发明名称 A COMBINATION OF A STARTER TURBINE AND A RESONANT COMBUSTION APPARATUS
摘要 1,210,521. Alloy laminate. NORTH AMERICAN ROCKWELL CORP. 1 Sept., 1967 [1 Sept., 1966; 3 Oct., 1966], No. 40150/67. Heading B5N. [Also in Divisions F1 and F2] Valve reeds 75 in an inlet valve assembly for gas turbine combustion apparatus, see Division F1, comprises outer layers of thin high-temperature alloy, e.g. beryllium nickel, and an inner layer of woven heat-resistant fabric, e.g. fibre glass impregnated with a phenolic resin.
申请公布号 GB1210521(A) 申请公布日期 1970.10.28
申请号 GB19670040150 申请日期 1967.09.01
申请人 NORTH AMERICAN ROCKWELL CORPORATION 发明人 ROBERT LELAND BINSLEY;ROBERT STANLEY SIEGLER
分类号 F02C7/277 主分类号 F02C7/277
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