Method for calculating rotor forced excitation hot spot temperature of air-cooled non-salient pole synchronous phase modifier
A technology of hot spot temperature and calculation method, which is applied in calculation, computer-aided design, complex mathematical operations, etc., and can solve problems such as inability to accurately evaluate hot spot temperature
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[0048] In order to make the present invention more comprehensible, preferred embodiments are described in detail below with accompanying drawings.
[0049] Such as image 3 As shown in the present invention, a method for calculating the rotor forced excitation hot spot temperature of an air-cooled hidden pole synchronous condenser comprises the following steps:
[0050] Step 1: Obtain the parameters of the input calculation model and material property parameters: only 24 parameters need to be input, including the axial length L of the calculation model of the hottest point section p (Unit: m), the average half tooth width of the rotor b tf (Unit: m), rotor half copper wire width b cuf (unit: m), the height of copper wire per turn of the rotor h cuf (unit: m), rotor turn-to-turn insulation thickness h zar (unit: m), rotor slot insulation thickness h ir (unit: m), the heat dissipation coefficient aph in the rotor radial ventilation hole kr (Unit: W / m 2 / K),, rotor addendu...
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