MOUNTING SYSTEM FOR MECHANICAL-SHOCK RESISTANT PRINTED CIRCUIT BOARD (PCB)

A shock resistant fuselage system includes first and second fuselage side walls (804, 806), each of the first and second fuselage side walls (804, 806) having a plurality of guide posts (802, 1006), and a printed circuit board (PCB) 800 rigidly attached to at least one of the first and second fusela...

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Bibliographic Details
Main Author NICOLOFF WILLIAM JOHN
Format Patent
LanguageChinese
English
Published 02.01.2018
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Summary:A shock resistant fuselage system includes first and second fuselage side walls (804, 806), each of the first and second fuselage side walls (804, 806) having a plurality of guide posts (802, 1006), and a printed circuit board (PCB) 800 rigidly attached to at least one of the first and second fuselage side walls (804, 806), the PCB 800 having a plurality of guide slots 1008, each of the pluralityof guide posts (802, 1006) slideably seated in a respective one of the plurality of guide slots 1008 so that elastic deformation of the PCB 800 is guided by the guide slots 1008 between the first andsecond fuselage side walls (804, 806). 抗冲击机身系统包括:第机身侧壁和第二机身侧壁(804、806),第机身侧壁和第二机身侧壁(804、806)中的每个具有多个引导柱(802、1006);和印刷电路板(PCB)800,其刚性地附接到第机身侧壁和第二机身侧壁(804、806)中的至少个,PCB 800具有多个引导槽1008,多个引导柱(802、1006)中的每个可滑动地安置在多个引导槽1008中的相应的个引导槽中,使得PCB 800的弹性变形在第机身侧壁和第二机身侧壁(804、806)之间由引导槽1008引导。
Bibliography:Application Number: CN201680015783