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    • 5. 发明授权
    • Holographic transfer lamination materials and process
    • 全息转印层压材料及工艺
    • US5360501A
    • 1994-11-01
    • US46463
    • 1993-04-07
    • L. Gordon Bolt
    • L. Gordon Bolt
    • B32B17/10B32B37/00B32B37/02B32B38/10B32B38/14G02B27/00G02B27/01G03H1/02B32B31/00
    • B32B37/02B32B17/10018B32B38/10B32B38/14G02B27/0103G03H1/0252B32B2307/40B32B2307/412B32B2315/08B32B2331/00B32B2363/00G02B2027/0109G03H2250/12G03H2250/37G03H2260/10
    • Disclosed is a process for configuring a hologram (30) onto a final laminate (38) incorporating the hologram (30), including a car windshield or an aircraft canopy. The process includes first developing the hologram (30) on a process substrate (22). Intermediate the hologram (30) and the process substrate (22) is a thermoplastic layer (24). After the hologram (30) has been developed, the hologram laminate (20) including the process substrate (22), thermoplastic layer (24), and hologram (30) is applied to a first final laminate layer (34) by means of an adhesive (32) such that the hologram (30) is facing the first final laminate layer (34). Once this step is completed heat is applied to the hologram laminate (20) to melt the thermoplastic layer (24), thus removing the process substrate (22). Therefore, a second final laminate layer (40) can be applied to the opposite side of the hologram (30) without any drawbacks from the thickness of any additional support layers in the final laminate (38).
    • 公开了一种用于将全息图(30)配置到包含汽车挡风玻璃或航空器罩的包含全息图(30)的最终层压板(38)上的方法。 该方法包括首先在处理衬底(22)上显影全息图(30)。 中间体全息图(30)和处理基板(22)是热塑性层(24)。 在全息图(30)已经显影之后,包括处理基板(22),热塑性层(24)和全息图(30)的全息图层压板(20)通过以下方式施加到第一最终层叠层(34) 粘合剂(32),使得全息图(30)面向第一最终叠层(34)。 一旦完成该步骤,就将热量施加到全息图层压板(20)上以熔化热塑性层(24),从而去除工艺衬底(22)。 因此,可以将第二最终层压层(40)施加到全息图(30)的相对侧,而没有来自最终层压体(38)中的任何附加支撑层的厚度的任何缺点。