DE59907475D1 - FUEL INJECTION SYSTEM FOR A RADIAL OR SLINGER COMBUSTION CHAMBER OF A SMALL TURBINE - Google Patents
FUEL INJECTION SYSTEM FOR A RADIAL OR SLINGER COMBUSTION CHAMBER OF A SMALL TURBINEInfo
- Publication number
- DE59907475D1 DE59907475D1 DE59907475T DE59907475T DE59907475D1 DE 59907475 D1 DE59907475 D1 DE 59907475D1 DE 59907475 T DE59907475 T DE 59907475T DE 59907475 T DE59907475 T DE 59907475T DE 59907475 D1 DE59907475 D1 DE 59907475D1
- Authority
- DE
- Germany
- Prior art keywords
- radial
- combustion chamber
- fuel injection
- injection system
- small turbine
- 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 - Lifetime
Links
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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19846976A DE19846976A1 (en) | 1998-10-12 | 1998-10-12 | Fuel injection system for radial or slinger combustion chamber of small gas turbine with radial or diagonal compressor located in front of combustion chamber to which is connected turbine part via axially running rotor shaft |
PCT/EP1999/006838 WO2000022350A1 (en) | 1998-10-12 | 1999-09-15 | Fuel injection system for the radial or slinger combustion chamber in a small gas turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
DE59907475D1 true DE59907475D1 (en) | 2003-11-27 |
Family
ID=7884197
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19846976A Withdrawn DE19846976A1 (en) | 1998-10-12 | 1998-10-12 | Fuel injection system for radial or slinger combustion chamber of small gas turbine with radial or diagonal compressor located in front of combustion chamber to which is connected turbine part via axially running rotor shaft |
DE59907475T Expired - Lifetime DE59907475D1 (en) | 1998-10-12 | 1999-09-15 | FUEL INJECTION SYSTEM FOR A RADIAL OR SLINGER COMBUSTION CHAMBER OF A SMALL TURBINE |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19846976A Withdrawn DE19846976A1 (en) | 1998-10-12 | 1998-10-12 | Fuel injection system for radial or slinger combustion chamber of small gas turbine with radial or diagonal compressor located in front of combustion chamber to which is connected turbine part via axially running rotor shaft |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1121561B1 (en) |
DE (2) | DE19846976A1 (en) |
WO (1) | WO2000022350A1 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19852768A1 (en) | 1998-11-16 | 2000-05-18 | Bmw Rolls Royce Gmbh | Small gas turbine with a radial or Slinger combustion chamber |
DE202005006522U1 (en) * | 2005-04-23 | 2006-06-01 | Priebe, Klaus-Peter | Device for reducing of sealed gap losses has inter-engaging labyrinth seals for rotating component and casing, with gap width of labyrinth seal adjustable by movement of one half of seal |
US7762072B2 (en) | 2007-01-16 | 2010-07-27 | Honeywell International Inc. | Combustion systems with rotary fuel slingers |
US7942006B2 (en) | 2007-03-26 | 2011-05-17 | Honeywell International Inc. | Combustors and combustion systems for gas turbine engines |
ES2322317B1 (en) * | 2007-06-20 | 2010-03-31 | Futur Investment Partners, S.A. | AERONAUTICAL TURBOPROPULSOR. |
RU2487258C1 (en) * | 2012-03-01 | 2013-07-10 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" | Gas turbine engine gas generator |
GB201509458D0 (en) | 2015-06-01 | 2015-07-15 | Samad Power Ltd | Micro-CHP gas fired boiler with gas turbine assembly |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1011066A (en) * | 1948-11-30 | 1952-06-18 | Combustion chamber | |
DE1152850B (en) * | 1960-04-30 | 1963-08-14 | Bmw Triebwerkbau Ges M B H | Gas turbine, in particular small gas turbine |
US3018625A (en) * | 1960-06-27 | 1962-01-30 | Continental Aviat & Eng Corp | Internal combustion turbine engine |
US3983694A (en) * | 1974-10-29 | 1976-10-05 | Eaton Corporation | Cup-shaped fuel slinger |
US4232526A (en) * | 1978-12-26 | 1980-11-11 | Teledyne Industries, Inc. | High intensity slinger type combustor for turbine engines |
US4429527A (en) * | 1981-06-19 | 1984-02-07 | Teets J Michael | Turbine engine with combustor premix system |
EP0198077B1 (en) * | 1984-10-10 | 1992-01-15 | PAUL, Marius A. | Gas turbine engine |
US5042256A (en) * | 1986-07-28 | 1991-08-27 | Teledyne Industries, Inc. | Turbine shaft fuel pump |
US5022228A (en) * | 1988-12-22 | 1991-06-11 | Allied-Signal Inc. | Over the shaft fuel pumping system |
-
1998
- 1998-10-12 DE DE19846976A patent/DE19846976A1/en not_active Withdrawn
-
1999
- 1999-09-15 EP EP99946177A patent/EP1121561B1/en not_active Expired - Lifetime
- 1999-09-15 DE DE59907475T patent/DE59907475D1/en not_active Expired - Lifetime
- 1999-09-15 WO PCT/EP1999/006838 patent/WO2000022350A1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
EP1121561A1 (en) | 2001-08-08 |
EP1121561B1 (en) | 2003-10-22 |
DE19846976A1 (en) | 2000-04-13 |
WO2000022350A1 (en) | 2000-04-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |