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Swami Keshvanand Institute of Technology,
Management & Gramothan, Jaipur
Department of Mechanical Engineering
(session 2023-24)
Topic :- UAV Designing and Simulation
ZEROGRAVITY AERO SYSTEMS PRIVATE LIMITED
MNIT, JAIPUR
Submitted To:-
Mr. Praveen Saraswat
Associate Professor
Submitted By:-
Mohit Pareek
20ESKME059
2
• About the Zerogravity Aero Systems Private Limited
• Services, Products and Projects of Zerogravity Aero systems Pvt. Ltd.
• Introduction of Unmanned Air Vehicle and their Classification
• Projects on VTOL UAV
• Necessity of VTOL UAV
• Up gradation of VTOL
• Reference
3
About the Zerogravity Aero Systems
Private Limited
• We enjoy developing technology solutions that push the limits :
o World’s first live air quality monitoring and mapping UAV.
o This UAV has a onboard air quality measurement sensor which record the
quality of air and also transmit that data to the ground station.
o Using this system air quality of remote areas as well as inaccessible areas
can be checked.
4
• Why do we use it ?
o Aerial Photography
o Agriculture & Farming
o Commercial, Industrial & Construction
o Drone racing & Sports
o Fire Fighting
o Hunting Support
o Hard to Reach, High Altitude or Critical Processes
o Military & Armed Forces
o Mapping Applications
5
Services, Products and Projects of Zerogravity
Aero systems Pvt. Ltd.
Services
6
Products
7
Projects
8
Clients
9
Introduction of Unmanned Air Vehicle and
their Classification
• The UAV is an acronym for
Unmanned Aerial Vehicle, which is
an aircraft with no pilot on board.
• UAVs can be remote controlled
aircraft or can fly autonomously
based on pre-programmed flight
plans or more complex dynamic
automation systems.
• UAVs are currently used for a
number of missions, including
reconnaissance and attack roles.
10
CLASSIFICATION OF UAV
11
Projects on VTOL UAV
MATERIAL PROCUREMENT:
• DEPRON SHEET
• BALSA WOOD
• PROPELLER
• MOTOR
• ELECTRONIC SPEED CONTROLLER
• SERVOS
• BATTERY
• RC TRANSMITTER RECEIVER
• GPS
• CORO SHEETS
12
13
Fig: Balsa Wood
Fig: Motor and ESC
Fig: Propeller
Fig : Depron sheet
14
Fig: GPS
Fig: Coro Sheet Fig: Servos
Fig: LIPO Battery
15
Fuselage Construction
Fig: Fuselage Body
16
Wings Construction
Design of Airfoil shape :
Clark y airfoil tool
E374
17
Rectangular wing with internal support
Fig: Rectangular Wing Construction 2m Span With Semi Symmetrical Airfoil
18
Simple UAV Converted to VTOL UAV
Fig : Simple UAV Prototype Fig : Converted VTOL UAV Prototype
19
Necessity of VTOL
20
VTOL Resolve The Upper Problem
Up gradation of VTOL
21
Why up gradation is necessary ?
• In VTOL UAV consist –: 5 motor ( 4 for the lift ,and another for the
thrust)
• Due to this increase weight of UAV and decreases the payload
• Reduce flight time
• Increase battery consumption
22
Solution of The Upper Problem
Fig : Tri motor VTOL
23
VTOL SPECIFICATION
Type - VTOL 4+1
Wing Span - 2000 mm
Take-Off Weight - 7 kg
Propulsion - Brushless Motors
Endurance - 70 Minutes
Nominal Cruise Speed - 17 m/s
Stall Speed - 12 m/s
Max Speed - 30 m/s
Operative Temperature - 10˚- 50˚
GPS/PPK/RTK - Enable
Flying Mode - Fully Autonomous / Manual
Video Quality - up to 4K
Onboard Sensors - Air Speed Sensor, PPK, RTK
Battery - Lithium polymer and Lithium Ion
24
Some Design part on Fusion 360
Fig : winglet design
Fig : quad copter body design
25
Fig : camera casing Fig : Airfoil wing design
Reference
26
• https://www.quora.com
• www.zenadrone.com
• www.kscst.iisc.ernet.in
• www.unmannedsystemstechnology.com
• www.nasa.gov
• en.wikipedia.org
• howthingsfly.si.edu
• www1.grc.nasa.gov
• pilotinstitute.com
• science.howstuffworks.com
• airfoiltools.com
• www.skytough.com
• www.paramountbusinessjets.com
• www.aerotime.aero
• www.flyaeroguard.com
27
THANK
YOU

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SKIT SUMMER TRAINING 2023.pptx

  • 1. Swami Keshvanand Institute of Technology, Management & Gramothan, Jaipur Department of Mechanical Engineering (session 2023-24) Topic :- UAV Designing and Simulation ZEROGRAVITY AERO SYSTEMS PRIVATE LIMITED MNIT, JAIPUR Submitted To:- Mr. Praveen Saraswat Associate Professor Submitted By:- Mohit Pareek 20ESKME059
  • 2. 2
  • 3. • About the Zerogravity Aero Systems Private Limited • Services, Products and Projects of Zerogravity Aero systems Pvt. Ltd. • Introduction of Unmanned Air Vehicle and their Classification • Projects on VTOL UAV • Necessity of VTOL UAV • Up gradation of VTOL • Reference 3
  • 4. About the Zerogravity Aero Systems Private Limited • We enjoy developing technology solutions that push the limits : o World’s first live air quality monitoring and mapping UAV. o This UAV has a onboard air quality measurement sensor which record the quality of air and also transmit that data to the ground station. o Using this system air quality of remote areas as well as inaccessible areas can be checked. 4
  • 5. • Why do we use it ? o Aerial Photography o Agriculture & Farming o Commercial, Industrial & Construction o Drone racing & Sports o Fire Fighting o Hunting Support o Hard to Reach, High Altitude or Critical Processes o Military & Armed Forces o Mapping Applications 5
  • 6. Services, Products and Projects of Zerogravity Aero systems Pvt. Ltd. Services 6
  • 10. Introduction of Unmanned Air Vehicle and their Classification • The UAV is an acronym for Unmanned Aerial Vehicle, which is an aircraft with no pilot on board. • UAVs can be remote controlled aircraft or can fly autonomously based on pre-programmed flight plans or more complex dynamic automation systems. • UAVs are currently used for a number of missions, including reconnaissance and attack roles. 10
  • 12. Projects on VTOL UAV MATERIAL PROCUREMENT: • DEPRON SHEET • BALSA WOOD • PROPELLER • MOTOR • ELECTRONIC SPEED CONTROLLER • SERVOS • BATTERY • RC TRANSMITTER RECEIVER • GPS • CORO SHEETS 12
  • 13. 13 Fig: Balsa Wood Fig: Motor and ESC Fig: Propeller Fig : Depron sheet
  • 14. 14 Fig: GPS Fig: Coro Sheet Fig: Servos Fig: LIPO Battery
  • 16. 16 Wings Construction Design of Airfoil shape : Clark y airfoil tool E374
  • 17. 17 Rectangular wing with internal support Fig: Rectangular Wing Construction 2m Span With Semi Symmetrical Airfoil
  • 18. 18 Simple UAV Converted to VTOL UAV Fig : Simple UAV Prototype Fig : Converted VTOL UAV Prototype
  • 20. 20 VTOL Resolve The Upper Problem
  • 21. Up gradation of VTOL 21 Why up gradation is necessary ? • In VTOL UAV consist –: 5 motor ( 4 for the lift ,and another for the thrust) • Due to this increase weight of UAV and decreases the payload • Reduce flight time • Increase battery consumption
  • 22. 22 Solution of The Upper Problem Fig : Tri motor VTOL
  • 23. 23 VTOL SPECIFICATION Type - VTOL 4+1 Wing Span - 2000 mm Take-Off Weight - 7 kg Propulsion - Brushless Motors Endurance - 70 Minutes Nominal Cruise Speed - 17 m/s Stall Speed - 12 m/s Max Speed - 30 m/s Operative Temperature - 10˚- 50˚ GPS/PPK/RTK - Enable Flying Mode - Fully Autonomous / Manual Video Quality - up to 4K Onboard Sensors - Air Speed Sensor, PPK, RTK Battery - Lithium polymer and Lithium Ion
  • 24. 24 Some Design part on Fusion 360 Fig : winglet design Fig : quad copter body design
  • 25. 25 Fig : camera casing Fig : Airfoil wing design
  • 26. Reference 26 • https://www.quora.com • www.zenadrone.com • www.kscst.iisc.ernet.in • www.unmannedsystemstechnology.com • www.nasa.gov • en.wikipedia.org • howthingsfly.si.edu • www1.grc.nasa.gov • pilotinstitute.com • science.howstuffworks.com • airfoiltools.com • www.skytough.com • www.paramountbusinessjets.com • www.aerotime.aero • www.flyaeroguard.com