发明名称 РОТОР КОМПРЕССОРА ГАЗОТУРБИННОГО ДВИГАТЕЛЯ
摘要 FIELD: engines and pumps. ^ SUBSTANCE: invention is related to gas-turbine engines, namely, to weldless connection of disks in compressor rotor, and makes it possible to provide unambiguous ensured tightening of rotor (without gaps in joints ) by tightening only by rims. Rotor of gas turbine engine compressor consists of impellers (3) with splines (4) arranged on projecting elements (5) in connection with shaft (8). Compression nut (12) on shaft (8) is installed only on the side of front wheel (6), and thrust conical shell (7) connected to shaft is installed downstream rotor. ^ EFFECT: ensured rotor tightening (without gaps in joints). ^ 4 cl, 2 dwg
申请公布号 RU2007106636(A) 申请公布日期 2008.08.27
申请号 RU20070106636 申请日期 2007.02.21
申请人 Открытое акционерное общество "АВИАДВИГАТЕЛЬ" (RU) 发明人 Тункин Анатолий Иванович (RU)
分类号 F04D29/60 主分类号 F04D29/60
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