DE1626070B1 - Gasgenerator nach Raketenbauart - Google Patents
Gasgenerator nach RaketenbauartInfo
- Publication number
- DE1626070B1 DE1626070B1 DE1967B0095483 DEB0095483A DE1626070B1 DE 1626070 B1 DE1626070 B1 DE 1626070B1 DE 1967B0095483 DE1967B0095483 DE 1967B0095483 DE B0095483 A DEB0095483 A DE B0095483A DE 1626070 B1 DE1626070 B1 DE 1626070B1
- Authority
- DE
- Germany
- Prior art keywords
- combustion chamber
- fuel
- gas generator
- oxygen carrier
- generator according
- 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
- 238000002485 combustion reaction Methods 0.000 claims description 83
- 239000000446 fuel Substances 0.000 claims description 54
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 25
- 239000001301 oxygen Substances 0.000 claims description 25
- 229910052760 oxygen Inorganic materials 0.000 claims description 25
- 239000007788 liquid Substances 0.000 claims description 14
- 239000007789 gas Substances 0.000 claims description 13
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 claims description 5
- 239000000463 material Substances 0.000 claims description 4
- 239000000919 ceramic Substances 0.000 claims description 2
- 238000001816 cooling Methods 0.000 description 9
- 238000006243 chemical reaction Methods 0.000 description 7
- 230000000694 effects Effects 0.000 description 6
- 238000002347 injection Methods 0.000 description 5
- 239000007924 injection Substances 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 230000002093 peripheral effect Effects 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- 238000001704 evaporation Methods 0.000 description 4
- 230000008020 evaporation Effects 0.000 description 4
- 239000000203 mixture Substances 0.000 description 3
- 239000003921 oil Substances 0.000 description 3
- 239000003380 propellant Substances 0.000 description 3
- 239000002826 coolant Substances 0.000 description 2
- 230000006378 damage Effects 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 235000015842 Hesperis Nutrition 0.000 description 1
- 235000012633 Iberis amara Nutrition 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 238000005119 centrifugation Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 239000000110 cooling liquid Substances 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 244000144992 flock Species 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000003779 heat-resistant material Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000000376 reactant Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 230000007704 transition Effects 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
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Nozzles (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE1626070 | 1967-11-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE1626070B1 true DE1626070B1 (de) | 1970-12-03 |
Family
ID=5682981
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE1967B0095483 Pending DE1626070B1 (de) | 1967-11-20 | 1967-11-20 | Gasgenerator nach Raketenbauart |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3568445A (enExample) |
| DE (1) | DE1626070B1 (enExample) |
| FR (1) | FR1592045A (enExample) |
| GB (1) | GB1230657A (enExample) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3937012A (en) * | 1970-11-28 | 1976-02-10 | Messerschmitt-Bolkow-Blohm Gmbh | Arrangement for the production of rotational energy in rocket combustion engines |
| DE2058583C3 (de) * | 1970-11-28 | 1975-02-20 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Einrichtung zum Einbringen von hypergolen Treibstoffen in die Brennkammer von Raketentriebwerken |
| JPS5348887Y2 (enExample) * | 1973-06-05 | 1978-11-22 | ||
| US3956885A (en) * | 1974-09-03 | 1976-05-18 | Avco Corporation | Electrothermal reactor |
| US5622046A (en) * | 1995-08-28 | 1997-04-22 | The United States Of America As Represented By The Secretary Of The Army | Multiple impinging stream vortex injector |
| WO2024052725A1 (en) * | 2022-09-09 | 2024-03-14 | Bordeu Schwarze Antonio | Liquid propellant gasifier and pressurizer |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2602290A (en) * | 1947-05-07 | 1952-07-08 | Daniel And Florence Guggenheim | Rotational fuel feed for combustion chambers |
| US2654997A (en) * | 1952-02-23 | 1953-10-13 | Esther C Goddard | Two-liquid combustion chamber for rocket apparatus |
| US3169368A (en) * | 1961-02-07 | 1965-02-16 | Bolkow Entwicklungen Kg | Combustion chamber for liquid fuels |
| FR1432989A (fr) * | 1964-04-22 | 1966-03-25 | Bolkow Gmbh | Chambre de combustion pour fusées à comburants liquides |
| GB1043020A (en) * | 1964-01-29 | 1966-09-21 | France Etat | Improvements in or relating to liquid injection devices, for jet propulsion or rocket type power units |
-
1967
- 1967-11-20 DE DE1967B0095483 patent/DE1626070B1/de active Pending
-
1968
- 1968-10-29 US US771565A patent/US3568445A/en not_active Expired - Lifetime
- 1968-11-18 GB GB1230657D patent/GB1230657A/en not_active Expired
- 1968-11-18 FR FR174233A patent/FR1592045A/fr not_active Expired
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2602290A (en) * | 1947-05-07 | 1952-07-08 | Daniel And Florence Guggenheim | Rotational fuel feed for combustion chambers |
| US2654997A (en) * | 1952-02-23 | 1953-10-13 | Esther C Goddard | Two-liquid combustion chamber for rocket apparatus |
| US3169368A (en) * | 1961-02-07 | 1965-02-16 | Bolkow Entwicklungen Kg | Combustion chamber for liquid fuels |
| GB1043020A (en) * | 1964-01-29 | 1966-09-21 | France Etat | Improvements in or relating to liquid injection devices, for jet propulsion or rocket type power units |
| FR1432989A (fr) * | 1964-04-22 | 1966-03-25 | Bolkow Gmbh | Chambre de combustion pour fusées à comburants liquides |
Also Published As
| Publication number | Publication date |
|---|---|
| GB1230657A (enExample) | 1971-05-05 |
| US3568445A (en) | 1971-03-09 |
| FR1592045A (enExample) | 1970-05-04 |
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