Gas turbine power plant

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

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60 3975, F02C 310

Patent

active

045985421

ABSTRACT:
A gas turbine engine is of a size suitable for generating electrical and heat energy for domestic and other purposes. The engine has a low number of components, and some of the components are capable of performing more than one function. For example, the engine has a centrifugal compressor driven by a centripetal turbine through a shaft. The compressor and turbine are mounted in a casing comprising a two part core and two end plates. The gas flow ducting is formed by surfaces on the compressor and turbine rotors, the core and the two end plates.

REFERENCES:
patent: 2709889 (1955-06-01), Mount
patent: 2709893 (1955-06-01), Birmann
patent: 2821067 (1958-01-01), Hill
patent: 2946192 (1960-07-01), Hambling
patent: 3422800 (1969-01-01), Haye
patent: 3751886 (1973-08-01), Sokolowski

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