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    • 6. 发明授权
    • Strain and vibration resistant halogen light bulb for aircraft and method
    • 用于飞机和方法的应变和抗振卤素灯泡
    • US5644189A
    • 1997-07-01
    • US385952
    • 1995-02-08
    • Jeffrey D. Busby
    • Jeffrey D. Busby
    • H01K1/44H01J5/48
    • H01K1/44
    • A rigidified quartz-halogen light bulb and method for forming an improved vibration-resistant, high temperature light bulb is provided in which the terminals of the high temperature light bulb and lead wires attached to the terminals at attachment sites are coated with thermal-setting epoxy. The thermal-setting epoxy is covered with individual heat-shrinkable sleeves. High temperature, thermal-setting epoxy is fillingly adhered between the individual shrink-fit sleeves and is partially adhered to the base of the light bulb. An exterior shrink-fit tubing is applied, encasing all of the terminals, lead wires, attachment sites, epoxy coatings, individual sleeves and interposed fill epoxy. The entire composite is cured in position to provide the rigidifying structure in combination with the light bulb.
    • 提供了一种刚性化的石英卤素灯泡和形成改进的耐振动,高温灯泡的方法,其中高温灯泡的端子和附着在安装位置的端子上的引线涂覆有热定型环氧树脂 。 热定型环氧树脂被单独的热收缩套管覆盖。 高温热定型环氧树脂充分粘附在各个收缩套管之间,并部分粘附到灯泡的底部。 应用外部收缩配管,封装所有端子,引线,附着位置,环氧树脂涂层,单个套筒和插入的填充环氧树脂。 整个复合材料固化在适当的位置,以提供与灯泡组合的硬化结构。