| 摘要 |
<p>1454206 Gas turbine engine combustion equipment- UNITED AIRCRAFT OF CANADA Ltd 1 Aug 1974 [2 Jan 1974] 34022/74 Addition to 1385903 Heading F1L In a modification of the primary/secondary airflow control arrangement described in Specification 1385903, the pivoted baffle (243) of that Specification is replaced by a baffle 38 mounted on axially slidable rods 42.</p> |
