Considering practical environment

whether parts in an airborne optoelectronic equipment may break

deform? How much deform of a part is? If it possible utilizing less material in a part and it’s performance is not affected? Using engineer analysis software we tackle the problem. Expounding characteristic of airborne optoelectronic platform frame structure show us syntony frequency is importation

adding sustentation and bore can increase it

minishing moment of inertia by reduce distance part to rotor can increase it too. Setting XXX optoelectronic platform frame seat structure for example

describe the progress of engineering analyze

by drawing as a result

stress

meet an emergency

distortion

safety factor can keep a view manifestation completely

we find out the weak link and redundancy part.The examples in the article illustrate guidance and importance of engineer analysis

it supplies us guidance for a better design.