Development of propulsion system for small ducted fan unmanned Ariel vehicle

1. 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

2. PRESENTATION OUTLINE
INTRODUCTION
METHODOLOGY
RESULTS &
DISCUSSION
CONCLUSION
RECOMMENDATIONS

3. IINNTTRROODDUUCCTTIIOONN

4. 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.

5. 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.

6. SCOPE

7. PROBLEM STATEMENT
UAV
DUCTED
FAN
Where suitable
location for
propulsion
system place
Parameter?
What propulsion
system chooses?

8. YYEESS
START
GENERAL STUDY
ABOUT UAV
RESEARCH ABOUT
PROPULSION SYSTEM AND
DUCTED FAN FOR UAV
IDENTIFY COMPONENT
ANALYZING DATA AND
AERODYNMIC
PROPULSION
SYSTEM
SELECTION
CONFIGURATION LAYOUT FOR
PROPULSION SYSTEM IN DUCTED FAN
FINISH
NNOO
METHODOLOGY

9. RESULTS

10. EXPLODED VIEW OF
SMALL DUCTED FAN UAV

11. BRUSHLESS MOTOR PROPELLER
TYPE OF EQUIPMENT IN
PROPULSION SYSTEM
TYPE OF EQUIPMENT IN
PROPULSION SYSTEM
ELECTRONIC SPEEED CONTROL
LITHIUM POLYMER BATTERY

12. EXPLODED VIEW OF
PROPULSION SYSTEM

13. ANALYSIS FOR MASS

14. AANNAALLYYSSIISS FFOORR TTHHRRUUSSTT

15. GRAPH OF OPERATION

16. COMPARISON BBEETTWWEEEENN WWEEIIGGHHTT && TTHHRRUUSSTT
32.04 N < 37.34 N
 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.

18. CCCCOOOONNNNCCCCLLLLUUUUSSSSIIIIOOOONNNN
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.

19. 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.

20. THANK YOU