Designing toroidal inductors with DC bias
G. D. Smith, United States. National Aeronautics and Space Administration, Goddard Space Flight Center
National Aeronautics and Space Administration, 1964 - Technology & Engineering - 9 pages
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4C BIA9 4eronautics and 9pace 9mith 9pace Administration Acceptable requirements BIAS by G. D. bias is presented cir mil combinations of core core constants Core Number core size core winding factor curves employed DC BIAS derive two equations design are presented designing the inductor designing toroidal inductors desirable combinations equations and requirements equations for selecting establishing the inductor frequency for core G. D. Smith Goddard indicate the desirable inductance tolerance inductance with temperature inductor equations inductor is given inductor requirements INDUCTORS WITH DC Llp2 magnet45ing meets the requirements method of designing NA9A TECHNICAL NOTE NASA NA9A TN National Aeronautics number of turns oersteds OT9 price peak current practical method procedure for establishing Q with frequency requirements are established requirements indicate selecting the smallest smallest core smallest possible core Smith Goddard Space step-by-step procedure Tables and curves TECHNICAL NOTE 4-505 toroidal core equa turns of wire variation of inductance variation of Q