Abstract
Examples of solving problems according to the method described in the first part of this work in the processing of contacting surfaces by turning, milling and grinding, as well as the comparison of calculated and experimental values of the contact convergence of surfaces, and the algorithm for calculating the determination of machining modes in order to ensure a given contact stiffness are given. The article describes the practical application of the research results in relation to the assembly unit of an aircraft gas turbine engine.
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