| 摘要 |
Invention herewith described refers to the gunpowder engine and the aircraft powered by this engine. The gunpowder as the energy which can be always ahead of the loading is dosed in cartridges. The inserted cartridge is through the forestock (11), as on the hunting rifle, activated by pulling the trigger (12) via the trigger guard (14) of the spring (16) that releases the firing pin through the spring (13) passing through the chamber (15) and striking the cartridge (10) activates the gunpowder propellant.The thrust wave from rectilinear movement transforms into the circular direction (17), runs the arranged airscrews (1) as shown in Fig. 4, where we have two routes of the gunpowder wave (17) for the two groups of engines that are started in series from one to four and from one to twelve. They are started one after another and individually in order to obtain a sufficient period of time for cooling. The mark 24 on the aircraft shows the distribution of 12 main engines, mark (25) shows the distribution of the four engines (Figure 3), the mechanical dark part (20), the grid (21), the ring shaped part with two holders for fixing on the machine part, the mark (23) shows the torches used for heating the air, the sign (19) marks the infrared light.
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