Non-intermittent detonation rotor of engine
A non-intermittent, engine technology, applied in the direction of machines/engines, mechanical equipment, gas turbine devices, etc., to achieve the effect of improving smoothness, strengthening the frequency of power, and reducing costs
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Embodiment 1
[0052] Embodiment one: the preferred embodiment of the present invention is described in detail as follows in conjunction with accompanying drawing: see figure 1 and figure 2 , the non-intermittent detonation rotor of the engine is a wheel disk rotating around the axis, including a wheel body 1 and front and rear bottom plates 9, 10 fitted with the front and rear sides of the wheel body. The disc body 1 and the front and rear bottom plates 9, 10 have central holes to form a premixed fuel inlet 8; There is a one-way valve 6 at the interface between the two; the combustion ring 5 is provided with a number of diffraction barriers 3, which divide the combustion ring 5 into several cut areas; the combustion ring 5 is equipped with an ignition Device 4; there is an outlet combustion pipe 7 between the combustion ring pipe 5 and the outer edge of the wheel body 1 . The ignition device or ignition method 4 ignites the premixed fuel in the combustion ring 5, and the combustion flame...
Embodiment 2
[0053] Embodiment two: see figure 1 , figure 2 and image 3 , the present embodiment is the same as the first embodiment, and the special feature is that the shapes of the front and rear base plates 9 and 10 are changed, and the shoulders of the base plates 9 and 10 are installed on the base 11 through bearings or bushings as rotation shafts. This structure can be directly used as a form of realization of the engine.
Embodiment 3
[0054] Embodiment three: see figure 1 , figure 2 and Figure 4 , the present embodiment is the same as the first embodiment, and the special feature is that the shape of the outlet combustion duct 7 is changed to a slightly backward-inclined design of the combustion air flow, and the bottom plate 10 is replaced by a turbine structure 12 . The high-speed airflow ejected from the outlet combustion pipe 7 passes through the turbine structure 12 to generate power, thereby enhancing the movement of the rotor. So this structure can be used as a form of realization of the engine rotor.
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