(adsbygoogle = window.adsbygoogle || []).push({}); 1. The problem statement, all variables and given/known data

(I have done parts i) through v) correctly. It is the remaining two I'm stuck on.

A toroid of rectangular cross-section has a height of 10mm, an inner diameter of 68mm and an outer diameter of 82mm. It is made of iron and is wound with 118 closely-spaced turns. When a current of 2A flows, calculate;

i)the mmf around the toroid

ii)the magnetic field-strength within the toroid

iii)Using B-H curve determine the flux density and flux in the ring,

iv)the relative permeability at this point on the curve

A 1mm air gap is then cut in the toroid. The current is still 2A. Calculate;

v)the new flux density in the ring,

vi)the mmf around the ring, and across the air gap.

vii) It is then required to establish a flux density of 0.75T in the air gap. Calculate the current needed to do this.

Answers to parts vi) and vii)

vi) 53, 183 A-t

vii) 8.0 A

2. Relevant equations

[tex]m.m.f.=NI=BS(R_{m}iron+R_{m}air)[/tex]

[tex]R_{m}=\frac{l}{\mu_{0}\mu_{r}S}[/tex]

where

[tex]\mu_{r}=557[/tex],

I have [tex]B=0.21T[/tex] (although the answer gives it as 0.23)

[tex]R_{m}(iron)=4.787*10^6[/tex] and [tex]R_{m}(air)=11.365*10^6[/tex]

[tex]S [/tex]= cross-sectional area = [tex]7*10^{-5}[/tex]

3. The attempt at a solution

I get the m.m.f. across the air gap correct if I use the value of B = 0.23T in answers. My answer was 0.21T and I found this was significant:

[tex]R_{m}(air)=\frac{l}{\mu_{0}S}[/tex]

[tex]m.m.f.=BS(R_{m}(air))[/tex]

[tex]=0.23*7*10^-5*11.365*10^6=183.5At[/tex]

I did as before with the iron, subtracting the 1mm from \piD for l (in metres)

[tex]m.m.f.=BS(R_{m}(iron)[/tex] where

[tex]R_{m}(iron)=\frac{l}{\mu_{0}\mu_{r}S}[/tex]

but I get 70, which is far from the answer of 53.

For the last part (vii) I don't know why it isn't simply

[tex]I=\frac{BS}{N}R_{m}(air)[/tex]

with this I get 5A rather than 8

Your help is much appreciated.

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# Air gap in toroid

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