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Multi-channel onboard microsecond pulse plasma flowing control power supply

A microsecond pulse and plasma technology, applied in electric pulse generator circuits, active components to generate pulses, electrical components, etc., can solve problems such as bulky, difficult to use on-board, and inability to remotely control, to ensure safe discharge. Effect

Inactive Publication Date: 2018-11-30
AIR FORCE UNIV PLA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the traditional high-voltage pulse power supply is bulky and heavy, and cannot be controlled remotely, and most of them use 220V mains power supply, which is only suitable for laboratory operation and difficult for airborne use.
In addition, a single high-voltage pulse power supply often only has one output, and two power supplies need to be installed in the roll control to drive the exciters on both sides of the wing to work independently, occupying a larger cabin volume and load capacity

Method used

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  • Multi-channel onboard microsecond pulse plasma flowing control power supply
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  • Multi-channel onboard microsecond pulse plasma flowing control power supply

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Embodiment Construction

[0039] Below in conjunction with accompanying drawing, the present invention is described in further detail:

[0040] The multi-channel airborne microsecond pulse plasma flow control power supply of the present invention includes a high-voltage module and a control module.

[0041]The high-voltage module is composed of the first on-board battery DC inverter module, voltage doubler charging module, channel selection module and pulse forming module, wherein the DC inverter module includes the inverter control relay SSR 0 And a 24V DC to hundreds of volts (V) AC inverter, such as figure 1 shown. The output end of the first onboard battery is connected to the input end of the DC inverter module. The DC voltage of 24 volts (V) output by the first onboard battery is boosted in the DC inverter module and converted from DC to AC to output an AC voltage of several hundred volts (V). The output terminal of the DC inverter module is connected to the input terminal of the voltage doubl...

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Abstract

The invention discloses a multi-channel onboard microsecond pulse plasma flowing control power supply. The multi-channel onboard microsecond pulse plasma flowing control power supply comprises a high-voltage module and a control module, wherein the high-voltage module comprises a first onboard battery DC inversion module, a voltage multiplication charging module, a channel selection module and a pulse formation module, and the control module comprises a remote controller, a receiving antenna, a receiver, a first fiber isolation plate until an N(th) fiber isolation plate, a first signal outputend until an N(th) signal output end and a second onboard battery. The power supply is provided with a plurality of output channels and can independently work, the various functions such as unmanned aerial vehicle plasma flowing control suppression separation, delayed speed reduction and rolling moment control can be achieved by combined application of multiple channels. The power supply also hasthe characteristics of small size and light weight, and remote control can be performed by the remote controller.

Description

technical field [0001] The invention relates to plasma flow control technology, in particular to a multi-channel airborne microsecond pulse plasma flow control power supply. Background technique [0002] Plasma flow control technology is a new type of active flow control technology, which has become an important research hotspot in the field of aerodynamics and aerothermodynamics in the world in recent years. A high-voltage pulse is applied between the two electrodes of the plasma actuator to ionize the air to form plasma. Plasma flow control can significantly suppress boundary layer separation and increase wing lift. Simultaneously applying plasma excitation on both sides of the aircraft wing can maximize the lift of the aircraft and delay the stall, while applying excitation to one side of the wing alone can increase the lift on one side of the wing while keeping the lift on the other side unchanged, thus Generate a large rolling moment to control the attitude of the air...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02M9/02H03K3/021
CPCH02M11/00H03K3/021
Inventor 梁华苏志宋慧敏贾敏吴云金迪魏彪谢理科
Owner AIR FORCE UNIV PLA
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