发明名称 SHRINKWRAP SYSTEM
摘要 <p>A fuselage of an aircraft (204, 202) or other portion of a motivecraft is sealed with a heat shrinkable film section (200). After the film section (200) is emplaced, a double-sided adhesive strip or adhesive transfer (206) is wrapped therearound. Then, adjoining sections (201) 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 (201) of heat shrinkable sheets assembled in similar overlapping fashion. The heat shrinkable material (200) may be pre-formed to loosely conform to the sections of the craft (204) to which it is to be adhered. A plurality of such loosely conformable sections (201) can be pre-packaged in a kit form having the adhesive medium (206) disposed at the outer or free edges thereof. The shrinkable material may be a multi-layered material having a shinkable first layer and a cushioning second layer.</p>
申请公布号 WO1998010930(A1) 申请公布日期 1998.03.19
申请号 US1997017135 申请日期 1997.09.15
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