DE3114820C2 - - Google Patents
Info
- Publication number
- DE3114820C2 DE3114820C2 DE19813114820 DE3114820A DE3114820C2 DE 3114820 C2 DE3114820 C2 DE 3114820C2 DE 19813114820 DE19813114820 DE 19813114820 DE 3114820 A DE3114820 A DE 3114820A DE 3114820 C2 DE3114820 C2 DE 3114820C2
- Authority
- DE
- Germany
- Prior art keywords
- pressure
- medium
- stage
- low
- gas 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 - Fee Related
Links
- 239000007789 gas Substances 0.000 description 30
- 239000000446 fuel Substances 0.000 description 9
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000005457 optimization Methods 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 239000002918 waste heat Substances 0.000 description 1
Classifications
-
- 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
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/068—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type being characterised by a short axial length relative to the diameter
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19813114820 DE3114820A1 (de) | 1981-04-11 | 1981-04-11 | "gas-turbo-motor" |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19813114820 DE3114820A1 (de) | 1981-04-11 | 1981-04-11 | "gas-turbo-motor" |
Publications (2)
Publication Number | Publication Date |
---|---|
DE3114820A1 DE3114820A1 (de) | 1982-11-04 |
DE3114820C2 true DE3114820C2 (enrdf_load_stackoverflow) | 1993-02-04 |
Family
ID=6130012
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19813114820 Granted DE3114820A1 (de) | 1981-04-11 | 1981-04-11 | "gas-turbo-motor" |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE3114820A1 (enrdf_load_stackoverflow) |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2625012A (en) * | 1950-04-18 | 1953-01-13 | Gen Engineering And Res Corp | Gas turbine power plant, including multiple fluid operated turbines |
GB1077955A (en) * | 1963-05-16 | 1967-08-02 | Bristol Siddeley Engines Ltd | Gas turbine jet propulsion units for aircraft |
GB1487324A (en) * | 1973-11-15 | 1977-09-28 | Rolls Royce | Gas turbine engines |
-
1981
- 1981-04-11 DE DE19813114820 patent/DE3114820A1/de active Granted
Also Published As
Publication number | Publication date |
---|---|
DE3114820A1 (de) | 1982-11-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8110 | Request for examination paragraph 44 | ||
D2 | Grant after examination | ||
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |