Power acceleration system applied to aircraft launching for orbital acceleration center
An acceleration system and aircraft technology, applied in the direction of launch/drag transmission, energy-saving operation measures, etc., can solve the problems of fuel consumption, energy and power consumption, and the power source cannot release large energy in a short time, so as to save energy consumption, Ease of large-scale manufacture and installation, low failure rate
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[0025] Embodiments of the technical solutions of the present invention will be described in detail below in conjunction with the accompanying drawings. The following examples are only used to illustrate the technical solutions of the present invention more clearly, and therefore are only examples, rather than limiting the protection scope of the present invention.
[0026] Such as figure 1 and figure 2 As shown, the orbital acceleration center power acceleration system used for aircraft launch includes an energy storage device with a constant output power, and the energy storage device is dynamically connected to the load-carrying acceleration device through connecting components.
[0027] The energy storage device includes a continuously variable transmission 1 , and the power output end of the continuously variable transmission 1 is connected to the connecting parts. Wherein the power drive of the continuously variable transmission 1 is driven by a motor.
[0028] The po...
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