发明名称 Structure
摘要 <p>A structure such as a containment case (2) for a gas turbine engine (1) comprises an annular housing (3) made of composite material. A sleeve-like flange unit (4) is fitted onto an end of the housing (3) and is mechanically joined thereto by a first portion (31, 32, 33) of the composite material of the housing which projects into a recess (411) of the flange unit (4). This reduces or eliminates the need to use mechanical fasteners to connect the housing (3) to the flange unit (4).</p>
申请公布号 GB201017120(D0) 申请公布日期 2010.11.24
申请号 GB20100017120 申请日期 2010.10.11
申请人 GKN AEROSPACE SERVICES LIMITED 发明人
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