DE2309715A1 - Gasturbinentriebwerk mit flaechensteuerungseinsatz - Google Patents
Gasturbinentriebwerk mit flaechensteuerungseinsatzInfo
- Publication number
- DE2309715A1 DE2309715A1 DE19732309715 DE2309715A DE2309715A1 DE 2309715 A1 DE2309715 A1 DE 2309715A1 DE 19732309715 DE19732309715 DE 19732309715 DE 2309715 A DE2309715 A DE 2309715A DE 2309715 A1 DE2309715 A1 DE 2309715A1
- Authority
- DE
- Germany
- Prior art keywords
- wall
- flow
- hood
- control insert
- area control
- 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.)
- Pending
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 238000002485 combustion reaction Methods 0.000 claims description 28
- 238000009434 installation Methods 0.000 claims description 2
- 239000007789 gas Substances 0.000 description 14
- 238000000926 separation method Methods 0.000 description 13
- 238000001816 cooling Methods 0.000 description 7
- 238000005253 cladding Methods 0.000 description 6
- 238000013461 design Methods 0.000 description 5
- 230000006866 deterioration Effects 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 230000006378 damage Effects 0.000 description 4
- 230000009467 reduction Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 239000000567 combustion gas Substances 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000013021 overheating Methods 0.000 description 2
- 239000003351 stiffener Substances 0.000 description 2
- 102100023121 Ninein Human genes 0.000 description 1
- 101710196576 Ninein Proteins 0.000 description 1
- 230000001154 acute effect Effects 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000010790 dilution Methods 0.000 description 1
- 239000012895 dilution Substances 0.000 description 1
- 238000002845 discoloration Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 108090000623 proteins and genes Proteins 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
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)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US23083972A | 1972-03-01 | 1972-03-01 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE2309715A1 true DE2309715A1 (de) | 1973-09-13 |
Family
ID=22866779
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19732309715 Pending DE2309715A1 (de) | 1972-03-01 | 1973-02-27 | Gasturbinentriebwerk mit flaechensteuerungseinsatz |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US3750397A (enExample) |
| JP (1) | JPS48100515A (enExample) |
| BE (1) | BE795867A (enExample) |
| CA (1) | CA963675A (enExample) |
| DE (1) | DE2309715A1 (enExample) |
| FR (1) | FR2174069B3 (enExample) |
| IT (1) | IT979502B (enExample) |
Families Citing this family (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4098074A (en) * | 1976-06-01 | 1978-07-04 | United Technologies Corporation | Combustor diffuser for turbine type power plant and construction thereof |
| US4373327A (en) * | 1979-07-04 | 1983-02-15 | Rolls-Royce Limited | Gas turbine engine combustion chambers |
| US4512158A (en) * | 1983-06-16 | 1985-04-23 | United Technologies Corporation | High blockage diffuser with means for minimizing wakes |
| US5077967A (en) * | 1990-11-09 | 1992-01-07 | General Electric Company | Profile matched diffuser |
| US5142871A (en) * | 1991-01-22 | 1992-09-01 | General Electric Company | Combustor dome plate support having uniform thickness arcuate apex with circumferentially spaced coolant apertures |
| CA2070518C (en) * | 1991-07-01 | 2001-10-02 | Adrian Mark Ablett | Combustor dome assembly |
| US5289687A (en) * | 1992-03-30 | 1994-03-01 | General Electric Company | One-piece cowl for a double annular combustor |
| FR2706534B1 (fr) * | 1993-06-10 | 1995-07-21 | Snecma | Diffuseur-séparateur multiflux avec redresseur intégré pour turboréacteur. |
| DE19539771B4 (de) * | 1995-10-26 | 2006-10-05 | Alstom | Gasturbine |
| US6513330B1 (en) | 2000-11-08 | 2003-02-04 | Allison Advanced Development Company | Diffuser for a gas turbine engine |
| US6401447B1 (en) | 2000-11-08 | 2002-06-11 | Allison Advanced Development Company | Combustor apparatus for a gas turbine engine |
| GB2391297A (en) * | 2002-07-24 | 2004-02-04 | Rolls Royce Plc | Gas supply assembly |
| US6952927B2 (en) * | 2003-05-29 | 2005-10-11 | General Electric Company | Multiport dome baffle |
| US8500399B2 (en) * | 2006-04-25 | 2013-08-06 | Rolls-Royce Corporation | Method and apparatus for enhancing compressor performance |
| GB0618991D0 (en) * | 2006-09-27 | 2006-11-08 | Rolls Royce Plc | A component for a gas turbine engine |
| FR2920524B1 (fr) * | 2007-08-30 | 2013-11-01 | Snecma | Turbomachine a chambre annulaire de combustion |
| US9046272B2 (en) * | 2008-12-31 | 2015-06-02 | Rolls-Royce Corporation | Combustion liner assembly having a mount stake coupled to an upstream support |
| FR2943726B1 (fr) * | 2009-03-31 | 2014-04-25 | Snecma | Capot d'entree tournant pour turbomachine, comprenant une extremite avant excentree |
| GB201001974D0 (en) * | 2010-02-08 | 2010-03-24 | Rolls Royce Plc | An outlet guide vane structure |
| EP2410138B8 (en) * | 2010-07-22 | 2017-07-19 | Ansaldo Energia IP UK Limited | Gas turbine engine flange arrangement and method for retrofitting same |
| FR2964725B1 (fr) * | 2010-09-14 | 2012-10-12 | Snecma | Carenage aerodynamique pour fond de chambre de combustion |
| EP2901082B1 (en) * | 2012-09-28 | 2019-11-06 | United Technologies Corporation | Inner diffuser case struts for a combustor of a gas turbine engine |
| US10190603B2 (en) | 2012-12-29 | 2019-01-29 | Spar Energy Llc | Power generation from atmospheric air pressure |
| US9938963B2 (en) * | 2012-12-29 | 2018-04-10 | Spar Energy Llc | Power generation from atmospheric air pressure |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3049882A (en) * | 1960-05-16 | 1962-08-21 | Gen Electric | Combustor construction with means for prevention of hot streaks |
| GB1040390A (en) * | 1965-07-12 | 1966-08-24 | Rolls Royce | Gas turbine engine |
| US3364678A (en) * | 1966-02-28 | 1968-01-23 | Gen Electric | Means for stabilizing fluid flow in diffuser-combustor systems in axial flow gas turbine engines |
| US3372542A (en) * | 1966-11-25 | 1968-03-12 | United Aircraft Corp | Annular burner for a gas turbine |
| US3589127A (en) * | 1969-02-04 | 1971-06-29 | Gen Electric | Combustion apparatus |
| US3581492A (en) * | 1969-07-08 | 1971-06-01 | Nasa | Gas turbine combustor |
| US3631674A (en) * | 1970-01-19 | 1972-01-04 | Gen Electric | Folded flow combustion chamber for a gas turbine engine |
-
0
- BE BE795867D patent/BE795867A/xx unknown
-
1972
- 1972-03-01 US US00230839A patent/US3750397A/en not_active Expired - Lifetime
-
1973
- 1973-02-20 CA CA164,893A patent/CA963675A/en not_active Expired
- 1973-02-27 IT IT20890/73A patent/IT979502B/it active
- 1973-02-27 FR FR7306829A patent/FR2174069B3/fr not_active Expired
- 1973-02-27 DE DE19732309715 patent/DE2309715A1/de active Pending
- 1973-03-01 JP JP48023799A patent/JPS48100515A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| JPS48100515A (enExample) | 1973-12-19 |
| CA963675A (en) | 1975-03-04 |
| FR2174069A1 (enExample) | 1973-10-12 |
| IT979502B (it) | 1974-09-30 |
| US3750397A (en) | 1973-08-07 |
| BE795867A (fr) | 1973-06-18 |
| FR2174069B3 (enExample) | 1976-03-05 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| OHJ | Non-payment of the annual fee |