Unmanned helicopter starting and power supply integrated power supply control system and method

An unmanned helicopter and power control technology, which is applied to motor vehicles, unmanned aerial vehicles, aircraft parts, etc., can solve problems such as poor stability and reliability, and achieve the effects of easy implementation, high system reliability, and good application prospects.

Active Publication Date: 2021-01-08
NANJING INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In view of the above deficiencies, the object of the present invention is to provide an unmanned helicopter start-up power supply integrated power control system and method to solve the problem of poor stability and reliability of the power control system existing in the prior art

Method used

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  • Unmanned helicopter starting and power supply integrated power supply control system and method
  • Unmanned helicopter starting and power supply integrated power supply control system and method
  • Unmanned helicopter starting and power supply integrated power supply control system and method

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Embodiment Construction

[0030] The present invention will be further described below in conjunction with the accompanying drawings. The following examples are only used to illustrate the technical solution of the present invention more clearly, but not to limit the protection scope of the present invention.

[0031] Such as figure 1 As shown, a system block diagram of an integrated power supply control system for unmanned helicopter startup and power supply. The system uses a brushless DC generator, a full-bridge LLC resonant conversion circuit, a 12V battery pack, and a DC / DC bidirectional buck-boost circuit to start the motor. , Digital signal processing chip, detection and conditioning circuit, driving circuit.

[0032] The brushless DC generator is connected to the turbine engine of the unmanned helicopter through a conveyor belt, the brushless DC generator is connected to one end of the full-bridge LLC resonant conversion circuit, and the other end of the full-bridge LLC resonant conversion cir...

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Abstract

The invention discloses an unmanned helicopter starting and power supply integrated power supply control system and method. The system comprises a brushless direct-current generator, a full-bridge LLCresonant conversion circuit, a storage battery pack, a DC / DC bidirectional buck-boost circuit, a starting motor and a detection and conditioning circuit. One end of the full-bridge LLC resonant conversion circuit is connected with the generator, and the other end of the full-bridge LLC resonant conversion circuit is connected with a direct-current bus; the brushless direct current generator is connected with a turbine engine of an unmanned helicopter; one end of the DC / DC bidirectional buck-boost circuit is connected with the storage battery pack, and the other end of the DC / DC bidirectionalbuck-boost circuit is connected with the direct-current bus; a starting motor is electrically connected between the DC / DC bidirectional buck-boost circuit and the storage battery pack; the full-bridgeLLC resonant conversion circuit, the DC / DC bidirectional buck-boost circuit and the storage battery pack are connected with the input end of the detection and conditioning circuit; and the starting motor is connected with the turbine engine through a gear. According to the invention, the power supply range of the generator is improved, the complete fault diagnosis and protection functions are realized, and the system has high reliability.

Description

technical field [0001] The invention relates to an integrated power supply control system and method for unmanned helicopter startup and power supply, and belongs to the technical field of unmanned helicopter power supply control. Background technique [0002] Unmanned helicopter has unique flight performance and use value. It has the characteristics of no casualties, small size, low cost, strong battlefield survivability, flexible flight, strong survivability, and strong airport adaptability. Helicopters are widely used in both military and civilian applications. On the military side, unmanned helicopters can perform various non-lethal tasks as well as soft and hard lethal tasks; on the civilian side, unmanned helicopters are used in atmospheric monitoring, traffic monitoring, resource exploration, power line detection, forest fire prevention etc. The unmanned helicopter generally supplies power to the starter motor through the battery to drive the turbine engine of the u...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D41/00
CPCB64D41/00B64U50/12B64U10/10
Inventor 黄卫忠赵涛张成朱爱华
Owner NANJING INST OF TECH
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