GB2476855B - Acoustic liner and heat exchanger for gas turbine inlet duct - Google Patents
Acoustic liner and heat exchanger for gas turbine inlet ductInfo
- Publication number
- GB2476855B GB2476855B GB1016602.3A GB201016602A GB2476855B GB 2476855 B GB2476855 B GB 2476855B GB 201016602 A GB201016602 A GB 201016602A GB 2476855 B GB2476855 B GB 2476855B
- Authority
- GB
- United Kingdom
- Prior art keywords
- heat exchanger
- gas turbine
- inlet duct
- turbine inlet
- acoustic liner
- 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 - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0206—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1016602.3A GB2476855B (en) | 2009-11-27 | 2010-10-04 | Acoustic liner and heat exchanger for gas turbine inlet duct |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB0920741.6A GB0920741D0 (en) | 2009-11-27 | 2009-11-27 | Air flow passage liner |
| GB1016602.3A GB2476855B (en) | 2009-11-27 | 2010-10-04 | Acoustic liner and heat exchanger for gas turbine inlet duct |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB201016602D0 GB201016602D0 (en) | 2010-11-17 |
| GB2476855A GB2476855A (en) | 2011-07-13 |
| GB2476855B true GB2476855B (en) | 2012-05-02 |
Family
ID=43243407
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1016602.3A Expired - Fee Related GB2476855B (en) | 2009-11-27 | 2010-10-04 | Acoustic liner and heat exchanger for gas turbine inlet duct |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2476855B (en) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2519501A (en) * | 2013-08-01 | 2015-04-29 | Rolls Royce Plc | Acoustic liner |
| FR3041704B1 (en) | 2015-09-29 | 2017-11-03 | Snecma | THERMAL EXCHANGE AND NOISE REDUCTION PANEL FOR A PROPULSIVE ASSEMBLY |
| GB2547049B (en) | 2016-02-08 | 2019-12-25 | Gkn Aerospace Services Ltd | Integrated heater |
| FR3051019B1 (en) | 2016-05-03 | 2020-01-10 | Airbus Operations | STRUCTURE PROVIDING ACOUSTIC WAVE ATTENUATION AND HEAT EXCHANGE |
| US10619570B2 (en) | 2017-11-14 | 2020-04-14 | The Boeing Company | Dendritic heat exchangers and methods of utilizing the same |
| US11060480B2 (en) | 2017-11-14 | 2021-07-13 | The Boeing Company | Sound-attenuating heat exchangers and methods of utilizing the same |
| US11525438B2 (en) | 2019-06-28 | 2022-12-13 | The Boeing Company | Shape memory alloy actuators and thermal management systems including the same |
| US11168584B2 (en) | 2019-06-28 | 2021-11-09 | The Boeing Company | Thermal management system using shape memory alloy actuator |
| US11143170B2 (en) | 2019-06-28 | 2021-10-12 | The Boeing Company | Shape memory alloy lifting tubes and shape memory alloy actuators including the same |
| FR3127989A1 (en) * | 2021-10-13 | 2023-04-14 | Airbus | AIRCRAFT PROPULSION SET |
| US12259196B2 (en) | 2022-06-16 | 2025-03-25 | The Boeing Company | Sound-attenuating heat exchangers and methods of exchanging heat and attenuating sound within sound-attenuating heat exchangers |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5743488A (en) * | 1994-12-05 | 1998-04-28 | Short Brothers Plc | Aerodynamic low drag structure |
| GB2410769A (en) * | 2004-02-05 | 2005-08-10 | Rolls Royce Plc | Engine cooling |
| US20060042225A1 (en) * | 2004-08-27 | 2006-03-02 | Pratt & Whitney Canada Corp. | Bypass duct fluid cooler |
| EP1860301A2 (en) * | 2006-05-26 | 2007-11-28 | United Technologies Corporation | Micro-perforated acoustic liner |
| EP2026325A2 (en) * | 2007-08-15 | 2009-02-18 | Rohr, Inc. | Linear acoustic liner |
| EP2206893A2 (en) * | 2008-12-23 | 2010-07-14 | General Electric Company | Combined Surface Cooler and Acoustic Absorber for Turbomachines |
-
2010
- 2010-10-04 GB GB1016602.3A patent/GB2476855B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5743488A (en) * | 1994-12-05 | 1998-04-28 | Short Brothers Plc | Aerodynamic low drag structure |
| GB2410769A (en) * | 2004-02-05 | 2005-08-10 | Rolls Royce Plc | Engine cooling |
| US20060042225A1 (en) * | 2004-08-27 | 2006-03-02 | Pratt & Whitney Canada Corp. | Bypass duct fluid cooler |
| EP1860301A2 (en) * | 2006-05-26 | 2007-11-28 | United Technologies Corporation | Micro-perforated acoustic liner |
| EP2026325A2 (en) * | 2007-08-15 | 2009-02-18 | Rohr, Inc. | Linear acoustic liner |
| EP2206893A2 (en) * | 2008-12-23 | 2010-07-14 | General Electric Company | Combined Surface Cooler and Acoustic Absorber for Turbomachines |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2476855A (en) | 2011-07-13 |
| GB201016602D0 (en) | 2010-11-17 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB2476855B (en) | Acoustic liner and heat exchanger for gas turbine inlet duct | |
| PL2591220T3 (en) | Gas turbine architecture with heat exchanger built into the exhaust | |
| GB2437377B (en) | A gas turbine engine heat exchanger arrangement | |
| GB2474567B (en) | Gas turbine engine temperature modulated cooling flow | |
| EP2655842A4 (en) | GAS TURBINE ENGINE HEAT EXCHANGER | |
| EP2519723A4 (en) | GAS TURBINE ENGINE AND HEAT EXCHANGER SYSTEM | |
| EP2770290A4 (en) | HEAT EXCHANGER OF EXHAUST GAS | |
| EP2419621A4 (en) | System and method for managing thermal issues in gas turbine engines | |
| GB2452476B (en) | Acoustic liner for gas turbine engine and method of manufacture thereof | |
| GB0813820D0 (en) | A fan casing for a gas turbine engine | |
| PL2324217T3 (en) | Combination of a heat exchanger and catalyst as a component of an exhaust gas system | |
| EP2256297B8 (en) | Gas turbine vane with improved cooling | |
| IL220266A0 (en) | A burner system and a method for increasing the efficiency of a heat exchanger | |
| GB0813821D0 (en) | A fan casing for a gas turbine engine | |
| GB0809759D0 (en) | Gas turbine engine | |
| EP2577031A4 (en) | Exhaust gas heat recovery heat exchanger | |
| EP2325459A4 (en) | COOLING AIR SUPPLY STRUCTURE FOR GAS TURBINE AND GAS TURBINE | |
| GB2473651B (en) | Gas turbine aircraft engines and operation thereof | |
| GB0903935D0 (en) | Gas turbine engine | |
| EP2589770A4 (en) | Seal air supply apparatus and exhaust gas turbine supercharger using seal air supply apparatus | |
| EP2565400A3 (en) | Exhaust gas duct for a gas turbine with heat resistant liner and gas turbine having such a gas duct | |
| GB0908128D0 (en) | An intake duct liner for a turbofan gas turbine engine | |
| GB0912270D0 (en) | System for cooling cooling-air in a gas turbine engine | |
| EP2148065A4 (en) | Gas turbine engine | |
| GB201300867D0 (en) | Air inlet duct for a turbojet nacelle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20211004 |