WEBVTT 00:00:00.452 --> 00:00:02.807 Certificate specific loss times core mass 00:00:02.822 --> 00:00:04.197 is only a starting point. 00:00:05.037 --> 00:00:07.301 Sheet tests do not reproduce production 00:00:07.316 --> 00:00:08.939 joints and assembled clamping. 00:00:09.803 --> 00:00:11.950 At corners, flux crosses gaps and 00:00:11.965 --> 00:00:13.808 transfers between laminations. 00:00:14.660 --> 00:00:16.100 At a three-phase T-joint, 00:00:16.261 --> 00:00:17.650 its direction changes. 00:00:18.514 --> 00:00:20.361 Cutting and clamping also change the 00:00:20.376 --> 00:00:21.191 stress state. 00:00:22.043 --> 00:00:24.033 A building factor connects material 00:00:24.048 --> 00:00:25.905 performance to the finished core. 00:00:26.769 --> 00:00:28.343 The article gives about one point 00:00:28.358 --> 00:00:29.632 one to one point three for 00:00:29.647 --> 00:00:31.126 three-phase step-lap cores, 00:00:31.314 --> 00:00:33.353 depending on design and manufacture. 00:00:34.217 --> 00:00:36.400 It is not a universal constant. 00:00:37.251 --> 00:00:39.525 Compare quotations using material grade, 00:00:39.621 --> 00:00:41.634 thickness, the named loss-test method, 00:00:41.756 --> 00:00:43.187 and the building factor with its 00:00:43.202 --> 00:00:43.834 basis. 00:00:44.686 --> 00:00:46.767 Then compare calculated loss at the 00:00:46.782 --> 00:00:48.157 design flux density.