The use of composite materials in modern designs is one of the promising areas. Despite a number of advantages, the use of composite materials imposes a number of restrictions on their use. One of them is a binder’s degradation temperature. The revision of the existing methodology for determining the thermal state of the compressor wheel through the use of modern calculation tools and their experimental justification will allow further reliable thermal calculation taking into account the anisotropy of material properties. For carrying out computational research and testing manufacturing technology, a three-dimensional model of the impeller of a centrifugal compressor and the motor shaft was developed.
A new methodology is proposed for designing professional retraining programs for aviation, rocket, and space industry employees, focused on the formation of the necessary competencies. The novelty of the proposed method is in the formalization of the design process and the use of digital technologies. The advantage is the use of a modular principle of program design, which provides the opportunity to implement individual training paths for workers in industrial enterprises. The methodology was successfully tested at the Moscow Aviation Institute (National Research University) in the provision of educational services to enterprises in the aviation and aerospace industries.
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