Double-walled combustion chamber shell having combined convectiv

Details Double-walled combustion chamber shell having combined convectiv Double-walled combustion chamber shell having combined convectiv

1977-02-01

1978-08-08

Garrett, Robert E.

Power plants

Combustion products used as motive fluid

External-combustion engine type

60 3966, 431351, 431353, F02C 718

Patent

active

041048741

ABSTRACT:
A combustion chamber shell, particularly for aircraft turbojet engines, cisting of an assembly of sleeves each of which comprises two parallel facings connected and braced to each other by multiple longitudinal ribs which form an equal number of channels for the passage of the cooling air. The sleeves are connected to each other by annular parts which, to the front and to the rear of the sleeve facings, form vents which are arranged with respect to each other in such a fashion that the air entering into the chamber through the said channels flows in them from rear to front.

REFERENCES:
patent: 2958194 (1960-11-01), Bayley
patent: 3360929 (1968-01-01), Drewry
patent: 3545202 (1970-12-01), Batt et al.
patent: 3899876 (1975-08-01), Williamson
patent: 3899882 (1975-08-01), Parker
patent: 3978662 (1976-09-01), Dubell et al.

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