GB0008471D0 - Gas turbine engine noise suppression - Google Patents
Gas turbine engine noise suppressionInfo
- Publication number
- GB0008471D0 GB0008471D0 GBGB0008471.5A GB0008471A GB0008471D0 GB 0008471 D0 GB0008471 D0 GB 0008471D0 GB 0008471 A GB0008471 A GB 0008471A GB 0008471 D0 GB0008471 D0 GB 0008471D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- turbine engine
- noise suppression
- engine noise
- suppression
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/663—Sound attenuation
- F04D29/665—Sound attenuation by means of resonance chambers or interference
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/16—Form or construction for counteracting blade vibration
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/388—Blades characterised by construction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0008471A GB2361035A (en) | 2000-04-07 | 2000-04-07 | Gas turbine engine vane with noise attenuation features |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0008471A GB2361035A (en) | 2000-04-07 | 2000-04-07 | Gas turbine engine vane with noise attenuation features |
Publications (2)
Publication Number | Publication Date |
---|---|
GB0008471D0 true GB0008471D0 (en) | 2000-05-24 |
GB2361035A GB2361035A (en) | 2001-10-10 |
Family
ID=9889350
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0008471A Withdrawn GB2361035A (en) | 2000-04-07 | 2000-04-07 | Gas turbine engine vane with noise attenuation features |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2361035A (en) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7018172B2 (en) * | 2003-12-22 | 2006-03-28 | United Technologies Corporation | Airfoil surface impedance modification for noise reduction in turbofan engines |
DE102004017096A1 (en) * | 2004-04-07 | 2005-10-27 | Mtu Aero Engines Gmbh | Strut for a turbine engine |
DE102006042647A1 (en) | 2006-09-12 | 2008-03-27 | Mtu Aero Engines Gmbh | Turbine of a gas turbine |
FR2911923B1 (en) * | 2007-01-25 | 2011-07-08 | Snecma | ACOUSTIC RECTIFIER FOR TURBOREACTOR BLOWER CASING |
US7607287B2 (en) | 2007-05-29 | 2009-10-27 | United Technologies Corporation | Airfoil acoustic impedance control |
JP6356801B2 (en) * | 2013-11-14 | 2018-07-11 | ゼネラル・エレクトリック・カンパニイ | Turbine component with negative CTE characteristics |
GB201707836D0 (en) | 2017-05-16 | 2017-06-28 | Oscar Propulsion Ltd | Outlet guide vanes |
EP3799030A1 (en) * | 2019-09-26 | 2021-03-31 | Rolls-Royce Deutschland Ltd & Co KG | Acoustic liner and gas turbine engine with such acoustic liner |
US11199107B2 (en) | 2020-04-13 | 2021-12-14 | Raytheon Technologies Corporation | Airfoil-mounted resonator |
US11566564B2 (en) | 2020-07-08 | 2023-01-31 | Raytheon Technologies Corporation | Acoustically treated panels |
US11230928B1 (en) | 2020-07-22 | 2022-01-25 | Raytheon Technologies Corporation | Guide vane with truss structure and honeycomb |
US11512608B2 (en) | 2020-08-14 | 2022-11-29 | Raytheon Technologies Corporation | Passive transpirational flow acoustically lined guide vane |
US11408349B2 (en) | 2020-08-14 | 2022-08-09 | Raytheon Technologies Corporation | Active flow control transpirational flow acoustically lined guide vane |
US12118971B2 (en) | 2021-05-12 | 2024-10-15 | B/E Aerospace, Inc. | Aircraft acoustic panel |
US11804206B2 (en) | 2021-05-12 | 2023-10-31 | Goodrich Corporation | Acoustic panel for noise attenuation |
US12104536B2 (en) | 2021-05-12 | 2024-10-01 | Rohr, Inc. | Nacelle liner comprising unit cell resonator networks |
US11830467B2 (en) | 2021-10-16 | 2023-11-28 | Rtx Coroporation | Unit cell resonator networks for turbomachinery bypass flow structures |
US11781485B2 (en) | 2021-11-24 | 2023-10-10 | Rtx Corporation | Unit cell resonator networks for gas turbine combustor tone damping |
US11965425B2 (en) | 2022-05-31 | 2024-04-23 | General Electric Company | Airfoil for a turbofan engine |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1350686A (en) * | 1970-09-04 | 1974-04-18 | Gen Electric | Aircraft gas turbine engines |
GB1522558A (en) * | 1976-04-05 | 1978-08-23 | Rolls Royce | Duct linings |
GB2026622A (en) * | 1978-07-08 | 1980-02-06 | Rolls Royce | Blade for Fluid Flow Machine |
US4235303A (en) * | 1978-11-20 | 1980-11-25 | The Boeing Company | Combination bulk absorber-honeycomb acoustic panels |
US5810552A (en) * | 1992-02-18 | 1998-09-22 | Allison Engine Company, Inc. | Single-cast, high-temperature, thin wall structures having a high thermal conductivity member connecting the walls and methods of making the same |
US5626462A (en) * | 1995-01-03 | 1997-05-06 | General Electric Company | Double-wall airfoil |
-
2000
- 2000-04-07 GB GB0008471A patent/GB2361035A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2361035A (en) | 2001-10-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |