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On the choice of parameters of device to reduce load on components of turbojet engine pressure vessels after fan blade breakage
Authors: Ivanov I.I. | Published: 27.05.2015 |
Published in issue: #10(631)/2012 | |
Category: Calculation and Design of Machinery | |
Keywords: gas-turbine engine, load reduction device, rotor, fan blade, breakage |
Computer-Aided Design and Strength Analysis of the Components of Air-Gas Channel of the Radial Turbine
Authors: Kiselev N.A. | Published: 29.07.2013 |
Published in issue: #3(636)/2013 | |
Category: Technology and Process Machines | |
Keywords: gas-turbine engine, centripetal turbine, three-dimensional shaping, air-gas channel, thermostressed state, CAD system |