US4419045A
Expired / Lapsed
US
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Method and device for reducing the noise of turbo-machines
Assignee: Safran Aircraft Engines SAS
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Filing: 1980-07-18
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Granted: 1983-12-06
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Expires: 2000-07-18
Abstract
Abstract A method and device for reducing the noise produced in a turbo-machine by e interaction of the blades of a ring of rotor blades and the vanes of a ring of stator vanes, by the creation of a counter-noise of opposed phase. This is achieved by the injection of a fluid into the flow passage of the machine in which the blades and vanes are located. The injection is carried out through orifices located on stationary parts of the machine and equal in number to the vanes of ring of stator vanes, the flow through the orifices being modulated at the frequency of the noise to be reduced and with a phase difference which increase in an incremental manner from one orifice to the next. The phase of the modulated flows injected through the orifices is simultaneously regulated so that the acoustic waves created by the flows are substantially in opposition, with respect to phase, to those of the noise to be reduced.
Inventors
- 👤 Pierre A. Andre
- 👤 Jean-Claude P. H. P. Thevenin
- 👤 Jean-Pierre Y. B. Girault
- 👤 Gerhard Richter
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 18:38
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/04; F02C7/045; F04; F04D; F04D29/00; F04D29/66; F04D29/661; G; G10; G10K; G10K11/00; G10K11/16; G10K11/175; G10K11/178; G10K11/1785; G10K11/1787; F05; F05D; F05D2260/00; F05D2260/96; F05D2260/962; G10K2210/00; G10K2210/10; G10K2210/121; G10K2210/128; G10K2210/1281; G10K2210/30; G10K2210/301; G10K2210/3031; G10K2210/321; G10K2210/3212; G10K2210/32121; Y; Y10; Y10S; Y10S415/00; Y10S415/914
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
284 words
In a turbo-machine which includes an elongated, hollow, stationary outer wall, a rotatable rotor ring mounted centrally inside of said outer wall and comprising an elongated rotor shaft and a number of radial rotor blades extending from said rotor shaft towards said stationary outer wall, and a stationary stator having a number of radial stator vanes extending towards said stationary outer wall, the improvement wherein said turbo-machine includes an apparatus for reducing the noise generated by the interaction of the rotating rotor blades and the stationary stator vanes by creating a counter-noise of opposed phase, this apparatus comprising: a plurality of injection orifices located in said stationary outer wall and distributed around the circumference thereof, the number of injection orifices being equal to the number of vanes in said stator ring, means forming a toroidal manifold surrounding said stationary outer wall, means for supplying a constant flow of fluid to said toroidal manifold, a plurality of feed pipes distributed around the circumference of said toroidal manifold, each feed pipe interconnecting with a respective injection orifice, a movable flow regulator shutter in each feed pipe, and means to move said flow regulator shutter in each feed pipe, each said means to move the flow regulator shutter in each feed pipe including a solenoid, a rod connected between the solenoid and the shutter, at least one sensing device mounted in said stationary outer wall responsive to the passage frequency of said moving rotor blades, and means for supplying electrical current in response to said sensing means to each said solenoid to operate said solenoid and move said rod and the attached shutter in response to on the passage of the rotor blades past the sensing device.
Claim 2
Dependent Claim
284 words
In a turbo-machine which includes an elongated, hollow, stationary outer wall, a rotatable rotor ring mounted centrally inside of said outer wall and comprising an elongated rotor shaft and a number of radial rotor blades extending from said rotor shaft towards said stationary outer wall, and a stationary stator having a number of radial stator vanes extending towards said stationary outer wall, the improvement wherein said turbo-machine includes an apparatus for reducing the noise generated by the interaction of the rotating rotor blades and the stationary stator vanes by creating a counter-noise of opposed phase, this apparatus comprising: a plurality of injection orifices located in said stationary outer wall and distributed around the circumference thereof, the number of injection orifices being equal to the number of vanes in said stator ring, means forming a toroidal manifold surrounding said stationary outer wall, means for supplying a constant flow of fluid to said toroidal manifold, a plurality of feed pipes distributed around the circumference of said toroidal manifold, each feed pipe interconnecting with a respective injection orifice, a movable flow regulator shutter in each feed pipe, and means to move said flow regulator shutter in each feed pipe, each said means to move the flow regulator shutter in each feed pipe including a solenoid, a rod connected between the solenoid and the shutter, at least one sensing device mounted in said stationary outer wall responsive to the passage frequency of said moving rotor blades, and means for supplying electrical current in response to said sensing means to each said solenoid to operate said solenoid and move said rod and the attached shutter in response to on the passage of the rotor blades past the sensing device.
Claim 3
Dependent Claim
231 words
In a turbo-machine which includes an elongated, hollow, stationary outer wall, a rotatable rotor ring mounted centrally inside of said outer wall and comprising an elongated rotor shaft and a number of radial rotor blades extending from said rotor shaft towards siad stationary outer wall, and a stationary stator ring having a number of radial stator vanes extending towards said stationary outer wall, the improvement wherein said turbo-machine includes an apparatus for reducing the noise generated by the interaction of the rotating rotor blades and the stationary stator vanes by creating a counter-noise of opposed phase, this apparatus comprising: a hollow air flow divider means positioned between said rotor shaft and said stationary outer wall so as to define an outer fan duct and an inner primary flow channel, wherein said radial stator vanes extend between said air flow divider means and said stationary outer wall, a plurality of injection orifices located in said air flow divider means to communicate with said outer fan duct, means forming a toroidal manifold within said hollow air flow divider means, means supplying a constant flow of fluid to said toroidal manifold, a plurality of feed pipes distributed around the circumference of said toroidal manifold, each feed pipe interconnecting with a respective injection orifice, a movable flow regulator shutter in each feed pipe, and means to move said flow regulator shutter in each feed pipe.
Claim 4
Dependent Claim
231 words
In a turbo-machine which includes an elongated, hollow, stationary outer wall, a rotatable rotor ring mounted centrally inside of said outer wall and comprising an elongated rotor shaft and a number of radial rotor blades extending from said rotor shaft towards siad stationary outer wall, and a stationary stator ring having a number of radial stator vanes extending towards said stationary outer wall, the improvement wherein said turbo-machine includes an apparatus for reducing the noise generated by the interaction of the rotating rotor blades and the stationary stator vanes by creating a counter-noise of opposed phase, this apparatus comprising: a hollow air flow divider means positioned between said rotor shaft and said stationary outer wall so as to define an outer fan duct and an inner primary flow channel, wherein said radial stator vanes extend between said air flow divider means and said stationary outer wall, a plurality of injection orifices located in said air flow divider means to communicate with said outer fan duct, means forming a toroidal manifold within said hollow air flow divider means, means supplying a constant flow of fluid to said toroidal manifold, a plurality of feed pipes distributed around the circumference of said toroidal manifold, each feed pipe interconnecting with a respective injection orifice, a movable flow regulator shutter in each feed pipe, and means to move said flow regulator shutter in each feed pipe.
Claim 5
Dependent Claim
75 words
A turbo-machine according to claim 2 wherein each said means to move the flow regulator shutter in each feed pipe includes a solenoid, a rod connected between the solenoid and the shutter, at least one sensing device mounted in said stationary outer wall, and means for supplying electrical current to each said solenoid to operate said solenoid and move said rod and the attached shutter based on the passage of the rotor past the device.
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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) | 1986-12-05 | 1987-06-06 | 1987-12-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1990-12-05 | 1991-06-06 | 1991-12-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1994-12-05 | 1995-06-06 | 1995-12-06 | $7700.00 | Window Closed / Lapsed |