Aerospace Instrument-Making Annotation << Back HIGH TEMPERATURE ELECTROMECHANICAL ENERGY CONVERTERS THAT CAN BE INTEGRATED IN TO AIRCRAFT ENGINE. PROSPECTS AND DESIGN PROBLEMS V.E. Vavilov, F.R. Ismagilov, I.Kh. Khayrullin, R.D. Karimov We prove the possibility of creating high-starter generatrov for installation in high-pressure shaft aircraft engine and indicated that in modern industry has created all the conditions for this. The main problems that may arise in the design of high-starter with generatrov high-coercivity permanent magnets and pre-payments made starter-generator for an ambient temperature of 300 C. Key words: aircraft engine, high-starter-generator, high-coercivity permanent magnets, high-pressure shaft. Contacts: E-mail: S2_88@mail.ru Pp. 48-56.