摘要 |
The gas turbine plant has a compressor (5, 6), a combustion engine (16), and a turbine (4), coupled to the compressor via a transmission (8, 9, 11, 12). Compressor rotor and turbine rotor are formed by corresponding parts of outside mass-produced tubro machines. The rotors are each formed by a radial rotor of a mass-produced exhaust gas turbocharger. The turbine acts via a multistage reduction gear (8, 9) on a driven shaft (10). This additionally serves to drive several compressors, and auxiliary units, e.g. fuel pump (17), lubricating oil pump (18). ADVANTAGE - Economical production costs, even with low production runs.
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申请人 |
BAYERISCHE MOTOREN WERKE AG, 8000 MUENCHEN, DE |
发明人 |
REGAR, KARL-NIKOLAUS, DR., 8000 MUENCHEN, DE |