发明名称 Heating system for composite rework of aircraft
摘要 <p>A method and apparatus comprising a laser unit and a controller. The laser unit is configured to generate a number of laser beams. The controller is configured to operate the laser unit to generate the number of laser beams resulting in a desired level of heating of a composite patch that cures the composite patch on a composite structure.</p>
申请公布号 EP2556915(A3) 申请公布日期 2013.10.30
申请号 EP20120179730 申请日期 2012.08.08
申请人 THE BOEING COMPANY 发明人 SAFAI, MORTEZA;MEREDITH, KIMBERLY D
分类号 B23K26/03;B23K26/06;B23K26/08;B29C73/10;B29C73/34 主分类号 B23K26/03
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