QUADCOPTER DESIGN ANALYSED

Last crawled date: 1 year, 10 months ago

This quadcopter design iS one of the most efficient tool to transfer basic needs . This is a quadcopter design which has a electronics, electronic speed controllers, motors, battery and payload in positions and all the arrangements within the specified weight.

This model has Engineering specificationsare as follows-
Max. permissible mass of airframe: 90 g
Mass of electronics: 42 g
Mass of batterie: 47 g
Total mass of motors and propellers: 26 g
Mass of wires: 25 g
Mass of payload: 250 g
Total permissible mass (without airframe): 390 g
Force of each motor: 1,17 N (120 g)
Total force of the four motors: 4,68 N (480 g)

Properties of my model:
Selected material: Ultem 9085
Density of material: 1,34 g/cm^3
Volume of part: 14 cm^3
Mass of part: 18,8 g

Mechanical values for FEM-Simulation:
Material Strength Allowable: 4500 PSI
Young's Modulus: 325 KSI
Poissons Ratio: 0,41

The model is available in STEP (.stp)- and (.stl)-format and can be used for a weight upto 250 grams.
All the attachments are as per the given grams and is one of the most powerful quadcopter.