GB1456018A - Active control of sound waves - Google Patents
Active control of sound wavesInfo
- Publication number
- GB1456018A GB1456018A GB5437072A GB5437072A GB1456018A GB 1456018 A GB1456018 A GB 1456018A GB 5437072 A GB5437072 A GB 5437072A GB 5437072 A GB5437072 A GB 5437072A GB 1456018 A GB1456018 A GB 1456018A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sound
- sources
- attenuated
- sound waves
- microphones
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 230000002238 attenuated effect Effects 0.000 abstract 4
- 230000001902 propagating effect Effects 0.000 abstract 3
- 230000003584 silencer Effects 0.000 abstract 2
- 230000002452 interceptive effect Effects 0.000 abstract 1
- 230000000644 propagated effect Effects 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L55/00—Devices or appurtenances for use in, or in connection with, pipes or pipe systems
- F16L55/02—Energy absorbers; Noise absorbers
- F16L55/033—Noise absorbers
- F16L55/0333—Noise absorbers by means of an active system
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/175—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using interference effects; Masking sound
- G10K11/178—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using interference effects; Masking sound by electro-acoustically regenerating the original acoustic waves in anti-phase
- G10K11/1785—Methods, e.g. algorithms; Devices
- G10K11/17857—Geometric disposition, e.g. placement of microphones
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/175—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using interference effects; Masking sound
- G10K11/178—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using interference effects; Masking sound by electro-acoustically regenerating the original acoustic waves in anti-phase
- G10K11/1787—General system configurations
- G10K11/17873—General system configurations using a reference signal without an error signal, e.g. pure feedforward
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2200/00—Mathematical features
- F05D2200/10—Basic functions
- F05D2200/11—Sum
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
- F05D2260/962—Preventing, counteracting or reducing vibration or noise by means of "anti-noise"
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K2210/00—Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
- G10K2210/10—Applications
- G10K2210/107—Combustion, e.g. burner noise control of jet engines
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K2210/00—Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
- G10K2210/10—Applications
- G10K2210/109—Compressors, e.g. fans
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K2210/00—Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
- G10K2210/10—Applications
- G10K2210/112—Ducts
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K2210/00—Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
- G10K2210/10—Applications
- G10K2210/128—Vehicles
- G10K2210/1281—Aircraft, e.g. spacecraft, airplane or helicopter
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K2210/00—Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
- G10K2210/30—Means
- G10K2210/301—Computational
- G10K2210/3011—Single acoustic input
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K2210/00—Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
- G10K2210/30—Means
- G10K2210/301—Computational
- G10K2210/3042—Parallel processing
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K2210/00—Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
- G10K2210/30—Means
- G10K2210/301—Computational
- G10K2210/3046—Multiple acoustic inputs, multiple acoustic outputs
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K2210/00—Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
- G10K2210/30—Means
- G10K2210/321—Physical
- G10K2210/3219—Geometry of the configuration
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K2210/00—Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
- G10K2210/30—Means
- G10K2210/321—Physical
- G10K2210/3229—Transducers
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K2210/00—Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
- G10K2210/50—Miscellaneous
- G10K2210/506—Feedback, e.g. howling
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Multimedia (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Exhaust Silencers (AREA)
Abstract
1456018 Sound wave attenuation by interference NATIONAL RESEARCH DEVELOPMENT CORP 15 Nov 1973 [24 Nov 1972] 54370/72 Headings FIB, FIG and F1J Apparatus for attenuating sound waves propagating in a duct, e.g. of a jet engine, Fig. 10, comprises an array of sound sources 11, 11a, 11b or 13, 13a, 13b longitudinally spaced relative to the axis of propagation of the sound waves to be attenuated the sources being adjacent the duct walls and the arrangement being such that the resultant of the generated sound waves propagating along the duct in one direction interferes destructively with the sound wave to be attenuated and the resultant of the generated sound waves propagating in the opposite direction is negligible. Detectors 12, 12a, 12b (each consisting of three or four microphones distributed around the duct) detect the sound to be attenuated and by means of an amplifying and delay unit cause signals to energize the sources 11, 11a, 11b (each consisting of three or four loudspeakers). The arrangement of speakers is such as to propagate sound of a particular frequency only towards the inlet orifice of the engine shown, this sound interfering destructively with the sound from the engine. The arrangement of the microphones is the same as that of the loudspeakers so that the microphones are not subject to positive feedback and respond only to the sound wave to be attenuated. At the rear of the engine are detectors 14, 14a, 14b and sources 13, 13a, 13b, comprising microphones and loudspeakers respectively, which behave similarly. In Fig. 11, a rectangular cross-section silencer 22 has sound detectors 23, 23', 23" coupled via amplifying and delay circuitry 25 to loudspeaker sources 24, 24', 24" to produce sound waves to interfere destructively with sound propagated along the silencer 22 from a jet engine 21.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5437072A GB1456018A (en) | 1972-11-24 | 1972-11-24 | Active control of sound waves |
FR7341862A FR2208573A5 (en) | 1972-11-24 | 1973-11-23 | |
DE2358436A DE2358436A1 (en) | 1972-11-24 | 1973-11-23 | METHOD OF ATTENUATING A SOUND FIELD PROPAGATING ALONG A GUIDE |
JP48132110A JPS4997601A (en) | 1972-11-24 | 1973-11-24 | |
US05/607,462 US4044203A (en) | 1972-11-24 | 1975-08-25 | Active control of sound waves |
HK469/80A HK46980A (en) | 1972-11-24 | 1980-08-28 | Active control of sound waves |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5437072A GB1456018A (en) | 1972-11-24 | 1972-11-24 | Active control of sound waves |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1456018A true GB1456018A (en) | 1976-11-17 |
Family
ID=10470785
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5437072A Expired GB1456018A (en) | 1972-11-24 | 1972-11-24 | Active control of sound waves |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPS4997601A (en) |
DE (1) | DE2358436A1 (en) |
FR (1) | FR2208573A5 (en) |
GB (1) | GB1456018A (en) |
HK (1) | HK46980A (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2117046A (en) * | 1982-03-17 | 1983-10-05 | Deutsche Forsch Luft Raumfahrt | Silencing in fluid flow impelling systems |
US4669122A (en) * | 1984-06-21 | 1987-05-26 | National Research Development Corporation | Damping for directional sound cancellation |
GB2191606A (en) * | 1986-04-28 | 1987-12-16 | Rolls Royce Plc | Active control of unsteady motion phenomena in turbomachinery |
GB2204916A (en) * | 1987-05-19 | 1988-11-23 | British Gas Plc | Gaseous flow silencer |
US4967550A (en) * | 1987-04-28 | 1990-11-06 | Rolls-Royce Plc | Active control of unsteady motion phenomena in turbomachinery |
WO1997016816A1 (en) * | 1995-10-30 | 1997-05-09 | Technofirst | Active acoustic attenuation device for use in a duct, particularly for soundproofing a ventilation and/or air-conditioning network |
WO1997020307A1 (en) * | 1995-11-30 | 1997-06-05 | Siemens Electric Limited | System and method for reducing engine noise |
WO2000005494A1 (en) * | 1998-07-22 | 2000-02-03 | Friedmund Nagel | Device and method for actively reducing the noise emissions of jet engines and for diagnosing the same |
US6308914B1 (en) | 1999-03-11 | 2001-10-30 | Gkn Westland Helicopters Limited | Apparatus for the suppression of infra red emissions from an engine |
EP2947649A2 (en) * | 2014-05-22 | 2015-11-25 | WaveScape Technologies GmbH | Assembly for the reduction of sound |
GB2582189A (en) * | 2019-03-12 | 2020-09-16 | Toshiba Kk | System for reducing interference noise of rotor and stator blades, and flight vehicle |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2385972A2 (en) * | 1977-04-01 | 1978-10-27 | Anvar | ACTIVE ACOUSTICAL ABSORBERS FOR DUCTS |
FR2386881A1 (en) * | 1977-04-05 | 1978-11-03 | Sound Attenuators Ltd | Active sound attenuation using secondary wave - has stored programme used to obtain signal representing secondary wave |
JPS5462509A (en) * | 1977-10-27 | 1979-05-19 | Agency Of Ind Science & Technol | Blower-noise reducing method by phase control |
GB8329218D0 (en) * | 1983-11-02 | 1983-12-07 | Ffowcs Williams J E | Reheat combustion system for gas turbine engine |
GB8405914D0 (en) * | 1984-03-07 | 1984-04-11 | Swinbanks M A | Reducing noise by cancellation |
JPS63140897A (en) * | 1986-12-02 | 1988-06-13 | Komatsu Ltd | Transverse blower |
DE4011658A1 (en) * | 1990-04-11 | 1991-10-17 | Messerschmitt Boelkow Blohm | Anti-sound wave generator - incorporates at least fluidic amplifier with input and output connections |
JP2972875B1 (en) | 1998-06-18 | 1999-11-08 | 京都大学長 | Noise reduction device for supersonic jet |
-
1972
- 1972-11-24 GB GB5437072A patent/GB1456018A/en not_active Expired
-
1973
- 1973-11-23 FR FR7341862A patent/FR2208573A5/fr not_active Expired
- 1973-11-23 DE DE2358436A patent/DE2358436A1/en not_active Ceased
- 1973-11-24 JP JP48132110A patent/JPS4997601A/ja active Pending
-
1980
- 1980-08-28 HK HK469/80A patent/HK46980A/en unknown
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2117046A (en) * | 1982-03-17 | 1983-10-05 | Deutsche Forsch Luft Raumfahrt | Silencing in fluid flow impelling systems |
US4669122A (en) * | 1984-06-21 | 1987-05-26 | National Research Development Corporation | Damping for directional sound cancellation |
GB2191606B (en) * | 1986-04-28 | 1991-01-23 | Rolls Royce Plc | Active control of unsteady motion phenomena in turbomachinery |
GB2191606A (en) * | 1986-04-28 | 1987-12-16 | Rolls Royce Plc | Active control of unsteady motion phenomena in turbomachinery |
US4967550A (en) * | 1987-04-28 | 1990-11-06 | Rolls-Royce Plc | Active control of unsteady motion phenomena in turbomachinery |
GB2204916B (en) * | 1987-05-19 | 1991-10-16 | British Gas Plc | A silencer |
GB2204916A (en) * | 1987-05-19 | 1988-11-23 | British Gas Plc | Gaseous flow silencer |
WO1997016816A1 (en) * | 1995-10-30 | 1997-05-09 | Technofirst | Active acoustic attenuation device for use in a duct, particularly for soundproofing a ventilation and/or air-conditioning network |
WO1997020307A1 (en) * | 1995-11-30 | 1997-06-05 | Siemens Electric Limited | System and method for reducing engine noise |
WO2000005494A1 (en) * | 1998-07-22 | 2000-02-03 | Friedmund Nagel | Device and method for actively reducing the noise emissions of jet engines and for diagnosing the same |
US6308914B1 (en) | 1999-03-11 | 2001-10-30 | Gkn Westland Helicopters Limited | Apparatus for the suppression of infra red emissions from an engine |
EP2947649A2 (en) * | 2014-05-22 | 2015-11-25 | WaveScape Technologies GmbH | Assembly for the reduction of sound |
GB2582189A (en) * | 2019-03-12 | 2020-09-16 | Toshiba Kk | System for reducing interference noise of rotor and stator blades, and flight vehicle |
GB2582189B (en) * | 2019-03-12 | 2021-07-28 | Toshiba Kk | System for reducing interference noise of rotor and stator blades, and flight vehicle |
US11415152B2 (en) | 2019-03-12 | 2022-08-16 | Kabushiki Kaisha Toshiba | System for reducing interference noise of rotor and stator blades, and flight vehicle |
Also Published As
Publication number | Publication date |
---|---|
JPS4997601A (en) | 1974-09-14 |
FR2208573A5 (en) | 1974-06-21 |
HK46980A (en) | 1980-09-05 |
DE2358436A1 (en) | 1974-05-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
732 | Registration of transactions, instruments or events in the register (sect. 32/1977) | ||
PE20 | Patent expired after termination of 20 years |
Effective date: 19931114 |