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Information × Registration Number 0307U003941, 0107U007617 , R & D reports Title Design of the rotating blading in turbocompressor TK32C-01 for strength in the visco-elastic zone popup.stage_title Розрахунок обертового напрямного апарата турбокомпресора ТК32С-01 на міцність у пружно - пластичній зоні для ВАТ "Пензадизельмаш" Head Vorobiev Yu.S, Registration Date 05-09-2007 Organization A.Podgorny Institute for Mechanical Engineering Problems of the National Academy of Sciences of Ukraine popup.description2 A concrete mathematical model has been developed for the construction and a procedure has been worked out for defining the deflected mode of the guide vanes in a turbocompressor developed by OJSC Penzadieselmash. This will ensure in-depth analysis of the deflected mode of the guide vanes in turbocompressor ТК32С-01 with account of its geometry and loads acting on the construction. Investigations have been conducted and recommendations have been worked out for reducing the level of stresses occurring in the guide vanes when they operate in the elastoplastic zone of stresses. In turn, this will increase the strength of the guide vanes in turbocompressor ТК32С-01 Product Description popup.authors popup.nrat_date 2020-04-02 Close