PERFECTIONNEMENTS AUX CHAMBRES DE COMBUSTION POUR MOTEURS A TURBINE A GAZ

A combustion chamber for, for example, an aircraft gas turbine engine, has an upstream end wall protected by a plate serving as a heat shield, the shield-plate being spaced from the dome and cooled by fluid flowing through orifices in the dome. The shield plate is itself formed with a plurality of s...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	JACQUES EMILE JULES CARUEL ET GUY DANIEL STORA
Format:	Patent
Sprache:	fre
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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