TH20675A - Compressor and rotary internal combustion engine - Google Patents

Abstract

Rotary internal combustion engine consisting of Three identical rotors And the main shaft that passes through the center of the three rotors The first rotor is used to compress the fuel / air mixture. And the second rotor is used for generating power And the third rotor will use the new compressed air.The rotation sequence of the three rotors is as follows The first rotor compresses the fuel / air mixture. Into the second rotor Which then ignites the fuel / air mixture to generate energy. The third rotor compresses the new air. And supply the compression to the second rotor to facilitate the combustion of the fuel / air mixture. Therefore, a second combustion device provides a better combustion. And the exhaust that is emitted is relatively clean.

Claims (4)

1.Rotary internal combustion engine It contains a new fuel / air mixture and air supply and includes a) a frame with a fuel / air mixture chamber. New energy and compressed air chambers Each room has a circular cross-section morphology. And coexistence, the first pass connects the fuel / air mixture compression chambers. And energy room And the second channel connects the new compressed air chamber. And power chamber; b) rotatable mounting shaft in the frame. And extends through all three chambers In order to coexist with the three chambers, c) the fins of the fuel / air mixture. Fixed on shaft to rotate with shaft in the fuel / air mixture chamber d) Energy flang fixed on shaft so that it rotates with shaft in energy chamber e) Compressed air fin fixed on shaft To rotate with the shaft in the new air compressor chamber; f) fuel / air compressor rotor Concentric To the shaft and connected to the flanges of the fuel / air mixture. In order to spin in that place In the fuel / air mixture compression chamber; g) centripetal energy rotor. And connected to the energy fins so that it rotates there in the energy chamber; h) the new compressed air rotor is centered on the shaft. And connect to new compressed air fins In order to spin it there in the new compressed air chamber. I) Cutter number one. From the fuel / air compressor rotor And pass through the first hole by the editor at one There will be at least one concave in such a way that the first cut is closed. And opens when the first edge is at least partially passed across the first compartment. In order for the fuel / air mixture to pass through the energy chamber j) method of ignition of the fuel / air mixture. In the power chamber and k) the second disconnector is connected from the new compressed air rotor. And passed through the second compartment The second trim will have at least one second concave. In such a way that the second vent is closed, the new compressed air enters the energy chamber, and the second edge, at least, sits in such a way that the fresh air is compressed. Through the energy chamber During combustion of the I-part of the fuel / air in the energy chamber 2.Rotary internal combustion engine As stated in Clause 1 where the energy room Is located between the fuel / air mixture compression chambers And new compressed air chambers 3.Rotary internal combustion engine As stated in claim 1, where the flanges are located at an angle from each other on the shaft 4.Rotary internal combustion engine As noted in claim 1, where each fin is connected to a common rotor. By a rocker-compatible pilot with a joint rotor