VESTNIK of Samara University. Aerospace and Mechanical EngineeringVESTNIK of Samara University. Aerospace and Mechanical Engineering2542-04532541-7533Samara National Research University70510.18287/2541-7533-2009-0-3-1(19)-253-259UnknownTheoretical definition of temperature fields at thermoplastic hardening of details of gas turbine enginesBarvinokV. A.vest@ssau.ruVishnyakovM. A.vest@ssau.ruIgnatievS. A.vest@ssau.ruSamara State Aerospace University0109200983-125325906062014Copyright © 2015, VESTNIK of the Samara State Aerospace University2015<p>In work the technique of theoretical definition of temperature fields at thermoplastic hardening is presented. As an example results of calculations for unilateral cooling of a large-sized detail of type of a disk of the turbine of gas turbine engines are shown. Comparison of settlement and experimental temperature fields is resulted.</p>Hardening thermoplastictemperature fieldsdeformationspressure residualУпрочнение термопластическоетемпературные полядеформациинапряжения остаточные