发明名称 Method of making a thermally stable composite honeycomb panel
摘要 A method for forming a thermally stable honeycomb panel which may be used in constructing large mirrors employs thermally stable composite planks comprised of about 50% graphite fibers and of about 50% borosilicate glass. These planks which are formed by hot pressing in vacuum serve as a basic construction material. The thermally stable honeycomb panel is comprised of a core member, a backplate member, and a faceplate member which are bonded by bonding process after a wet frit paste is first applied and then dried to remove volatile solvents. The bonding is completed in an oven in an air atmosphere at a temperature sufficient to melt the glass in the frit paste after the organic binder material is boiled out. After holding the honeycomb panel components at a predetermined temperature for ensuring that all the glass in the frit is melted, the bonded panel is allowed to cool to room temperature. The glass re-soldifies to form bond strengths between the core member, backplate member, and faceplate member which exhibit parent material strength. The thermally stable honeycomb panel has a thermal expansion value in the range from about -5 to about +5 X 10-7 inch/inch/ DEG C. over a range of about 0 DEG C.-300 DEG C.
申请公布号 US4692367(A) 申请公布日期 1987.09.08
申请号 US19860856064 申请日期 1986.04.24
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY 发明人 RICHTER, MARK A.
分类号 B32B3/12;C03B11/14;C03C14/00;G02B5/08;G02B7/182;(IPC1-7):B32B7/04;B32B31/20 主分类号 B32B3/12
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