DE3906580A1 - Leichtes turbinenstrahltriebwerk nach dem baukastenprinzip - Google Patents
Leichtes turbinenstrahltriebwerk nach dem baukastenprinzipInfo
- Publication number
- DE3906580A1 DE3906580A1 DE3906580A DE3906580A DE3906580A1 DE 3906580 A1 DE3906580 A1 DE 3906580A1 DE 3906580 A DE3906580 A DE 3906580A DE 3906580 A DE3906580 A DE 3906580A DE 3906580 A1 DE3906580 A1 DE 3906580A1
- Authority
- DE
- Germany
- Prior art keywords
- stage
- engine according
- turbine
- jet engine
- turbine jet
- 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.)
- Withdrawn
Links
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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/18—Lubricating arrangements
-
- 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
- F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
-
- 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
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
- F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/12—Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT67322/88A IT1219194B (it) | 1988-04-11 | 1988-04-11 | Turboreattore leggero modulare |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3906580A1 true DE3906580A1 (de) | 1989-10-19 |
Family
ID=11301439
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE3906580A Withdrawn DE3906580A1 (de) | 1988-04-11 | 1989-03-02 | Leichtes turbinenstrahltriebwerk nach dem baukastenprinzip |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE3906580A1 (it) |
FR (1) | FR2629872A1 (it) |
IL (1) | IL89449A0 (it) |
IT (1) | IT1219194B (it) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19852768A1 (de) * | 1998-11-16 | 2000-05-18 | Bmw Rolls Royce Gmbh | Kleingasturbine mit einer Radial- oder Slinger-Brennkammer |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE1025642B1 (fr) * | 2017-10-16 | 2019-05-15 | Safran Aero Boosters S.A. | Carter de compresseur avec reservoir d'huile pour turbomachine |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2880573A (en) * | 1952-08-27 | 1959-04-07 | Gen Motors Corp | Afterburner fuel injection system |
GB1039677A (en) * | 1963-07-10 | 1966-08-17 | Rolls Royce | Combustion chamber for a gas turbine engine |
GB1020145A (en) * | 1964-12-07 | 1966-02-16 | Rolls Royce | Power plant e.g. for jet propulsion of aircraft |
US3552873A (en) * | 1969-01-10 | 1971-01-05 | John N Ghougasian | Supersonic jet engine |
-
1988
- 1988-04-11 IT IT67322/88A patent/IT1219194B/it active
-
1989
- 1989-03-02 DE DE3906580A patent/DE3906580A1/de not_active Withdrawn
- 1989-03-02 IL IL89449A patent/IL89449A0/xx unknown
- 1989-04-07 FR FR8904626A patent/FR2629872A1/fr not_active Withdrawn
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19852768A1 (de) * | 1998-11-16 | 2000-05-18 | Bmw Rolls Royce Gmbh | Kleingasturbine mit einer Radial- oder Slinger-Brennkammer |
Also Published As
Publication number | Publication date |
---|---|
IT1219194B (it) | 1990-05-03 |
IL89449A0 (en) | 1989-09-10 |
IT8867322A0 (it) | 1988-04-11 |
FR2629872A1 (fr) | 1989-10-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8139 | Disposal/non-payment of the annual fee |