Nozzle wall

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle with jacketed or hollow...

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Details

2989001, 60267, F02K 997, F02K 182, F02K 964

Patent

active

052265986

ABSTRACT:
A nozzle wall for two-dimensional (2D) hot gas nozzles of rocket or jet engines has a multilayer structure, in which a thermally conductive layer is flexibly connected to a support structure and a sliding layer is arranged between them to permit parallel movement of the thermally conductive layer. Also, a manufacturing method for the nozzle wall allows successive operations to be automatic to allow quality control inspections between these operations.

REFERENCES:
patent: 3127737 (1964-04-01), Ledwith
patent: 3460759 (1969-08-01), Gregory et al.
patent: 3690103 (1972-09-01), Dederra et al.
patent: 3768256 (1973-10-01), Butter et al.
patent: 3910039 (1975-10-01), Fortini
patent: 4078604 (1978-03-01), Christl et al.
patent: 4582678 (1986-04-01), Niino et al.

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