DE3614311A1 - Antriebsanlage fuer luftfahrzeuge - Google Patents
Antriebsanlage fuer luftfahrzeugeInfo
- Publication number
- DE3614311A1 DE3614311A1 DE19863614311 DE3614311A DE3614311A1 DE 3614311 A1 DE3614311 A1 DE 3614311A1 DE 19863614311 DE19863614311 DE 19863614311 DE 3614311 A DE3614311 A DE 3614311A DE 3614311 A1 DE3614311 A1 DE 3614311A1
- Authority
- DE
- Germany
- Prior art keywords
- flow
- circuit
- thrust
- drive system
- air inlet
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 claims abstract description 8
- 230000008569 process Effects 0.000 claims abstract description 8
- 238000002485 combustion reaction Methods 0.000 claims abstract description 6
- 238000006073 displacement reaction Methods 0.000 claims abstract description 4
- 238000011144 upstream manufacturing Methods 0.000 claims description 2
- 239000003570 air Substances 0.000 description 37
- 239000007789 gas Substances 0.000 description 20
- 230000008901 benefit Effects 0.000 description 5
- 239000013598 vector Substances 0.000 description 5
- 238000013459 approach Methods 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000000717 retained effect Effects 0.000 description 2
- 238000009966 trimming Methods 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 239000012080 ambient air Substances 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000009931 harmful effect Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 210000004072 lung Anatomy 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 238000009423 ventilation Methods 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
- F02K3/077—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 the plant being of the multiple flow type, i.e. having three or more flows
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
-
- 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
- F02K3/075—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 controlling flow ratio between flows
-
- 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
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/105—Heating the by-pass flow
- F02K3/11—Heating the by-pass flow by means of burners or combustion chambers
-
- 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
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)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19863614311 DE3614311A1 (de) | 1986-04-28 | 1986-04-28 | Antriebsanlage fuer luftfahrzeuge |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19863614311 DE3614311A1 (de) | 1986-04-28 | 1986-04-28 | Antriebsanlage fuer luftfahrzeuge |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE3614311A1 true DE3614311A1 (de) | 1987-10-29 |
| DE3614311C2 DE3614311C2 (enExample) | 1989-11-02 |
Family
ID=6299686
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19863614311 Granted DE3614311A1 (de) | 1986-04-28 | 1986-04-28 | Antriebsanlage fuer luftfahrzeuge |
Country Status (1)
| Country | Link |
|---|---|
| DE (1) | DE3614311A1 (enExample) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4012103C1 (en) * | 1990-04-14 | 1991-07-25 | Karl Dipl.-Ing. 2742 Gnarrenburg De Kastens | Hypersonic aircraft reaction drive - has flow tube with frontal air entry slot and trough at trailing end |
| DE4117933A1 (de) * | 1990-04-14 | 1991-11-21 | Kastens Karl | Turbotriebwerk fuer hyperschallfluggeraete |
| DE4121995A1 (de) * | 1991-07-03 | 1992-01-09 | Kastens Karl | Tangentialgeblaese fuer turbotriebwerke |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2651175A (en) * | 1946-09-11 | 1953-09-08 | Rolls Royce | Controlling combustion system of gas-turbine engines |
| DE1301650B (de) * | 1965-01-30 | 1969-08-21 | Rolls Royce | Mantelstromgasturbinenstrahltriebwerk |
| DE2917303A1 (de) * | 1979-04-28 | 1980-10-30 | Dornier Gmbh | Antriebsanlage fuer luftfahrzeuge |
-
1986
- 1986-04-28 DE DE19863614311 patent/DE3614311A1/de active Granted
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2651175A (en) * | 1946-09-11 | 1953-09-08 | Rolls Royce | Controlling combustion system of gas-turbine engines |
| DE1301650B (de) * | 1965-01-30 | 1969-08-21 | Rolls Royce | Mantelstromgasturbinenstrahltriebwerk |
| DE2917303A1 (de) * | 1979-04-28 | 1980-10-30 | Dornier Gmbh | Antriebsanlage fuer luftfahrzeuge |
Non-Patent Citations (1)
| Title |
|---|
| DE-Z.: Luft- und Raumfahrt 3/85, S. 65 u. 66 * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4012103C1 (en) * | 1990-04-14 | 1991-07-25 | Karl Dipl.-Ing. 2742 Gnarrenburg De Kastens | Hypersonic aircraft reaction drive - has flow tube with frontal air entry slot and trough at trailing end |
| DE4117933A1 (de) * | 1990-04-14 | 1991-11-21 | Kastens Karl | Turbotriebwerk fuer hyperschallfluggeraete |
| DE4121995A1 (de) * | 1991-07-03 | 1992-01-09 | Kastens Karl | Tangentialgeblaese fuer turbotriebwerke |
Also Published As
| Publication number | Publication date |
|---|---|
| DE3614311C2 (enExample) | 1989-11-02 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| OP8 | Request for examination as to paragraph 44 patent law | ||
| D2 | Grant after examination | ||
| 8364 | No opposition during term of opposition | ||
| 8339 | Ceased/non-payment of the annual fee |