Integrated equipment control system for unmanned plane

An unmanned helicopter and equipment integration technology, applied in the field of unmanned aircraft, can solve the problems of poor system integration and complicated wiring, and achieve the effect of simple layout, comprehensive data collection and high integration.

Inactive Publication Date: 2017-05-31
GUANGXI UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, each existing sensor corresponds to its own control system, resulting in poor integration of the system and complicated wiring

Method used

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  • Integrated equipment control system for unmanned plane

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Embodiment Construction

[0010] Please refer to the attached figure 1 Shown, the present invention is the equipment comprehensive control system of unmanned helicopter, and it is mainly by control board 1, display 2, engine timer 3, engine temperature sensor 4, equipment current and voltage sensor 5, engine oil temperature sensor 6, engine exhaust The temperature sensor 7 and the oil quantity sensor 8 are composed of several parts.

[0011] Wherein, the display 2 and the engine timer 3 are integrated on the control board 1, so that the system has a high degree of integration and takes up little space.

[0012] The control board 1 is provided with a data interface 9 and a charging interface 10 . The data obtained by the sensor can be backed up through the data interface 9 . The charging interface 10 is used for charging the control system.

[0013] The engine temperature sensor 4 , equipment current and voltage sensor 5 , engine oil temperature sensor 6 , engine exhaust temperature sensor 7 and oil ...

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Abstract

The invention relates to an integrated equipment control system for an unmanned plane. The integrated equipment control system comprises a main control board, a display, an engine timer, an engine temperature sensor, an equipment current voltage sensor, an engine machine oil temperature sensor, an engine exhaust temperature sensor and a fuel content sensor, wherein the display and the engine timer are integrated on the main control board, the main control board is provided with a data interface and a charging interface, and the engine temperature sensor, the equipment current voltage sensor, the engine machine oil temperature sensor, the engine exhaust temperature sensor and the fuel content sensor are connected with the main control board. The integrated equipment control system has advantages of high integration level, complete data acquisition and concise layout.

Description

technical field [0001] The invention relates to a composition system of an unmanned aircraft, in particular to an equipment comprehensive control system of an unmanned helicopter, and belongs to the technical field of unmanned aircraft. Background technique [0002] In order to monitor the various systems and parts of the unmanned aircraft, it is usually necessary to install different sensors, and use the data obtained by the sensors to determine whether maintenance is required. [0003] However, each existing sensor corresponds to its own control system, resulting in poor system integration and complicated wiring. [0004] Therefore, in order to solve the above technical problems, it is indeed necessary to provide an integrated control system for unmanned aircraft with an improved structure, so as to overcome the defects in the prior art. Contents of the invention [0005] In order to solve the above problems, the object of the present invention is to provide an integrat...

Claims

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Application Information

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Patent Type & AuthorityApplications(China)
IPC IPC(8): G01D21/02
CPCG01D21/02G01M99/005
Inventor陈春峰
OwnerGUANGXI UNIV