| 摘要 |
<p>An improved bulkhead for dual industrial and aero gas turbines with annular or can combustors that may be formed by one or more bulkhead elements (10). Each element has a fuel-air channel (12) havig an air inlet (11) and a fuel-air mixtre outlet (13). Each element further includes at least one manifold for liquid (14) or gas (16) fuel. The channel and the manifold are formed by a plurality of etched layers of macrolaminate or platelet material. Each element further includes an air cooling channel (42) for cooling the backside of the bulkhead.</p> |
