FINAL YEAR PROJECT PRESENTATION

“DEVELOPMENT OF PROPULSION SYSTEM

FOR SMALL DUCTED FAN UAV”

NAME FARAHIDA BINTI YACOB

MATRIC NO DD090121

SUPERVISOR DR. ZAMRI B. OMAR

PANEL 1) DR. BAMBANG BASUNO

2) DR. NOER HAYATI

PRESENTATION OUTLINE

INTRODUCTION

METHODOLOGY

RESULTS & DISCUSSION

CONCLUSION

RECOMMENDATIONS

INTRODUCTIONINTRODUCTION

PROPULSION SYSTEM

Propulsion means to push forward or drive an

object forward.

A propulsion system is a machine that produces thrust to push an object

forward.

Thrust is the force which moves any aircraft through the

air.

OBJECTIVE OF PROJECT

To produce a configuration layout of propulsion system for ducted fan UAV

by using SolidWork.

To determine suitable propulsion

system for small ducted fan UAV.

SCOPE

UAVDUCTED

FAN

Where suitable location for propulsion

system place

Parameter?

What propulsion system chooses?

PROBLEM STATEMENT

YESYES

START

GENERAL STUDY ABOUT UAV

RESEARCH ABOUT PROPULSION SYSTEM AND

DUCTED FAN FOR UAV

IDENTIFY COMPONENT

ANALYZING DATA AND AERODYNMIC

CONFIGURATION LAYOUT FOR PROPULSION SYSTEM IN DUCTED FAN

PROPULSION SYSTEM

SELECTION

FINISH

NONO

METHODOLOGY

RESULTS

EXPLODED VIEW OF SMALL DUCTED FAN UAV

TYPE OF EQUIPMENT IN PROPULSION SYSTEM

TYPE OF EQUIPMENT IN PROPULSION SYSTEM

BRUSHLESS MOTOR PROPELLER

ELECTRONIC SPEEED CONTROLLITHIUM POLYMER BATTERY

EXPLODED VIEW OF PROPULSION SYSTEM

ANALYSIS FOR MASS

ANALYSIS FOR THRUSTANALYSIS FOR THRUST

GRAPH OF OPERATION

COMPARISON BETWEEN WEIGHT & THRUSTCOMPARISON BETWEEN WEIGHT & THRUST

From the analysis that have been made, we can see the value of thrust can produce a force for single system is 18.66N. As we know the weight of the model is 32.04 N, because of that it need double system of thrust that can produce 37.34 N force which is more than the weight to be able to take off.

32.04 N < 37.34 N

CONCLUSIONCONCLUSIONCONCLUSIONCONCLUSION

The development more focused on the propulsion system to the main objective to raise aircraft weighting less than 4kg and the second objective is do configuration layout for propulsion system small ducted fan UAV.

For the first planning, we planning used the glowplug engine, but to reduce the weight and save space, we choose brushless motor to replaced. Propulsion system used coaxial propeller to generate double thrust.

RECOMMENDATION

Review the system of remote control that can be implement on the aircraft .

Creating a more ergonomic design structure.Review the structure that can accommodate cargo aircraft

such as camera, voice recorder, scanner and other mobile devices.

Diversification of the propulsion system, for example, the aircraft may use an internal combustion engine, electric motor or using solar energy.

THANK YOU