The invention relates to an
aerospace current-carrying
slip ring temperature rise modeling method based on multi-
physics field
coupling, and belongs to the technical field of conductive friction pairs. The method comprises the following steps: firstly, calculating a theoretical
contact region of a
brush contact and a confluence disc, and calculating
contact resistance and
contact resistance heat of the
brush contact and the confluence disc based on conductive spots; in addition, the resistance
Joule heat is calculated based on the resistance of the
bus plate, and the friction heat between the
sliding contact and the
bus plate is further calculated. and finally, the total heat generated by the
contact resistance heat, the confluence disc resistance
Joule heat and the friction heat is synthesized, the heat dissipation rate is calculated through heat
radiation, and the heat dissipation rate and the generated heat reach
dynamic balance to calculate the steady-state temperature. Compared with a previous experimental measurement method, the method has the advantages that the
coupling relation among a thermal field, a force field and an
electric field is explored, modeling is performed on a temperature rise mechanism of the current-carrying
slip ring for
spaceflight, and factors influencing the temperature of the current-carrying
slip ring are analyzed, so that the method has the advantages of saving a large amount of funds and time and improving the working reliability of the
satellite current-carrying slip ring.