发明名称 GAS TURBINE PLANT
摘要 FIELD: aviation. SUBSTANCE: gas generator 1, power turbine 2, outer drive units 3 and 4 part and units of plant control system 5 are placed on transportable platform 8 during assembly. Heat shield 11 and antivibrating device 13 are also mounted, after which alignment and testing jobs are connected at the Manufacturing plant and transportable platform 8 with components carried on it is delivered to point of operation and is secured to foundation by means of fastenings 9. During operation of plant, outer drive units 3 and 4 and part of units of control system 5 are located in colder zone, thus enhancing their operational reliability. Operational reliability is also enhanced by antivibrating devices 12. Outer drive units 3 and 4 and part of units of control system 5 are mounted on platform 8 from beneath which makes them accessible which is of great importance for performing scheduled maintenance and repair jobs. EFFECT: improved operational characteristics. 1 dwgn
申请公布号 RU2117797(C1) 申请公布日期 1998.08.20
申请号 RU19960124183 申请日期 1996.12.25
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "A.LJUL'KA-SATUR 发明人 CHEPKIN V.M.;MARCHUKOV E.JU.;SOROKIN K.JU.;TARASOV N.JA.;CHERNOV E.I.
分类号 F02C7/20;(IPC1-7):F02C7/20 主分类号 F02C7/20
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