发明名称 HONEYCOMB STRUCTURE
摘要 PURPOSE:To enhance heat resistance and corrosion resistance by forming a honeycomb core of a heat-resistance metal bonded with a solder material while forming surface plates of a heat-resistant metal bonded with a solder material, and covering at least one of the surface plates with a ceramic flame spray coating film. CONSTITUTION:A honeycomb core 2 is formed using a thin plate composed of nickel, cobalt, iron, aluminum, titanium and other heat-resistant alloy being a heat-resistant metal as a base material. Then, the thin plates are bonded at predetermined places by brazing, that is, a solder material such as silver or nickel solder. Surface plates 3 are composed of a heat-resistant metal and bonded to both surfaces of the honeycomb core 2. At least one of the surface plates 3 is covered with a ceramic flame spray coating film 4. This ceramic flame spraying film 4 is composed, for example, of silicon carbide, silicon nitride, zirconia or alumina.
申请公布号 JPH02128832(A) 申请公布日期 1990.05.17
申请号 JP19880282692 申请日期 1988.11.09
申请人 SHOWA AIRCRAFT IND CO LTD 发明人 NOMOTO KAZUHIKO
分类号 B32B15/04;B32B3/12;B32B7/02;B32B18/00;C23C4/10 主分类号 B32B15/04
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