IT7925254A0 - Metodo ed apparato per sopprimere il rumore a bassa frequenza, generato internamente, di un turbomotore a gas. - Google Patents
Metodo ed apparato per sopprimere il rumore a bassa frequenza, generato internamente, di un turbomotore a gas.Info
- Publication number
- IT7925254A0 IT7925254A0 IT7925254A IT2525479A IT7925254A0 IT 7925254 A0 IT7925254 A0 IT 7925254A0 IT 7925254 A IT7925254 A IT 7925254A IT 2525479 A IT2525479 A IT 2525479A IT 7925254 A0 IT7925254 A0 IT 7925254A0
- Authority
- IT
- Italy
- Prior art keywords
- turboengine
- suppressing
- gas
- low frequency
- frequency noise
- Prior art date
Links
Classifications
-
- 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
- G10K11/161—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general in systems with fluid flow
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Fluid Mechanics (AREA)
- Acoustics & Sound (AREA)
- Multimedia (AREA)
- Exhaust Silencers (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/965,652 US4244440A (en) | 1978-12-01 | 1978-12-01 | Apparatus for suppressing internally generated gas turbine engine low frequency noise |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7925254A0 true IT7925254A0 (it) | 1979-08-21 |
IT1122866B IT1122866B (it) | 1986-04-30 |
Family
ID=25510281
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT25254/79A IT1122866B (it) | 1978-12-01 | 1979-08-21 | Metodo ed apparato per sopprimere il rumore a bassa frequenza,generato internamente,di un turbomotore a gas |
Country Status (6)
Country | Link |
---|---|
US (1) | US4244440A (it) |
JP (1) | JPS5575538A (it) |
DE (1) | DE2934996A1 (it) |
FR (1) | FR2442970B1 (it) |
GB (1) | GB2036875B (it) |
IT (1) | IT1122866B (it) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3339106C1 (de) * | 1983-10-28 | 1985-04-04 | Metronic Electronic GmbH, 7210 Rottweil | Elektromotorisch angetriebenes Geblaese fuer ein Luftsprudelmassagegeraet |
US4733751A (en) * | 1985-12-27 | 1988-03-29 | General Dynamics, Pomona Division | Rocket exhaust disrupter |
US4979587A (en) * | 1989-08-01 | 1990-12-25 | The Boeing Company | Jet engine noise suppressor |
US5929396A (en) * | 1997-07-29 | 1999-07-27 | Awad; Elias A. | Noise reducing diffuser |
GB0000279D0 (en) * | 2000-01-08 | 2000-03-01 | Wood Group Pressure Control Li | Pipe choke |
US6886598B2 (en) * | 2001-01-08 | 2005-05-03 | Wood Group Pressure Control Limited | Choke restrictor devices and methods |
US7469720B2 (en) * | 2003-04-28 | 2008-12-30 | Wood Group Pressure Control Limited | High energy dissipative and erosion resistant fluid flow enhancer |
US7412832B2 (en) * | 2004-03-26 | 2008-08-19 | General Electric Company | Method and apparatus for operating gas turbine engines |
US7246481B2 (en) * | 2004-03-26 | 2007-07-24 | General Electric Company | Methods and apparatus for operating gas turbine engines |
WO2008115173A1 (en) * | 2007-03-15 | 2008-09-25 | Dow Global Technologies Inc. | Mixer for a continuous flow reactor, continuous flow reactor, method of forming such a mixer, and method of operating such a reactor |
GB201007215D0 (en) | 2010-04-30 | 2010-06-16 | Rolls Royce Plc | Gas turbine engine |
CA2898486C (en) * | 2010-05-20 | 2018-04-24 | William Matthew Martin | Method and device for in-line injection of flocculent agent into a fluid flow of mature fine tailings |
US8307943B2 (en) | 2010-07-29 | 2012-11-13 | General Electric Company | High pressure drop muffling system |
US8430202B1 (en) | 2011-12-28 | 2013-04-30 | General Electric Company | Compact high-pressure exhaust muffling devices |
US8511096B1 (en) | 2012-04-17 | 2013-08-20 | General Electric Company | High bleed flow muffling system |
US9399951B2 (en) | 2012-04-17 | 2016-07-26 | General Electric Company | Modular louver system |
US8550208B1 (en) | 2012-04-23 | 2013-10-08 | General Electric Company | High pressure muffling devices |
US10794515B2 (en) * | 2017-12-14 | 2020-10-06 | Thomas A. Hartman | Valve or pipe discharge with velocity reduction discharge plate |
USD853274S1 (en) * | 2018-02-08 | 2019-07-09 | In The Black Revocable Trust | Planter |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2915136A (en) * | 1956-05-28 | 1959-12-01 | Friedrich O Ringleb | Apparatus for suppressing noise |
US2987883A (en) * | 1959-06-22 | 1961-06-13 | Boeing Co | Jet engine noise suppression nozzle with aerodynamic supplemental fluting |
US3033307A (en) * | 1959-10-06 | 1962-05-08 | Industrial Acoustics Co | Noise attenuating apparatus |
US3392529A (en) * | 1965-07-23 | 1968-07-16 | Rolls Royce | Aircraft provided with a gas turbine vertical lift engine |
GB1110154A (en) * | 1966-04-05 | 1968-04-18 | Rolls Royce | Aircraft jet power plant |
US3495682A (en) * | 1968-02-28 | 1970-02-17 | Otis D Treiber | Jet engine exhaust silencer construction |
FR1580553A (it) * | 1968-07-26 | 1969-09-05 | ||
US3630311A (en) * | 1969-07-31 | 1971-12-28 | Gen Electric | Jet engine nozzle system for noise suppression |
FR2094212A5 (it) * | 1970-05-11 | 1972-02-04 | Bertin & Cie | |
FR2214855B1 (it) * | 1973-01-22 | 1976-04-30 | Aerospatiale | |
US3987883A (en) * | 1975-04-17 | 1976-10-26 | International Business Machines Corporation | Ribbon lifting mechanism for a wire matrix printer |
US4064961A (en) * | 1976-04-05 | 1977-12-27 | Rohr Industries, Incorporated | Slanted cavity resonator |
US4135363A (en) * | 1976-05-13 | 1979-01-23 | United Technologies Corporation | Device to provide flow inversion in a turbofan exhaust tailpipe to achieve low jet noise |
US4109750A (en) * | 1977-05-24 | 1978-08-29 | Lockheed Aircraft Corporation | Zeno duct sound attenuating means |
-
1978
- 1978-12-01 US US05/965,652 patent/US4244440A/en not_active Expired - Lifetime
-
1979
- 1979-07-02 GB GB7922990A patent/GB2036875B/en not_active Expired
- 1979-08-21 IT IT25254/79A patent/IT1122866B/it active
- 1979-08-28 FR FR7921582A patent/FR2442970B1/fr not_active Expired
- 1979-08-30 DE DE19792934996 patent/DE2934996A1/de not_active Ceased
- 1979-08-31 JP JP11049979A patent/JPS5575538A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
FR2442970A1 (fr) | 1980-06-27 |
DE2934996A1 (de) | 1980-06-12 |
IT1122866B (it) | 1986-04-30 |
US4244440A (en) | 1981-01-13 |
GB2036875B (en) | 1982-09-29 |
JPS5575538A (en) | 1980-06-06 |
JPH0319366B2 (it) | 1991-03-14 |
GB2036875A (en) | 1980-07-02 |
FR2442970B1 (fr) | 1985-06-07 |
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