发明名称 Core-molded shrink-plastic cover sealing locking device inside detachable section of e.g. aircraft body shell, has perimeter sealed and adhered to mounting surface
摘要 The perimeter (25) of the open side (23) of the cover (20), surrounds a locking device on the inside of the structural section. It includes a hole (29) through which a locking bolt can be moved back and forth. The bolt engages an opposite opening in the structural section. Along the perimeter, the cover is adhered using a sealant mass, onto a corresponding mounting surface on the interior of the structural section. An independent claim is included for the method of making the cover. A shrink plastic section is laid over a molding core. The core has an edge extending beyond its base. The shrink section is heated to a predetermined temperature over a given interval, to achieve the required shrinkage. It is then cooled over a set temperature range for a given interval. The projecting region left at the base is cut away, to leave a perimeter suitable for sealing as described. The cover is then positioned and sealed onto the surface provided on the structural component. Preferred features: Before heating the shrink plastic, its projecting edge is held firmly by a clamping plate held by fasteners to the underside. Edge separation is facilitated by a groove surrounding the core.
申请公布号 DE10012001(A1) 申请公布日期 2001.09.27
申请号 DE20001012001 申请日期 2000.03.11
申请人 DAIMLERCHRYSLER AG 发明人 HOFER, ANDREAS
分类号 B64C1/14;(IPC1-7):B62D25/24 主分类号 B64C1/14
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