Gas turbine engines with particle traps

Power plants – Combustion products used as motive fluid – With safety device

Patent

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Details

60 39464, F23R 302, F02C 730

Patent

active

051521342

ABSTRACT:
A gas turbine engine (10) incorporates a particle trap (46) that forms an entrapment region (73) in a plenum (24) which extends from within the combustor (18) to the inlet (32) of a radial-inflow turbine (52, 54). The engine (10) is thereby adapted to entrap particles that originate downstream from the compressor (14) and are otherwise propelled by combustion gas (22) into the turbine (52, 54). Carbonaceous particles that are dislodged from the inner wall (50) of the combustor (18) are incinerated within the entrapment region (73) during operation of the engine (10).

REFERENCES:
patent: 2476507 (1949-07-01), Parmele
patent: 2575415 (1951-11-01), Grimac
patent: 2635564 (1953-04-01), Havemann
patent: 2706150 (1955-04-01), Lloyd
patent: 3274757 (1966-09-01), Wapler
patent: 4148186 (1979-04-01), Virr
patent: 4184326 (1980-01-01), Pane, Jr. et al.
patent: 4539918 (1985-09-01), Beer et al.

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