Fuel vaporizers for a gas turbine engine combustion engine

Details Fuel vaporizers for a gas turbine engine combustion engine Fuel vaporizers for a gas turbine engine combustion engine

1984-10-15

1988-05-10

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combustion products generator

60756, F02C 722

Patent

active

047426845

ABSTRACT:
A fuel vaporizer for a gas turbine engine combustion chamber comprises a hollow cylindrical stem open at one end and branching into two radial branch ducts at the other end which terminate in outlets facing towards the inlet end. In order to ensure more even cooling of the vaporizer stem, the fuel injector which lies inside the stem has two outlets which direct fuel onto those parts of the interior wall of the stem which lie between the branch passages, and a baffle divides the interior of the stem to ensure that each branch passage is fed with fuel from only one fuel injector, and each fuel injector supplies only one branch passage.

REFERENCES:
patent: 2956404 (1960-10-01), Kassner et al.
patent: 3626444 (1971-12-01), Carvel
patent: 4275564 (1981-06-01), Kappler et al.

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