Drkwing
Mechanical
- Dec 10, 2004
- 39
I have recently started working in a project about the design of an anmanned Aerial Vehicle (UAV). My responsibility is the design of the Retractable Landing Gear. Based on my lack of previous experience on design of Landing Gears, I started reading on the topic and examination of different uavs on the market today.
The landing gear will be a tricycle one with the main lg legs are probably retracting into the fuselage. For the sake of simplicity regarding main landing gear, I plan to use composite legs without shock absorbers (just like in the GA series, gnat, predator, altus..)
In the concept phase, I calculated the main landing gear load, max kinetic energy to be absorbed, energy to be absorbed by tires. But in the literature the following procedure is the calculation of shock absorber stroke, which is absent on m design.
What is the procedure for calculating the length and section of the gear legs which will absorb the landing energy by deflection?
Any help will be greatly appreciated..
Thanx in advance.
The landing gear will be a tricycle one with the main lg legs are probably retracting into the fuselage. For the sake of simplicity regarding main landing gear, I plan to use composite legs without shock absorbers (just like in the GA series, gnat, predator, altus..)
In the concept phase, I calculated the main landing gear load, max kinetic energy to be absorbed, energy to be absorbed by tires. But in the literature the following procedure is the calculation of shock absorber stroke, which is absent on m design.
What is the procedure for calculating the length and section of the gear legs which will absorb the landing energy by deflection?
Any help will be greatly appreciated..
Thanx in advance.