The invention relates to a pretension aviation part heat-fatigue strength integrated measurement platform for the heat-fatigue strength of an aviation part. The platform comprises a main machine frame, a static force loading device, an exciting system, a temperature control system and a control part. Compared with platforms in the prior art, the platform disclosed in the invention has the following advantages: certain pretension is loaded on a sample at a preset temperature through the temperature control device, and pull and press fatigue test of the sample is carried out, so the pretension setting range is large, real working conditions of the aviation part are well simulated, and obtained experiment results approach the real fatigue life and the real fatigue strength.