; G10K2210/512; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 29
Claim 1
Independent Claim
175 words
A noise source for use in an active noise cancellation system which minimizes noise emanating from an aircraft engine having an outer shroud and a fan, said noise source comprising: a noise radiating element mounted to said outer shroud; means for applying a variable force to said noise radiating element; a sensor disposed on said noise radiating element, said sensor producing a feedback signal proportional to displacement of said noise radiating element; means for producing a blade passage frequency signal corresponding to the blade passage frequency of said fan; and a controller having an input connected to said sensor, another input connected to said means for producing a blade passage frequency signal, and an output connected to said means for applying a variable force, said controller being responsive to said feedback signal and said blade passage frequency signal to determine a control signal which is sent to said means for applying a variable force, said control signal causing said means for applying a variable force to vary the force applied to said noise radiating element.
Claim 2
Dependent Claim
175 words
A noise source for use in an active noise cancellation system which minimizes noise emanating from an aircraft engine having an outer shroud and a fan, said noise source comprising: a noise radiating element mounted to said outer shroud; means for applying a variable force to said noise radiating element; a sensor disposed on said noise radiating element, said sensor producing a feedback signal proportional to displacement of said noise radiating element; means for producing a blade passage frequency signal corresponding to the blade passage frequency of said fan; and a controller having an input connected to said sensor, another input connected to said means for producing a blade passage frequency signal, and an output connected to said means for applying a variable force, said controller being responsive to said feedback signal and said blade passage frequency signal to determine a control signal which is sent to said means for applying a variable force, said control signal causing said means for applying a variable force to vary the force applied to said noise radiating element.
Claim 3
Dependent Claim
27 words
The noise source of claim 1 wherein said means for applying a variable force comprises a force transmitting mechanism arranged in contact with said noise radiating element.
Claim 4
Dependent Claim
31 words
The noise source of claim 2 wherein said force transmitting mechanism comprises an expandable element which is excited by said control signal and a spring which contacts said noise radiating element.
Claim 5
Dependent Claim
22 words
The noise source of claim 1 further comprising at least two clamps which support said noise radiating element on said outer shroud.
Claim 6
Dependent Claim
32 words
The noise source of claim 4 wherein said noise radiating element includes a plurality of flanges extending therefrom so that two of said flanges are adjacent to each one of said clamps.
Claim 7
Dependent Claim
26 words
The noise source of claim 5 wherein said means for applying a variable force comprises a force transmitting mechanism associated with each one of said flanges.
Claim 8
Dependent Claim
31 words
The noise source of claim 6 wherein each one of said force transmitting mechanisms comprises an expandable element contacting one of said clamps and a spring contacting one of said flanges.
Claim 9
Dependent Claim
26 words
The noise source of claim 4 wherein said means for applying a variable force comprises two force transmitting mechanisms associated with each one of said clamps.
Claim 10
Dependent Claim
34 words
The noise source of claim 8 wherein each one of said force transmitting mechanisms comprises an expandable element contacting one of said clamps and a spring contacting one side of said noise radiating element.
Claim 11
Dependent Claim
16 words
The noise source of claim 4 wherein said clamps are resiliently mounted to said outer shroud.
Claim 12
Dependent Claim
16 words
The noise source of claim 1 further comprising an actuator disposed on said noise radiating element.
Claim 13
Independent Claim
285 words
An apparatus for minimizing noise emanating from an aircraft engine which has an outer shroud and a fan, said apparatus comprising: a noise radiating element mounted to said outer shroud; means for applying a variable force to said noise radiating element; a sensor disposed on said noise radiating element, said sensor producing a feedback signal proportional to displacement of said noise radiating element; means for producing a blade passage frequency signal corresponding to the blade passage frequency of said fan; a frequency tuning controller having an input connected to said sensor, another input connected to said means for producing a blade passage frequency signal, and an output connected to said means for applying a variable force, said frequency tuning controller being responsive to said feedback signal and said blade passage frequency signal to determine a frequency control signal which is sent to said means for applying a variable force, said frequency control signal causing said means for applying a variable force to vary the force applied to said noise radiating element; means for sensing noise generated by said engine, said means for sensing noise producing an error signal corresponding to the level of noise sensed; and a noise cancellation controller having an input connected to said means for sensing noise, another input connected to said means for producing a blade passage frequency signal, and an output connected to said noise radiating element, said noise cancellation controller being responsive to said error signal and said blade passage frequency signal to determine a noise control signal which is sent to said noise radiating element, said noise control signal causing said noise radiating element to generate a noise field which minimizes the total noise emanating from said engine.
Claim 14
Independent Claim
285 words
An apparatus for minimizing noise emanating from an aircraft engine which has an outer shroud and a fan, said apparatus comprising: a noise radiating element mounted to said outer shroud; means for applying a variable force to said noise radiating element; a sensor disposed on said noise radiating element, said sensor producing a feedback signal proportional to displacement of said noise radiating element; means for producing a blade passage frequency signal corresponding to the blade passage frequency of said fan; a frequency tuning controller having an input connected to said sensor, another input connected to said means for producing a blade passage frequency signal, and an output connected to said means for applying a variable force, said frequency tuning controller being responsive to said feedback signal and said blade passage frequency signal to determine a frequency control signal which is sent to said means for applying a variable force, said frequency control signal causing said means for applying a variable force to vary the force applied to said noise radiating element; means for sensing noise generated by said engine, said means for sensing noise producing an error signal corresponding to the level of noise sensed; and a noise cancellation controller having an input connected to said means for sensing noise, another input connected to said means for producing a blade passage frequency signal, and an output connected to said noise radiating element, said noise cancellation controller being responsive to said error signal and said blade passage frequency signal to determine a noise control signal which is sent to said noise radiating element, said noise control signal causing said noise radiating element to generate a noise field which minimizes the total noise emanating from said engine.
Claim 15
Dependent Claim
26 words
The apparatus of claim 12 wherein said means for applying a variable force comprises a force transmitting mechanism arranged in contact with said noise radiating element.
Claim 16
Dependent Claim
30 words
The apparatus of claim 13 wherein said force transmitting mechanism comprises an expandable element which is excited by said control signal and a spring which contacts said noise radiating element.
Claim 17
Dependent Claim
21 words
The apparatus of claim 12 further comprising at least two clamps which support said noise radiating element on said outer shroud.
Claim 18
Dependent Claim
31 words
The apparatus of claim 15 wherein said noise radiating element includes a plurality of flanges extending therefrom so that two of said flanges are adjacent to each one of said clamps.
Claim 19
Dependent Claim
25 words
The apparatus of claim 16 wherein said means for applying a variable force comprises a force transmitting mechanism associated with each one of said flanges,
Claim 20
Dependent Claim
30 words
The apparatus of claim 17 wherein each one of said force transmitting mechanisms comprises an expandable element contacting one of said clamps and a spring contacting one of said flanges.
Claim 21
Dependent Claim
25 words
The apparatus of claim 15 wherein said means for applying a variable force comprises two force transmitting mechanisms associated with each one of said clamps.
Claim 22
Dependent Claim
33 words
The apparatus of claim 19 wherein each one of said force transmitting mechanisms comprises an expandable element contacting one of said clamps and a spring contacting one side of said noise radiating element.
Claim 23
Dependent Claim
15 words
The apparatus of claim 15 wherein said clamps are resiliently mounted to said outer shroud.
Claim 24
Dependent Claim
26 words
The apparatus of claim 12 wherein said noise radiating element is disposed inside of said outer shroud near a sound port formed in said outer shroud.
Claim 25
Dependent Claim
15 words
The apparatus of claim 12 further comprising an actuator disposed on said noise radiating element.
Claim 26
Independent Claim
83 words
A method for adjusting the resonant frequency of a noise radiating element used in an active noise cancellation system which minimizes noise emanating from an aircraft engine having an outer shroud and a fan, said method comprising the steps of: sensing the displacement of said noise radiating element; sensing the blade passage frequency of said fan; and adjusting the stiffness of the noise radiating element in accordance with the displacement of said noise radiating element and the blade passage frequency of said fan.
Claim 27
Independent Claim
83 words
A method for adjusting the resonant frequency of a noise radiating element used in an active noise cancellation system which minimizes noise emanating from an aircraft engine having an outer shroud and a fan, said method comprising the steps of: sensing the displacement of said noise radiating element; sensing the blade passage frequency of said fan; and adjusting the stiffness of the noise radiating element in accordance with the displacement of said noise radiating element and the blade passage frequency of said fan.
Claim 28
Dependent Claim
28 words
The method of claim 24 wherein said step of adjusting the stiffness of the noise radiating element comprises varying a bending moment applied to said noise radiating element.
Claim 29
Dependent Claim
28 words
The method of claim 24 wherein said step of adjusting the stiffness of the noise radiating element comprises varying a linear force applied to said noise radiating element.
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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) | 1998-01-16 | 1998-07-18 | 1999-01-17 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2002-01-16 | 2002-07-18 | 2003-01-17 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2006-01-16 | 2006-07-18 | 2007-01-17 | $7700.00 | Window Closed / Lapsed |