FR2992018B1 - Montage d'un distributeur de turbine haute-pression sur une chambre a combustion d'une turbomachine - Google Patents
Montage d'un distributeur de turbine haute-pression sur une chambre a combustion d'une turbomachineInfo
- Publication number
- FR2992018B1 FR2992018B1 FR1255637A FR1255637A FR2992018B1 FR 2992018 B1 FR2992018 B1 FR 2992018B1 FR 1255637 A FR1255637 A FR 1255637A FR 1255637 A FR1255637 A FR 1255637A FR 2992018 B1 FR2992018 B1 FR 2992018B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- mounting
- combustion chamber
- pressure turbine
- dispenser
- 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
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
Classifications
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- 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
- F23R3/60—Support structures; Attaching or mounting means
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1255637A FR2992018B1 (fr) | 2012-06-15 | 2012-06-15 | Montage d'un distributeur de turbine haute-pression sur une chambre a combustion d'une turbomachine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1255637A FR2992018B1 (fr) | 2012-06-15 | 2012-06-15 | Montage d'un distributeur de turbine haute-pression sur une chambre a combustion d'une turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2992018A1 FR2992018A1 (fr) | 2013-12-20 |
FR2992018B1 true FR2992018B1 (fr) | 2016-05-06 |
Family
ID=46579138
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1255637A Active FR2992018B1 (fr) | 2012-06-15 | 2012-06-15 | Montage d'un distributeur de turbine haute-pression sur une chambre a combustion d'une turbomachine |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2992018B1 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102015212573A1 (de) | 2015-07-06 | 2017-01-12 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammer mit integriertem Turbinenvorleitrad sowie Verfahren zu deren Herstellung |
US11248789B2 (en) | 2018-12-07 | 2022-02-15 | Raytheon Technologies Corporation | Gas turbine engine with integral combustion liner and turbine nozzle |
FR3107108B1 (fr) | 2020-02-11 | 2022-07-08 | Safran Aircraft Engines | Ensemble COMPRENANT un carter et une chambre de combustion, et turbomachine ainsi equipee |
FR3107106B1 (fr) | 2020-02-11 | 2022-07-08 | Safran Aircraft Engines | Ensemble COMPRENANT un carter et une chambre de combustion, et turbomachine ainsi equipee |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2672013A (en) * | 1950-06-30 | 1954-03-16 | Curtiss Wright Corp | Gas turbine cooling system |
US3018624A (en) * | 1954-03-02 | 1962-01-30 | Bristol Siddeley Engines Ltd | Flame tubes for use in combustion systems of gas turbine engines |
US2994509A (en) * | 1959-04-10 | 1961-08-01 | Curtiss Wright Corp | Variable area turbine nozzle |
DE19629191C2 (de) * | 1996-07-19 | 1998-05-14 | Siemens Ag | Verfahren zur Kühlung einer Gasturbine |
FR2871847B1 (fr) * | 2004-06-17 | 2006-09-29 | Snecma Moteurs Sa | Montage d'un distributeur de turbine sur une chambre de combustion a parois en cmc dans une turbine a gaz |
FR2871844B1 (fr) * | 2004-06-17 | 2006-09-29 | Snecma Moteurs Sa | Montage etanche d'un distributeur de turbine haute pression sur une extremite d'une chambre de combustion dans une turbine a gaz |
-
2012
- 2012-06-15 FR FR1255637A patent/FR2992018B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR2992018A1 (fr) | 2013-12-20 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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CD | Change of name or company name |
Owner name: SNECMA, FR Effective date: 20170713 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170717 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |