Impulse type cycle engine
A pulsed, engine technology, applied in the field of aircraft drive, can solve the problems of inability to meet the long-distance drive capability, difficulty in large-scale preparation of antimatter fuel, and difficulty in storage.
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Embodiment 1
[0029] see figure 1 , the pulse type impulse cycle engine provided by the present invention is now described. The pulse-type impulse cycle engine includes an acceleration device 10 . The accelerating device 10 can accelerate the particle beam in its tube to a high sub-light velocity state. The high sub-light speed state of the particles refers to the state close to the speed of light, that is, the speed of the particles is greater than 90% of the speed of light and less than the speed of light. Accelerate the particle beam in a high-frequency group mode, and output multiple batches of accelerated particle beams in a periodic manner, so that the acceleration driving force is more uniform. Optionally, before the particle beam enters the accelerating device 10 , a linear accelerator can be set to accelerate and adjust the particle beam, so as to improve the quality of the incident particle beam entering the accelerating device 10 . Among them, when the particles in the particl...
Embodiment 2
[0036] read on figure 2 , as an impulse cycle engine provided in Embodiment 2 of the present invention, the impulse cycle engine may also include a deflection plate 3, the deflection plate 3 is used to receive the impact of the particle beam discharged from the first guide pipe 11 or the second guide pipe 21, The kinetic energy of the particle beam is transmitted to the deflection disk 3, and the angle of the deflection disk 3 is adjusted to control the direction of motion of the aircraft. The propulsion method of this kind of aircraft is referred to as indirect propulsion.
[0037] Further, see figure 1 and figure 2 , as a pulsed impulse cycle engine provided in Embodiment 2 of the present invention, the central axis of the first circular accelerator 101 coincides with the central axis of the second circular accelerator 102 . Specifically, the first circular accelerator 101 and the second circular accelerator 102 are arranged in parallel, and assuming that a certain plane...
Embodiment 3
[0039] see image 3 , as a pulse type impulse cycle engine provided in Embodiment 3 of the present invention, the difference from Embodiment 2 is that the first circular accelerator and the second circular accelerator are arranged on the same plane, which can also eliminate the Torque to avoid aircraft imbalance. Certainly, in other embodiments, the first circular accelerator and the second circular accelerator may also be symmetrically arranged on different planes, which is not limited here.
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