Method for lowering no-load loss of transformer core and coil winding sleeving assembly
A no-load loss and coil winding technology, applied in the field of transformers, can solve the problems of increasing the reluctance of the iron core, increasing the no-load loss value of the amorphous alloy transformer core, etc., so as to reduce the no-load loss, reduce the noise value, and improve the overall performance. Effect
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Embodiment 1
[0051] This embodiment provides a method for reducing the no-load loss of the transformer core, including the following steps:
[0052] Firstly, each layer of amorphous alloy strips is overlapped end to end, and each layer of amorphous alloy strips forms an overlapping gap with another layer of amorphous alloy strips below, so as to obtain an amorphous alloy core.
[0053] Secondly, open the amorphous alloy core at the tower head according to the lapping sequence, and then fit the coil winding on the amorphous alloy core; after the fitting is completed, close the laps of the amorphous alloy core in sequence according to the strip stacking sequence.
[0054] Finally, inject the composite material into the lap space of the amorphous alloy iron core after the set, and let it stand for 30 minutes; the composite material includes epoxy powder, acetone and iron powder, and the mass ratio of epoxy powder, acetone and iron powder is 40 :70:1.
Embodiment 2
[0056] This embodiment provides a method for reducing the no-load loss of the transformer core, including the following steps:
[0057] Firstly, each layer of amorphous alloy strips is overlapped end to end, and each layer of amorphous alloy strips forms an overlapping gap with another layer of amorphous alloy strips below, so as to obtain an amorphous alloy core.
[0058] Secondly, open the amorphous alloy core at the tower head according to the lapping sequence, and then fit the coil winding on the amorphous alloy core; after the fitting is completed, close the laps of the amorphous alloy core in sequence according to the strip stacking sequence.
[0059] Finally, inject the composite material into the gap of the lapping head of the amorphous alloy iron core after the set, and let it stand for 60 minutes; wherein the composite material includes epoxy powder, acetone and iron powder, and the mass ratio of epoxy powder, acetone and iron powder is 60 :90:1.
Embodiment 3
[0061] This embodiment provides a method for reducing the no-load loss of the transformer core, including the following steps:
[0062] Firstly, each layer of amorphous alloy strips is overlapped end to end, and each layer of amorphous alloy strips forms an overlapping gap with another layer of amorphous alloy strips below, so as to obtain an amorphous alloy core.
[0063] Secondly, open the amorphous alloy core at the tower head according to the lapping sequence, and then fit the coil winding on the amorphous alloy core; after the fitting is completed, close the laps of the amorphous alloy core in sequence according to the strip stacking sequence.
[0064] Finally, inject the composite material into the gap of the amorphous alloy core after the set, and let it stand for 50 minutes; the composite material includes epoxy powder, cyclohexanone and soft magnetic powder, and epoxy powder, cyclohexanone and soft magnetic powder The mass ratio is 47:76:1.
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