Heating control method, device, equipment and medium for helicopter windshield

A windshield and heating control technology, applied in the field of control, can solve the problems of large overshoot, windshield burst, windshield temperature easily exceeding the target constant temperature point, etc., to avoid overshoot of temperature rise and ensure the effect of normal work

Active Publication Date: 2021-06-11
北京神导科技股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Among them, the "switching method" has the advantages of fast heating and fast response, but when the ambient temperature is below zero or is about to reach the target constant temperature point, the windshield glass will easily burst when heated at full power, and the overshoot to reach the target constant temperature point is relatively small. The “duty ratio method” has the characteristics of small overshoot and high adjustment accuracy. However, the current “duty ratio method” uses fixed closed-loop control parameters, and the control conditions are affected by the current ambient temperature and heating time. Constraints such as constant temperature accuracy and other constraints will cause the windshield glass temperature to fail to reach the target constant temperature temperature point under strong convection conditions, and the windshield glass temperature will easily exceed the target constant temperature temperature point under weak convection conditions
And, when adopting above-mentioned two kinds of methods to control windshield heating, all can't realize the control of windshield temperature rising speed.

Method used

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  • Heating control method, device, equipment and medium for helicopter windshield
  • Heating control method, device, equipment and medium for helicopter windshield
  • Heating control method, device, equipment and medium for helicopter windshield

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0025] figure 1 It is a flowchart of a heating control method for a helicopter windshield provided by Embodiment 1 of the present invention. This embodiment is applicable to controlling the heating of the windshield when the "defogging" or "anti-icing" function of the helicopter windshield is turned on. The method can be executed by the heating control device for the windshield of the helicopter provided in the embodiment of the present invention. The device can be implemented in the form of software and / or hardware, and generally can be integrated in a processor.

[0026] Such as figure 1 As shown, the method of this embodiment specifically includes:

[0027] S110. Acquire the current temperature of the windshield when the acquisition time is reached.

[0028] A transparent resistance wire is laid in the inner layer of the windshield, and the heat generated by the resistance wire can adjust the temperature of the windshield after being energized. Wherein, the temperature o...

Embodiment 2

[0056] figure 2 It is a flow chart of a heating control method for a helicopter windshield provided by Embodiment 2 of the present invention. This embodiment is optimized on the basis of the foregoing embodiments. Wherein, after obtaining the current temperature of the windshield, at least one of the following may also be included:

[0057] If the current temperature is in the low temperature protection heating range, the heating power of the windshield is determined as the anti-overshoot heating power, wherein the anti-overshoot heating power is less than the maximum heating power;

[0058] If the current temperature is in the accelerated heating range, the heating power of the windshield is determined as the maximum heating power;

[0059] If the current temperature is in the high-temperature critical heating range, the heating power of the windshield is determined according to the heating power trend of the windshield;

[0060] If the current temperature is in the high t...

Embodiment 3

[0096] image 3 It is a flowchart of a heating control method for a helicopter windshield provided by Embodiment 3 of the present invention. On the basis of the foregoing embodiments, this embodiment provides a specific implementation manner.

[0097] Such as image 3 As shown, the method of this embodiment specifically includes:

[0098] S310. Acquire the current temperature T of the windshield when the collection time is reached n .

[0099] S320, judging T n Whether it is in the low temperature protection heating interval (-∞, 0), if yes, execute S330, if not, execute S340.

[0100] S330. Set the heating power of the windshield to half of the maximum heating power through a 50% duty cycle and perform a heating operation, and return to execute S320.

[0101] Among them, the cycle of the duty cycle matches the frequency of the AC power supply of the helicopter. For example, the frequency of the AC power supply of the helicopter is 400 Hz. In order to avoid the occurrenc...

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Abstract

The embodiment of the invention discloses a heating control method, device, equipment and medium for a windshield glass of a helicopter. The method includes: acquiring the current temperature of the windshield when the collection time is reached; determining the temperature difference that matches the temperature difference according to the temperature difference between the current temperature and the historical temperature of the windshield at the previous collection time. heating power; after controlling the heating device to heat the windshield according to the heating power, return to the operation of obtaining the current temperature of the windshield when the collection time is reached, so as to control the windshield according to a constant temperature rise Speed ​​heating to target heating temperature. The above technical solution improves the controllability of the windshield heating rate when the helicopter windshield glass defogging and anti-icing functions are turned on, ensures the normal operation of the windshield glass, and avoids the problem of overshooting of the windshield glass heating up.

Description

technical field [0001] The embodiments of the present invention relate to the technical field of control, and in particular, to a heating control method, device, equipment and medium for a helicopter windshield. Background technique [0002] The helicopter windshield is an important structural and functional part of the helicopter. It needs to maintain good optical performance under harsh conditions such as fogging and icing, and provide the driver with a clear view to ensure driving safety. Therefore, the helicopter windshield needs to have functions such as defogging and anti-icing. [0003] The defogging function and anti-icing function of the windshield are realized by heating the windshield. A transparent resistance wire is laid in the inner layer of the windshield. After the resistance wire is powered, heat can be generated, and then the temperature of the windshield can be adjusted. At the same time, a temperature sensor is laid in the inner layer of the bottom of th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/14B60S1/02
CPCB60S1/026B64C1/1492
Inventor 王志宇陈栋
Owner 北京神导科技股份有限公司
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