Mechanismus pro uvolnění břemene při pádové zkoušce.

Abstract

The bachelor thesis is describing design of shackle release mechanism for drop test of aircraft and design of whole device. The first part is a search of existing devices and evaluation of appropriateness for drop test of aircraft. Based on the evaluation of variants, the actual mechanism of the device is designed. The dimensions of the individual components are designed from stress caused by the wight of the load or adapted to the requirements of the design. The strenght of the components is checked analytically. The bachelor thesis also includes drawing documentation containing drawing assemly and manufacturing drawing of one component.

Description

Subject(s)

device, shackle release mechanism, own design, strength calculation, drawing documentation

Citation