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Information × Registration Number 0209U001860, 0108U008446 , R & D reports Title Development of Design Configuration of New Generation Engine in 10 to 15 t Thrust Class for Civil and Transport Aircraft. popup.stage_title Head KRITSYN GENNADY, Registration Date 12-03-2009 Organization Zaporozhye Machine-Buiding Design Bureau Progress State Enterprise named after Academician A.G. Ivchenco popup.description2 Technical report No. 12Д.00.00.000 ПТ entitled "Preliminary Technical Proposal on AI-2112D-1 turbofan engine" (118p.p.) and Technical report No. 12Д.00. 000-01 ПТ entitled "AI-2112D-1 three-shaft turbofan engine in class ranged from 10 to 15 tons of thrust for passenger and transport aircraft" (560 p.p.) were issued according to these frameworks. Engine designation: АI-2112D-1. The technical documents resulted from these technical reports are listed below: - Review of situation on the market of for passenger and transport aircraft powered by TFE in class ranged from 10 to 15 tons of thrust; - Determining of key tendencies to development of technical level values of TFE in class ranged from 10 to 15 tons of thrust; - Defining a strategy to be pursued in development of technology advance to design a new generation TFE in class ranged from 10 to 15 tons of thrust; - Identification of parameters and structural configuration for AI-2112D-1demonstrator baseline version in class ranged from 10 to15 tons of thrust; - Identification of АI-2112D-1 component parameters and development of engine preliminary mathematical model; - Thermodynamic analysis; - Altitude -airspeed performance; - Evaluation of gasdynamic characteristics for engine compressors, combustion chamber and turbine, transition ducts, bypass duct; - Calculation and design study of engine key components; - Description of engine key systems; - Description of engine design; - Assessment of strength and service life of engine key parts; - Assessment of expected engine reliability values; - Assessment of engine standardization and commonality levels; - Engine overhaulability; - Study of engine maintainability and monitoring capability; - Selection of materials required for engine design; - Assessment of R&D scope to ensure development of a new generation TFE in class ranged from 10 to 5 tons of thrust; - Assessment of prospects for engine development; - Execution of preliminary patent investigations. Product Description popup.authors popup.nrat_date 2020-04-02 Close