Differentially geared regenerative reverse flow turbo shaft engi

Details Differentially geared regenerative reverse flow turbo shaft engi Differentially geared regenerative reverse flow turbo shaft engi

1977-06-20

1979-02-27

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Multiple fluid-operated motors

60 3951R, F02C 310, F02C 710

Patent

active

041412125

ABSTRACT:
A gas turbine engine is constructed having a forward differentially geared power output with an adjacent inlet for the introduction of airflow to the engine. After the airflow is compressed, it is discharged into an annular regenerator which is heated by exhaust gases. A reverse flow can-type combustor is located within the annular regenerator and receives the preheated air therefrom. The exhaust gas from the combustor is directed forward, first, to the power turbine and then to the gasifier turbine, after which it is exhausted through the regenerator.

REFERENCES:
patent: 2654565 (1953-10-01), Feilden
patent: 3100378 (1963-08-01), Austen et al.
patent: 3154918 (1964-11-01), Kronoyard
patent: 3452542 (1969-07-01), Saferstein et al.
patent: 3842595 (1974-10-01), Smith et al.
patent: 4030288 (1977-06-01), Davis et al.

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