Double-flow injection rotor engine
A technology for engines and nozzles, applied in the field of injection dual-flow rotary engines, which can solve the problems of low power density and reduced efficiency of piston internal combustion engines, and achieve the effects of simple structure, high power density and high efficiency
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Embodiment 1
[0040] Such as figure 1 , Figure 11 with Figure 12 The jet dual-flow rotary engine shown includes a forward rotating structure 1, a reverse rotating structure 2 and a nozzle 3, on which the forward rotating structure 1 is provided with radially symmetrical blades 11, and in the reverse direction Axial blades 21 are arranged on the rotating structure 2, and the two counter-rotating structures 2 are coaxially arranged, and the forward-rotating structure 1 is arranged between the two counter-rotating structures 2, and the The axis of the forward-rotating structure 1 is collinear with the axis of the counter-rotating structure 2, the nozzle 3 communicates with the high-pressure working medium source 4, and the nozzle is set on the outside of the forward-rotating structure 1 A fixed structure 31, the nozzle 3 is arranged on the nozzle fixed structure 31, the gas working medium injected by the nozzle 3 is opposite to the radial surface arranged on the forward rotation structure...
Embodiment 2
[0042] Such as figure 2 with Figure 13 The jet dual-flow rotor engine shown differs from Embodiment 1 in that: the nozzle fixed structure 31 is set inside the forward rotating structure 1, and the nozzle 3 is arranged on the On the nozzle fixed structure 31, the gas working medium sprayed by the nozzle 3 is divided into two gas working fluid flows after the impact transmission of the radially symmetrical blades 11 arranged on the forward rotating structure 1 , wherein one stream of gaseous working medium impinges on the axial flow vane 21 on one of the counter-rotating structures 2 , wherein another stream of gaseous working medium impacts on the other one of the counter-rotating structures 2 The axial blades 21 are impact driven.
Embodiment 3
[0044] Such as image 3 with Figure 14 The jet dual-flow rotary engine shown includes a forward rotating structure 1, a reverse rotating structure 2 and a nozzle 3, on which the forward rotating structure 1 is provided with radially symmetrical blades 11, and in the reverse direction Axial blades 21 are arranged on the rotating structure 2, and the two counter-rotating structures 2 are coaxially arranged, and the forward-rotating structure 1 is arranged between the two counter-rotating structures 2, and the The axis of the forward rotating structure 1 is collinear with the axis of the reverse rotating structure 2, the nozzle 3 communicates with the high-pressure working medium source 4, and the forward rotating structure 1 and the reverse rotating The outer casing of the structure 2 is provided with a revolving structure 32 fixedly connected to the counter-rotating structure 2, the nozzle 3 is arranged on the revolving structure 32, and the gas working fluid injected by the ...
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