| 摘要 |
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 plurality of 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 and second fuselage side walls (804, 806). |
