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Simulated power transfer control device and power transfer control method realized by adopting same

An electrical control and analog transfer technology, applied in circuit devices, electrical components, emergency power supply arrangements, etc., can solve problems such as the lack of power transfer function battery power supply paths in the aircraft control system

Inactive Publication Date: 2015-02-04
BEIJING INST OF ELECTRONICS SYST ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention is to solve the lack of power transfer function in the existing aircraft control system and the verification of the battery power supply path of the electrical system

Method used

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  • Simulated power transfer control device and power transfer control method realized by adopting same

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specific Embodiment approach 1

[0015] Specific implementation mode one: refer to figure 1 Describe this embodiment in detail, a kind of analog transfer control device described in this embodiment, it also includes transfer control combination 1, computer 2, launch equipment 3 and power supply 4,

[0016] The bomb-on device 3 is installed on the aircraft,

[0017] The ejection device 3, the power transfer control combination 1, the computer 2 and the power supply 4 are connected by cables,

[0018] Power transfer control combination 1 includes a control switch and an indicator light,

[0019] The power signal output end of the power supply 4 is connected to the power signal input end of the control switch, the control switch is connected to the indicator light display signal input end, the control signal input / output end of the control switch is connected to the output / input end of the computer 2 control signal, and the control switch The power signal output end is connected to the power signal input end o...

specific Embodiment approach 2

[0023] Specific embodiment 2: According to the power transfer control method realized by an analog power transfer control device described in specific embodiment 1, in this embodiment, the computer 2 controls the control switch to connect the power supply 4, and the power supply 4 is a control switch Power supply, the control switch is energized to make the indicator light display brightness, the control switch controls the launch device 3 on the aircraft to be connected, and at the same time, the computer 2 detects the voltage of the launch device 3 .

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Abstract

The invention discloses a simulated power transfer control device and a power transfer control method realized by adopting the device, relating to the field of power transfer control of aircrafts, and aiming at solving the problems of lack of a power transfer function in existing aircraft launching control systems and incapability of checking power supply access of a battery of an electric system. Airborne equipment disclosed by the invention is mounted on an aircraft; the airborne equipment, a power transfer control combination, a computer and a power supply source are connected with one another by cables; the power transfer control combination comprises a control switch and an indictor light. The power source signal output end of the power supply source is connected with the power source signal input end of the control switch, and the control switch is connected with the display signal input end of the indicator light. A control signal of the control switch is connected with the control signal of the computer, the power source signal output end of the control switch is connected with the power source signal input end of the airborne equipment, the detection signal output end of the airborne equipment is connected with the detection signal input end of the computer, and aircraft superposed power supply and simulated power transfer control are realized through computer control. The device and the method can be used for ground test control of the aircrafts.

Description

technical field [0001] The invention relates to a method for realizing an analog power transfer control device. In particular, the invention relates to a method for realizing the analog power transfer control device of the aircraft by the launch control system of the aircraft. It belongs to the field of aircraft power transfer control. Background technique [0002] At present, with the rapid development of weapons and equipment, the test coverage of aircraft is required to cover the entire process of aircraft operation. [0003] After the aircraft is unplugged and disconnected, the power supply should be changed from the ground power supply to the battery power supply. In the traditional test process, the power transfer function of the launch control system and the battery power supply path of the electrical system cannot be verified. Contents of the invention [0004] The invention aims to solve the lack of power transfer function in the existing aircraft launch control...

Claims

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Application Information

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IPC IPC(8): H02J9/04
Inventor 王玉姣程鹏田福强
Owner BEIJING INST OF ELECTRONICS SYST ENG
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