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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

Inactive Publication Date: 2019-12-10
QINGDAO DUQIU NEW ENERGY TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Aiming at the defects in the prior art, the present invention provides an orbital acceleration center power acceleration system applied to aircraft launch to solve the problem that the traditional technology is limited by the fact that the power source cannot release a large amount of energy in a short time, so that the vehicle forms a Smooth acceleration curve consumes a lot of fuel and energy to maintain power consumption in the acceleration phase

Method used

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  • Power acceleration system applied to aircraft launching for orbital acceleration center
  • Power acceleration system applied to aircraft launching for orbital acceleration center

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Embodiment Construction

[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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Abstract

The invention discloses a power acceleration system applied to aircraft launching for an orbital acceleration center, and relates to the technical field of power propulsion systems. The system comprises an energy storage device with constant output power, wherein the energy storage device is in power connection with a bearing acceleration device through a connecting component. The system solves the problems that a traditional technology is limited by a power source and cannot release a large energy in a short time, so that a smooth acceleration curve is formed by a vehicle, and a large amountof fuel and energy are consumed to maintain the power consumption of the acceleration stage.

Description

technical field [0001] The invention relates to the technical field of power propulsion systems, in particular to a power acceleration system for an orbital acceleration center used in launching an aircraft. Background technique [0002] The vehicles in the market consume a huge amount of energy during the acceleration from stationary to normal driving speed. Taking aircraft as an example, the aircraft needs to use fuel to provide continuous flight power during flight. Among them, For manned aviation aircraft, the fuel carrying capacity of small aircraft is mostly at 20 tons. When the aircraft accelerates from the ground to take-off, the fuel consumption is the largest during this period, accounting for 1 / 4 of the fuel carrying capacity, making energy consumption It is huge. After analysis by researchers, it is found that the main reason is that when the engine is driving the forward device, it cannot release a huge amount of energy in a short time to propel the aircraft for...

Claims

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Application Information

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IPC IPC(8): B64F1/04
CPCB64F1/04Y02T50/80
Inventor 成立张艳
Owner QINGDAO DUQIU NEW ENERGY TECH CO LTD