发明名称 Method for heating or cooling seal for fixing metal insert on composite material part of e.g. turbojet, of aircraft, involves heating or cooling seal by heater/cooler placed in contact with metal insert
摘要 <p>The method involves heating or cooling a seal by a heater/cooler (10) placed in contact with a metal insert (2), where the metal insert includes an opening (18) such that a head (16) of the heater/cooler is placed inside the opening. The head of the heater/cooler and the opening of the insert are connected by a threaded connection, where the heater/cooler is portable such as gun type, and the heater/cooler includes an electric inductor (14) or cold liquid cooperating with a thermal transmission bar (15). An independent claim is also included for a method for separation of a metal insert from a composite material part.</p>
申请公布号 FR2991408(A1) 申请公布日期 2013.12.06
申请号 FR20120055001 申请日期 2012.05.30
申请人 SNECMA 发明人 HENRY PHILIPPE, PAUL, MARIE;CHICHERY EMMANUEL;ELISSEEFF TIMOTHEE
分类号 F16B11/00 主分类号 F16B11/00
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