THE DESIGN OF ELEMENTS OF COMPONENTS AND SUBASSEMBLIES OF AIRCRAFT ENGINES,

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Abstract:

This is a textbook for course work and diploma projects in the field of aircraft engine building. It can also be used by students in institutes of higher education and technical schools of other machine building specialties, as well as by engineering and technical personnel working in the field of aircraft engine building and gas turbine building. The various design solutions used in the design of aircraft engine parts and units are examined. In each chapter are discussed the general requirements on the examined design elements, and recommendations are given on the basis of experience gained in industry. After an over all evaluation of the given design procedure, actual examples are given of various solutions of some problem taken from the practice of aircraft engine building. Based on examples of the design of several units of gas turbine engines, the relationship is shown between the design solutions for separate elements of the unit according to the technical requirements the accepted and design scheme of a unit and an engine as a whole. Author

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