FR2958016B1 - Methode de reduction des instabilites de combustion par le choix du positionnement d'un prelevement d'air sur une turbomachine - Google Patents
Methode de reduction des instabilites de combustion par le choix du positionnement d'un prelevement d'air sur une turbomachineInfo
- Publication number
- FR2958016B1 FR2958016B1 FR1052105A FR1052105A FR2958016B1 FR 2958016 B1 FR2958016 B1 FR 2958016B1 FR 1052105 A FR1052105 A FR 1052105A FR 1052105 A FR1052105 A FR 1052105A FR 2958016 B1 FR2958016 B1 FR 2958016B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- choosing
- positioning
- air tank
- reducing combustion
- 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.)
- Active
Links
- 238000002485 combustion reaction Methods 0.000 title 1
- 238000000034 method Methods 0.000 title 1
Classifications
-
- 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
- F02C7/24—Heat or noise insulation
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M20/00—Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
- F23M20/005—Noise absorbing means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
-
- 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"
-
- 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
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/14—Purpose of the control system to control thermoacoustic behaviour in the combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1052105A FR2958016B1 (fr) | 2010-03-23 | 2010-03-23 | Methode de reduction des instabilites de combustion par le choix du positionnement d'un prelevement d'air sur une turbomachine |
US13/053,779 US20110232288A1 (en) | 2010-03-23 | 2011-03-22 | Method of reducing combustion instabilities by choosing the position of a bleed air intake on a turbomachine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1052105A FR2958016B1 (fr) | 2010-03-23 | 2010-03-23 | Methode de reduction des instabilites de combustion par le choix du positionnement d'un prelevement d'air sur une turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2958016A1 FR2958016A1 (fr) | 2011-09-30 |
FR2958016B1 true FR2958016B1 (fr) | 2017-03-24 |
Family
ID=43567812
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1052105A Active FR2958016B1 (fr) | 2010-03-23 | 2010-03-23 | Methode de reduction des instabilites de combustion par le choix du positionnement d'un prelevement d'air sur une turbomachine |
Country Status (2)
Country | Link |
---|---|
US (1) | US20110232288A1 (fr) |
FR (1) | FR2958016B1 (fr) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8926268B2 (en) | 2012-03-08 | 2015-01-06 | Hamilton Sundstrand Corporation | Bleed noise reduction |
EP3051206B1 (fr) * | 2015-01-28 | 2019-10-30 | Ansaldo Energia Switzerland AG | Agencement de combustion séquentielle d'une turbine à gaz avec un mélangeur et un amortisseur |
US10513984B2 (en) | 2015-08-25 | 2019-12-24 | General Electric Company | System for suppressing acoustic noise within a gas turbine combustor |
US10724739B2 (en) | 2017-03-24 | 2020-07-28 | General Electric Company | Combustor acoustic damping structure |
US10415480B2 (en) | 2017-04-13 | 2019-09-17 | General Electric Company | Gas turbine engine fuel manifold damper and method of dynamics attenuation |
US11149948B2 (en) | 2017-08-21 | 2021-10-19 | General Electric Company | Fuel nozzle with angled main injection ports and radial main injection ports |
US11131252B2 (en) | 2017-09-29 | 2021-09-28 | Pratt & Whitney Canada Corp. | Method and system for operating a gas turbine engine |
US11156162B2 (en) | 2018-05-23 | 2021-10-26 | General Electric Company | Fluid manifold damper for gas turbine engine |
US11506125B2 (en) | 2018-08-01 | 2022-11-22 | General Electric Company | Fluid manifold assembly for gas turbine engine |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2807932A (en) * | 1952-11-25 | 1957-10-01 | Jr Albert G Bodine | Gas turbine with acoustic surge control |
EP0597138B1 (fr) * | 1992-11-09 | 1997-07-16 | Asea Brown Boveri AG | Chambre de combustion pour turbine à gaz |
US5575144A (en) * | 1994-11-28 | 1996-11-19 | General Electric Company | System and method for actively controlling pressure pulses in a gas turbine engine combustor |
US5593277A (en) * | 1995-06-06 | 1997-01-14 | General Electric Company | Smart turbine shroud |
US7272931B2 (en) * | 2003-09-16 | 2007-09-25 | General Electric Company | Method and apparatus to decrease combustor acoustics |
GB2443838B (en) * | 2006-11-16 | 2009-01-28 | Rolls Royce Plc | Combustion control for a gas turbine |
-
2010
- 2010-03-23 FR FR1052105A patent/FR2958016B1/fr active Active
-
2011
- 2011-03-22 US US13/053,779 patent/US20110232288A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
FR2958016A1 (fr) | 2011-09-30 |
US20110232288A1 (en) | 2011-09-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2958016B1 (fr) | Methode de reduction des instabilites de combustion par le choix du positionnement d'un prelevement d'air sur une turbomachine | |
EP2959108A4 (fr) | Turbine à gaz ayant un étage désaccordé | |
FR2970031B1 (fr) | Aube profilee de turbomachine avec passages de refroidissement. | |
BR112014007288A2 (pt) | motor de turbina a gás | |
GB201322857D0 (en) | Turbomachine with blow-off valves located at the intermediate case | |
GB2498006B (en) | Gas turbine engine systems | |
EP2964924A4 (fr) | Entrée de moteur à turbine à gaz | |
GB201121889D0 (en) | Active flow control intake for a gas turbine engine | |
PL390758A1 (pl) | Urządzenie wieszaka tarczy wzmacniającej turbiny do gazowego silnika turbinowego | |
EP2693122A4 (fr) | Chambre de combustion pour un moteur de turbine à gaz et turbine à gaz | |
GB201121887D0 (en) | Intake liner for a gas turbine engine | |
GB201308602D0 (en) | A Shroud Arrangement for a Gas Turbine Engine | |
BR112013030379A2 (pt) | ''motor de turbina a gás compreendendo três corpos rotativos'' | |
GB201308605D0 (en) | A shroud arrangement for a gas turbine engine | |
FR2975037B1 (fr) | Aube de turbomachine composite avec pied integre | |
GB201308603D0 (en) | A Shroud Arrangement for a Gas Turbine Engine | |
EP2713013A4 (fr) | Moteur de turbine à gaz | |
GB201308604D0 (en) | A shroud arrangement for a gas turbine engine | |
FR2967720B1 (fr) | Turbine a vapeur avec arret de flux | |
EP2776677A4 (fr) | Agencement de compresseur de moteur à turbine à gaz | |
FR2975131B1 (fr) | Suspension du canal de flux froid d'un turboreacteur par des biellettes et des chapes radiales sur le carter d'echappement | |
GB201104043D0 (en) | A gas turbine engine | |
SG11201402895RA (en) | Gas turbine engine with low fan pressure ratio | |
SG11201403008WA (en) | Gas turbine engine oil buffering | |
GB2517860B (en) | Turbine engine comprising an upstream attachment means for a de-oiling pipe |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 6 |
|
PLFP | Fee payment |
Year of fee payment: 7 |
|
RM | Correction of a material error |
Effective date: 20160404 |
|
PLFP | Fee payment |
Year of fee payment: 8 |
|
CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
|
PLFP | Fee payment |
Year of fee payment: 9 |
|
PLFP | Fee payment |
Year of fee payment: 10 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
PLFP | Fee payment |
Year of fee payment: 15 |