Still low airgap flux density-help please
Answers
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forget to add, to run the program, first click mesh domain and then run the test scenario.
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an attempt to move up the queue.
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Hi,
Currently I am analyzing your project. I will keep you informed.
Best regards.
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thank you, i will turn my notification on for this thread.
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Hi,
Sorry for the delay, time to analyze the Flux project. To be sur that what we get in Flux is correct, I used Ampere theorem.
In your case, the formula that I used to compute the flux density in the air gap is:
B=(Mu_0*N*i)/e. where:
N: number of turns in the rotor
I: current in the rotor (300 A)
E: air gap thickness
B=(4*pi() e-7*2400)/11 e-3 = 0.27 T.
I found the same thing as in Flux when I draw a path in the air gap.
As a conclusion, the value of the flux density in the air gap is correct.
Hope this help.
Best regards.
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Altair Forum User said:
Hi,
Sorry for the delay, time to analyze the Flux project. To be sur that what we get in Flux is correct, I used Ampere theorem.
In your case, the formula that I used to compute the flux density in the air gap is:
B=(Mu_0*N*i)/e. where:
N: number of turns in the rotor
I: current in the rotor (300 A)
E: air gap thickness
B=(4*pi() e-7*2400)/11 e-3 = 0.27 T.
I found the same thing as in Flux when I draw a path in the air gap.
As a conclusion, the value of the flux density in the air gap is correct.
Hope this help.
Best regards.
thank you for your explanation. If I use your formula, the number of turns is actually 32.5 turns in the rotor. So, B=(4*pi() e-7*32.5*300)/11 e-3=1.1T. Can you please explain why you used 2400(8 turns?)? many thanks in advance. I have stuck on this for a while and this is the first time i encountered this problem since upgraded from Flux 11.1
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trying to bump up the queue again.
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Hi,
The path chosen to apply the Ampere theorem is on one rotor tooth. For this reason I divide the number of turns by 4. In the end the total is (32.5/4)*300=2400.
Best regards.
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Altair Forum User said:
Hi,
The path chosen to apply the Ampere theorem is on one rotor tooth. For this reason I divide the number of turns by 4. In the end the total is (32.5/4)*300=2400.
Best regards.
thank you for your help. the problem has been solved. the flux density is now 0.9 in the airgap as per my original assumption.
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