IL26652A - Internal combustion rotative engine - Google Patents
Internal combustion rotative engineInfo
- Publication number
- IL26652A IL26652A IL2665266A IL2665266A IL26652A IL 26652 A IL26652 A IL 26652A IL 2665266 A IL2665266 A IL 2665266A IL 2665266 A IL2665266 A IL 2665266A IL 26652 A IL26652 A IL 26652A
- Authority
- IL
- Israel
- Prior art keywords
- stator
- gaz
- blade
- engine according
- rotor
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims description 9
- 239000000203 mixture Substances 0.000 claims description 7
- 150000001875 compounds Chemical class 0.000 claims description 3
- 239000000446 fuel Substances 0.000 claims description 3
- 238000004880 explosion Methods 0.000 claims description 2
- UHOVQNZJYSORNB-UHFFFAOYSA-N Benzene Chemical compound C1=CC=CC=C1 UHOVQNZJYSORNB-UHFFFAOYSA-N 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 230000035515 penetration Effects 0.000 description 1
Landscapes
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
I n t e r n a l c o m b u s t i o n r o t a t i v e e n g i n a a n a a The invention relates to an internal combustion engine where the movement of acting parts is As the ternative movement of pistons in the existing internal combustion the constructiontlimitates the number of tions per minute and in the motors gives only one working tact per 2 rotations of the The present invention has basically the object of providing a tinuous rotative movement of the working device and enables the transmission of power directly to the rotor without alternative movement and to obtain one working tact per one rotation of the The cylinder which exists in the internal combustion engines is here replaced by a circular which the combustion chamber is enclosed between the motor blade fixed on the rotor and the second blade which remains fixed in the moment of After the motor blade moves together with the the circular At the end of each motor blade raises the second bladetwhich returns in the initial position after the motor blade has The second blade is moved back by means of an external spring acting its pivot or by Then the operation The compressed gaz mixture enters the through the inner tube placed in the and through adequate openings in the inner tube and the Inlet of gaz mixture can also be executed by means of cams and valves like in the existing In the latter case the inner tube is In the benzine or petrol the help of a spark In case of fuel compressed hot air can be introduced in the stator through the inner tube or The fuel is introduced in the by means of an This tact is the working In case of great power expansion working tact can be made in two or more In this case there are two or more acents their rotors fixed on the same The after explosion or completely expanded in the first in the next stator of corresponding through the exhaust opening of the first In the second tor the gaz will be completely the connecting tube ween two adjacents stators a valve is In the jacent stator neither plug nor is injector exhaust ning is as the compound steam the opening in the stators the moment when the motor blade reaches The hermetizing near the shaft labyrinth or Movement of working tact per one rotation of the double power in one stator in comparison with a linder of same uniformity of power transmission by means of half a number of comparison with existing linder easy exhaust without case compound more effective full simplicity of 1 The mentioned compressors and pumps are from existing They must only be adapted for that they are not cribed The invention will now be described with reference to the panying drawings in is a view in axial cross section of the tor and is a diagrammatic view in a longitudinal cross The device illustrated in the and is shown in the ment of inlet of compressed In and The motor blade is fixed on the The second blade is fixed on its pivot spark plug is provided for After ignition and the raise of pression in the chamber of between the two blade moves with the rotor in circular direc burned gaz expands until the moment when the blade reaches the haust opening After its further blade with its spring softly the blade the blade had blade is moved back by means of an nal spring acting on its pivot or by means of cams shown on the the operation The part of the stator permit the blade to pass over a predetermined The compressed means of auxiliary gaz mixture fills the inner tube and through the openings and ters in the After inlet and before the ning in the inner tube is closed by the rotor in the moment it passes openings are and the needed quantity of gaz mixture hot passes In the opening a non return light valve can be provided to prevent penetration of the exploded gaz in the tube prepared mixture or hot also be introduced in the of the inner by means of valves like it is used in benzine and Diesel insufficientOCRQuality
Claims (6)
1. An internal combustion rotative engine provided with circular stator and a hollow rotor which is provided with an inlet opening through which the compressed gaz enters into the combustion chamber,the stator being provided with an exhaust opening for the gaz after expansion.The chamber of combustion is. defined between two bladesioue of them fixed to the rotor and the second fixed to the stator,the first blade,at the end of each rotation,raising the second blade; he second blade being returned to its initial position by an external spring acting on its pivot,
2. An engine according to the claim 1.provided with cams actuating the second blade·
3. An engine according to the claim 1. provided with a supply of prepared and compressed gaz mixture or hot air through an inner tube in the rotor,
4. An engine according to the claim 1, provided with a supply of prepared gaz mixture, ot air and fuel by means of valves and cams*
5. An engine according to the claim 1, provided with groups of two or more adjacents stators where the expansion of burned gaz is effectuated in stages,in consecutive order in each stator.(Compound system)*
6. An engine according to the claims 1,,5· provided with one stator or group of stators wich are provided with two or more pairs of blades (two or more chambers of combustion) in each stator, placed symmetrically in relation to the centre and where are produced two or more explosions per one rotation of the rotor in the same stator. Dated the 05 October 1966.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IL2665266A IL26652A (en) | 1966-10-05 | 1966-10-05 | Internal combustion rotative engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IL2665266A IL26652A (en) | 1966-10-05 | 1966-10-05 | Internal combustion rotative engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IL26652A true IL26652A (en) | 1970-04-20 |
Family
ID=11044031
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IL2665266A IL26652A (en) | 1966-10-05 | 1966-10-05 | Internal combustion rotative engine |
Country Status (1)
| Country | Link |
|---|---|
| IL (1) | IL26652A (en) |
-
1966
- 1966-10-05 IL IL2665266A patent/IL26652A/en unknown
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