Combustion chamber stress reducing means

Details Combustion chamber stress reducing means Combustion chamber stress reducing means

1977-08-29

1979-04-17

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3936, F02C 720

Patent

active

041493737

ABSTRACT:
A gas turbine engine is shown having an annular burner casing with an annular burner therein. A conventional fuel and air supply can be provided. The burner is formed of conventional louver construction at the forward part thereof with the last louver of both the inner and outer burner wall being welded to its upstream louver with a curled forward end being curled to extend away from the upstream louver. This connection is formed on the louvers which restrict the flow through the burner.

REFERENCES:
patent: 1816770 (1931-07-01), Gradl
patent: 2858673 (1958-11-01), Wirt
patent: 3468560 (1969-09-01), Cassel
patent: 3788065 (1974-01-01), Markowski

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