发明名称 ЭНЕРГЕТИЧЕСКАЯ ГАЗОТУРБИННАЯ УСТАНОВКА
摘要 FIELD: power engineering. ^ SUBSTANCE: proposed gas-turbine power plant contains gas-turbine engine whose input device is furnished with stator flange. Rotor of free power turbine of gas-turbine power plant has shaft, useful load drive flange, labyrinth disk and radial-thrust bearing from side of input device. Relief space of free power turbine is formed by stator flange, labyrinth disk and input device housing. Labyrinth disk is installed by ring radial flange on ring radial flange of useful load drive shaft and is axially fixed by flange of useful load drive. Drive shafts of useful load and rotor of free power turbine are connected by torque transmitting device made, for instance, in form of splines and are also connected by coupling bolt. ^ EFFECT: improved reliability of gas-turbine plant by reducing stresses in drive shaft and axial forces acting onto radial-thrust bearing. ^ 2 cl, 4 dwg
申请公布号 RU2004110258(A) 申请公布日期 2005.10.20
申请号 RU20040110258 申请日期 2004.04.05
申请人 Открытое акционерное общество "Авиадвигатель" (RU) 发明人 Сулимов Даниил Дмитриевич (RU);Васкецов Олег Анатольевич (RU);Климов Валерий Николаевич (RU);Щипицын Валентин Петрович (RU);Кузнецов Валерий Алексеевич (RU);Черн ев Иван Анатольевич (RU)
分类号 F01D3/02;F02C7/36 主分类号 F01D3/02
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