The Importance of Core Loss Testing - Private Webinars - EASA | The Electro•Mechanical Authority
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To schedule private education for your group, contact:

Dale Shuter, CMP
Meetings & Expositions Manager

+1 314 993 2220, ext. 3335
dshuter@easa.com

1 hour of training

$500 for EASA Chapters/Regions
$800 for member companies
$1000 for non-members

How a webinar works

All EASA private webinars are live events in which the audio and video are streamed to your computer over the Internet. Prior to the program, you will receive a web link to join the meeting. 

The presentation portion of the webinar will last about 45 minutes, followed by about 15 minutes of questions and answers.

Requirements

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  • TV or projector/screen

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Private Webinars

EASA's private webinars are an inexpensive way to bring an EASA engineer into your service center, place of business or group meeting without incurring travel expenses or lost production time.

The list below is a sampling of topics that could be made available to your group. Any webinar previously presented by EASA staff could potentially be made available for your meeting!
See other topics presented previously.

Article

The Importance of Core Loss Testing

  • August 2026
  • Number of views: 85
  • Article rating:

Older versions of core loss testers used higher values (the upper limit was set at 10 W/lb. or even higher) for “marginal” and “good” watts-loss per pound. Today, we recognize that the core loss should not exceed five watts/pound, and there should not be hot spots more than 15 degrees C hotter than ambient. Both of those considerations are critical. A half-inch diameter (12mm) hot spot will probably not raise the watts loss, but the localized hot spot can lead to premature winding failure. Both the core loss and hot spot temperature MUST be considered when evaluating a core prior to rewind. Eddy-current losses in a core vary as the square of the lamination thickness – or diameter of the hot spot. That means a ¼" (6mm) diameter hot spot generates about 80 times as much heat as a single lamination.

Figure 1 is a winding failure in a large synchronous alternator. Figure 2 is the same alternator with a failure in the same location. Although a core hot spot was identified, it was decided not to fix the hot spot due to an emergency required repair. The second failure occurred within an hour of operation. It is telling just how much the top sticks along two teeth have discolored due to heating from a core that was still “bad.”

Image

Figure 1: This winding failure shorted laminations in the core.

Image

Figure 2: This failure resulted from hot spots due to shorted laminations, which resulted from the first winding failure. This winding failed in under an hour of operation.



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