DE2219981A1 - Anordnung und Einrichtung in einem Flugzeug für Heißdampfbetrieb - Google Patents
Anordnung und Einrichtung in einem Flugzeug für HeißdampfbetriebInfo
- Publication number
- DE2219981A1 DE2219981A1 DE19722219981 DE2219981A DE2219981A1 DE 2219981 A1 DE2219981 A1 DE 2219981A1 DE 19722219981 DE19722219981 DE 19722219981 DE 2219981 A DE2219981 A DE 2219981A DE 2219981 A1 DE2219981 A1 DE 2219981A1
- Authority
- DE
- Germany
- Prior art keywords
- aircraft according
- supply
- combustion chamber
- nozzle
- aircraft
- 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
- 238000009434 installation Methods 0.000 title description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 15
- 238000002485 combustion reaction Methods 0.000 claims description 14
- 229910052782 aluminium Inorganic materials 0.000 claims description 9
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 9
- 239000000446 fuel Substances 0.000 claims description 7
- 238000002844 melting Methods 0.000 claims description 6
- 239000007788 liquid Substances 0.000 claims description 5
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 4
- 230000008020 evaporation Effects 0.000 claims description 4
- 238000001704 evaporation Methods 0.000 claims description 4
- 229910052744 lithium Inorganic materials 0.000 claims description 4
- 229920002545 silicone oil Polymers 0.000 claims description 4
- 239000000843 powder Substances 0.000 claims description 3
- 229910052710 silicon Inorganic materials 0.000 claims description 3
- 239000010703 silicon Substances 0.000 claims description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 2
- 229910001080 W alloy Inorganic materials 0.000 claims description 2
- 238000001816 cooling Methods 0.000 claims 1
- 239000003779 heat-resistant material Substances 0.000 claims 1
- 239000011819 refractory material Substances 0.000 claims 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 4
- 239000001257 hydrogen Substances 0.000 description 4
- 229910052739 hydrogen Inorganic materials 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 239000004449 solid propellant Substances 0.000 description 4
- 150000004767 nitrides Chemical class 0.000 description 3
- 229910052715 tantalum Inorganic materials 0.000 description 3
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- 229910052721 tungsten Inorganic materials 0.000 description 3
- 239000010937 tungsten Substances 0.000 description 3
- 235000015842 Hesperis Nutrition 0.000 description 2
- 235000012633 Iberis amara Nutrition 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 239000012298 atmosphere Substances 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 150000001247 metal acetylides Chemical class 0.000 description 2
- 150000002736 metal compounds Chemical class 0.000 description 2
- 229910001092 metal group alloy Inorganic materials 0.000 description 2
- 229910052758 niobium Inorganic materials 0.000 description 2
- 239000010955 niobium Substances 0.000 description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000003870 refractory metal Substances 0.000 description 2
- 229910021332 silicide Inorganic materials 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910001362 Ta alloys Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 239000012943 hotmelt Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- CWQXQMHSOZUFJS-UHFFFAOYSA-N molybdenum disulfide Chemical compound S=[Mo]=S CWQXQMHSOZUFJS-UHFFFAOYSA-N 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000012299 nitrogen atmosphere Substances 0.000 description 1
- -1 or high-melting Substances 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- JTJMJGYZQZDUJJ-UHFFFAOYSA-N phencyclidine Chemical compound C1CCCCN1C1(C=2C=CC=CC=2)CCCCC1 JTJMJGYZQZDUJJ-UHFFFAOYSA-N 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 239000002760 rocket fuel Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 239000002966 varnish 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
- 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
- F02K9/44—Feeding propellants
- F02K9/52—Injectors
-
- 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
-
- 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
-
- 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
- F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
-
- 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
- F02K9/97—Rocket nozzles
- F02K9/974—Nozzle- linings; Ablative coatings
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT355071A AT313713B (de) | 1971-04-23 | 1971-04-23 | Flugzeug |
Publications (1)
Publication Number | Publication Date |
---|---|
DE2219981A1 true DE2219981A1 (de) | 1972-11-30 |
Family
ID=3552056
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19722219981 Pending DE2219981A1 (de) | 1971-04-23 | 1972-04-24 | Anordnung und Einrichtung in einem Flugzeug für Heißdampfbetrieb |
Country Status (3)
Country | Link |
---|---|
AT (1) | AT313713B (enrdf_load_stackoverflow) |
CH (1) | CH562399A5 (enrdf_load_stackoverflow) |
DE (1) | DE2219981A1 (enrdf_load_stackoverflow) |
-
1971
- 1971-04-23 AT AT355071A patent/AT313713B/de not_active IP Right Cessation
-
1972
- 1972-04-17 CH CH574972A patent/CH562399A5/xx not_active IP Right Cessation
- 1972-04-24 DE DE19722219981 patent/DE2219981A1/de active Pending
Also Published As
Publication number | Publication date |
---|---|
AT313713B (de) | 1974-02-25 |
CH562399A5 (enrdf_load_stackoverflow) | 1975-05-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE2842032A1 (de) | Verfahren und vorrichtung zum verbrennen kohlenstoffhaltiger brennstoffe | |
DE4028224A1 (de) | Waffe | |
DE2801367A1 (de) | Strahler-brenner fuer fluessige brennstoffe | |
DE202017006759U1 (de) | Vorrichtung und System zur Steuerung von Flugkörpern und Kill-Vehicles, die mit gelförmigen Treibstoffen betrieben wird | |
EP0737271B1 (de) | Diskusförmiger flugkörper für extrem hohe geschwindigkeiten | |
WO1987003355A1 (en) | Process for raising the temperature of catalysts and device for performing the process | |
DE2219981A1 (de) | Anordnung und Einrichtung in einem Flugzeug für Heißdampfbetrieb | |
DE1064760B (de) | Zuendeinrichtung fuer Brennkammern von Rueckstossantrieben | |
DE60216671T2 (de) | Anzünder für Treibladungen | |
DE2723517C3 (de) | Zündvorrichtung für einen Block brennbaren Pulvers | |
DE19924907B4 (de) | Feststofftriebwerk für eine Staustrahlrakete | |
EP0100840A2 (de) | Teilverbrennbarer Treibladungsanzünder | |
DE4130377A1 (de) | Brenner fuer dieselmotorenabgas-partikelfilter | |
DE194853C (enrdf_load_stackoverflow) | ||
DE102008029150A1 (de) | Gasgenerator | |
DE2623582C2 (de) | Raketengeschoß mit Ausklappleitwerk und Treibspiegel | |
DE113747C (enrdf_load_stackoverflow) | ||
EP0189545A1 (de) | Luftatmender Feststoff-Staustrahlantrieb | |
DE1626101C (de) | Treibstoffversorgungssystem fur ein Raketentriebwerk | |
DE941034C (de) | Zuendvorrichtung fuer Raketen- oder Duesenmotoren | |
CH454538A (de) | Abgasverbrenner | |
WO2022053496A1 (de) | Schubkammervorrichtung und verfahren zum betreiben einer schubkammervorrichtung | |
DE347854C (de) | Gasturbine mit pendelnder Fluessigkeit als Treibmittel | |
AT326492B (de) | Betriebssicheres kraftfahrzeug mit heissdampfantries | |
DE1751858C (de) | Kreiszylindrisches Mantelrohr fur ein Mantelstrahlheizrohr |