AT64313B - Explosion turbine with a cylindrical rotor rotating between two fixed cylindrical bodies. - Google Patents
Explosion turbine with a cylindrical rotor rotating between two fixed cylindrical bodies.Info
- Publication number
- AT64313B AT64313B AT64313DA AT64313B AT 64313 B AT64313 B AT 64313B AT 64313D A AT64313D A AT 64313DA AT 64313 B AT64313 B AT 64313B
- Authority
- AT
- Austria
- Prior art keywords
- explosion
- chambers
- cylindrical
- rotor rotating
- fixed
- Prior art date
Links
- 238000004880 explosion Methods 0.000 title claims description 9
- 239000000203 mixture Substances 0.000 claims description 5
- 239000002360 explosive Substances 0.000 description 3
- 239000007789 gas Substances 0.000 description 2
- 108091006146 Channels Proteins 0.000 description 1
- 230000004941 influx Effects 0.000 description 1
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Description
<Desc/Clms Page number 1>
EMI1.1
EMI1.2
EMI1.3
<Desc/Clms Page number 2>
EMI2.1
<Desc/Clms Page number 3>
dieser Drehbewegung statt, auch geht die Drehung des Läufers auf Grund des vorangegangenen Druckes des komprimierten Explosionsgemisches noch so weit, dass die Kammern 8 mit den hochgespannten Explosionsgusen die Kammern 10 erreichen.
In diesem Augenblick findet ein plötzliches Auspuffen des hochgespannten Explosionagases aus sämtlichen Kammern 8 in die sämtlichen Kammern 10 statt, wobei durch den heftigen Rückdruck eine Weiterdrehung des Läufers in der Pfeilrichtung hervorgerufen wird, bis die Kammern 8 die in der Reihenfolge nächsten Kanunern 9 des inneren Zylinders gerade zu erreichen beginnen, wobei ein neuer Zustrom von komprimierten Explosionsgemisch und ein entsprechender Druck auf die vorangehenden
EMI3.1
im Gange, dann könnte wohl auch durch den Rückdruck des explodierten Gemisches bzw.
durch die Explosionsgase eine ausreichende Teildrehung des Läufers unter Mitwirkung der Schwungkraft desselben oder eines angeordneten Schwungrades erzielt werden, doch ist es zweckmässiger, wenn die im Augenblick der Explosionen wegen der Geschlossenheit der Exptosionskammern durchaus notwendige kurze Teildrehung durch ein direkt wirkendes Druckmittel, hier also durch den vorangegangenen Druck des direkt auf die vorderen Flächen der Kammern 8 wirkenden komprimierten Explosionsgemisches, gesichert wird, wie es Zweck der Erfindung ist.
<Desc / Clms Page number 1>
EMI1.1
EMI1.2
EMI1.3
<Desc / Clms Page number 2>
EMI2.1
<Desc / Clms Page number 3>
This rotary movement takes place, and due to the previous pressure of the compressed explosion mixture, the rotation of the rotor goes so far that the chambers 8 with the highly tensioned explosion guses reach the chambers 10.
At this moment there is a sudden exhaustion of the high-tension explosive gas from all chambers 8 into all chambers 10, with the violent back pressure causing the rotor to continue to rotate in the direction of the arrow until the chambers 8 are the next in sequence channels 9 of the inner cylinder just begin to achieve, with a new influx of compressed explosive mixture and a corresponding pressure on the previous one
EMI3.1
in progress, then the back pressure of the exploded mixture or
A sufficient partial rotation of the rotor can be achieved by the explosion gases with the help of the centrifugal force of the same or an arranged flywheel, but it is more expedient if the brief partial rotation, which is absolutely necessary at the moment of the explosions due to the closed nature of the explosion chambers, is achieved by a directly acting pressure medium, in this case by the previous pressure of the compressed explosive mixture acting directly on the front surfaces of the chambers 8, is secured, as is the purpose of the invention.
Claims (1)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR64313X | 1910-11-10 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| AT64313B true AT64313B (en) | 1914-04-10 |
Family
ID=8697404
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT64313D AT64313B (en) | 1910-11-10 | 1911-10-11 | Explosion turbine with a cylindrical rotor rotating between two fixed cylindrical bodies. |
Country Status (1)
| Country | Link |
|---|---|
| AT (1) | AT64313B (en) |
-
1911
- 1911-10-11 AT AT64313D patent/AT64313B/en active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| AT64313B (en) | Explosion turbine with a cylindrical rotor rotating between two fixed cylindrical bodies. | |
| US1676211A (en) | Transmission for rotary engines | |
| US1931545A (en) | Combustion turbine | |
| US2198130A (en) | Internal combustion engine | |
| US1294771A (en) | Internal-combustion rotary engine. | |
| US1463646A (en) | Apparatus for performing cycles of compression, expansion, combustion, suction, exhaust, and the like | |
| US1615619A (en) | Two-way water turbine | |
| US1116781A (en) | Internal-combustion engine. | |
| US1045732A (en) | Turbo-displacement engine. | |
| US2372480A (en) | Rotary pump | |
| AT42218B (en) | Gas turbine that is operated with exhaust gases from explosion engines. | |
| US915236A (en) | Rotary engine. | |
| US1256995A (en) | Rotary engine. | |
| US3594104A (en) | Multiple stage rotary engine | |
| DE1106028B (en) | Device for low-loss compression of gases | |
| AT81745B (en) | Gas pressure charger. | |
| AT43523B (en) | Explosive engine with radially arranged cylinders rotating around a fixed shaft. | |
| US886279A (en) | Rotating internal-combustion engine. | |
| AT26904B (en) | Power machine with rotating pistons. | |
| US890208A (en) | Rotary gas-engine. | |
| US1336997A (en) | Rotary engine | |
| AT27386B (en) | Power machine with a rotating piston. | |
| US1401478A (en) | Rotary internal-combustion engine | |
| US974634A (en) | Rotary turbine-engine. | |
| AT85773B (en) | Internal combustion engine with a rotating housing provided with piston vanes. |