发明名称 Shrinkwrap system
摘要 A fuselage of an aircraft or other portion of a motive craft is sealed with a heat shrinkable film section. After the film section is emplaced, a double-sided adhesive strip or adhesive transfer is wrapped therearound. Then, adjoining sections of film are adhered to the tape or adhesive to form an overlap. When heat is applied to the film an airtight seal is formed. The adhesive film may be used to adhere together adjacent other sections of heat shrinkable sheets assembled in similar overlapping fashion. The heat shrinkable material may be pre-formed to loosely conform to the sections of the craft to which it is to be adhered. A plurality of such loosely conformable sections can be pre-packaged in a kit form having the adhesive medium disposed at the outer or free edges thereof. The heat shrinkable material may be a multi-layered material having a shrinkable first layer and a cushioning second layer.
申请公布号 AU4592597(A) 申请公布日期 1998.04.02
申请号 AU19970045925 申请日期 1997.09.15
申请人 OTHELL BICKERSTAFF 发明人 OTHELL BICKERSTAFF
分类号 B32B5/08;B64F1/00;C09J5/10 主分类号 B32B5/08
代理机构 代理人
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