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
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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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