1 The Air Jellyfish Group #1: Jacob Chard Ben Sponagle Chris Theriault Shane Yates Supervisor: Dr. Marek Kujath.

Slides:



Advertisements
Similar presentations
Stair Climbing Robot Team 7 Senior Design Project Dalhousie University Dept. of Mechanical Engineering Fall 2008.
Advertisements

Malte Marko Daniel MacDonald Stephen Thomas Matthew Gleddie
Group 5 Self-Assembling Picnic Table
Feasibility Study of Replacing an Industrial Hydraulic Lift System with an Electro-Mechanical Lift System Critical Design Review Thursday, 21 September.
Personal Mobility Lift Capstone Team Members: Jim Folgate Bill Beers Ryan Pelton David Zuercher.
 A radio controlled aircraft (model) is controlled remotely by a hand held transmitter & receiver within the aircraft.  The.
Abstract Since dawn of time humans have aspired to fly like birds. However, human carrying ornithopter that can hover by flapping wings doesn’t exist despite.
Team Shane Stumvoll, Alex Willard, Robert Yarnell, Hubert Jayakumar, Tim Teal 1.
The Helicopter.
Preliminary Design Review Group 13 – Flapping Wing MAV NASA Parker Cook George Heller Joshua Nguyen Brittney Theis.
NASA Lunabotics Mining Competition Interim Design Presentation Team 19: Aleks Fedoriw Duncan Haldane Arthur Pack Michael Pearse Carlos Ruiz.
Team 7.  Stephanie Beaton  Keith Gillis  Mark Larade  Eric Sharp  Yves Sharp  Supervisor: ◦ Dr. Marek Kujath 2.
Kelley Fletcher Dustin Eseltine Ryan Sargent Group 5.
Conceptual Design Presentation ME 4182 Team: Guys Engineering Nathan Bessette, Rahul Bhatia, Andrew Cass, Zeeshan Saiyed, Glen Stewart YJ Chok.
AN-NAJAH NATIONAL UNIVERSITY FACULTY OF ENGINEERING DEPARTMENT OF MECHATRONICS ENGINEERING STAIR CLIMBING WHEELCHAIR Prepared by: supervisor: Dua’a Dmadi.
Giving Bertha! LTA CDR David Dryjanski – Design/Construction, SolidWorks Expert Rachel Ellman - Design/Construction Carl Engel - Team manager, Propulsion.
Motion Rotary Motion Rotary motion is motion in a circle. The starting point for many mechanisms. Measurement: Rotary motion is measured in either angular.
The Cialitron by LevTech
Launch Lug – helps to guide the rocket upward until it reaches enough velocity for the fins to engage. Parachute – assists in the safe recovery of the.
PRINCIPLES OF FLIGHT CHAPTER 7 THE HELICOPTER.
Human Powered Submarine
Drag Queen LTA Completed Design Review Nestor Lara, 2004.
Wave Energy Conversion Team: Andrew Cameron Brent MacLean Helen McDonald Steve McDonald Nicholas Smith Supervisors:Dr. Robert Bauer Dr. Larry Hughes Richard.
EASELECTRIC Team 4 Adam Frank Jackie Jon. Introduction NSF Program: Expanding world of disabled artists Growing demand for adjustable easels Disabilities.
Design Team #11 1. Team Members Jeffery Aucoin Dima Eshtaya Sean Milley Jamie Zwicker Team Supervisor Dr. Robert Bauer 2.
ECE 480 Design Team 3 Doug’s Kitchen Robot Team Members - Thomas Manner - Ali Alsatarwah - Ka Kei Yeung - Daniel Phan Team Facilitator - Professor Lixin.
Erik Mueller Michael White. Introduction Problem Solution Load-cell Paddle-sensors Testing Q&A Sources.
UNC ROVERSAT IV University of Northern Colorado Critical Design Review Friday, June
R I T Team Members: Dan Lester → Team Lead Chris Feuerstein → Lead Engineer/Electrical Lead Mike Schwec → Electrical Support Jacob Hillmon → Electrical.
Completed Design Review Team Airblade Timothy Davenport Brian Guerrero Mark Kastantin Oscar Kataura William Peters Robert Taylor.
4 Spheres 3 Presents The Development of Gus™. Objectives  Reliability, stability and controllability  Most efficient battery usage possible  Clarify.
Ch Ch.15 Term 051. Ch-12  T051: Q: 16. A cube of volume 8.0 cm3 is made of material with a bulk modulus of 3.5×109 N/m2. When it is subjected.
Senior Design: Validation of Design December 15, 2008.
Concept Design Review Pinwheel Technologies (C3) Heather Blaha Matt Fuxa Joey King Michael McConnell Domenic Tassoni.
FIRST Robotics A view from the Systems Engineering Perspective Chris Mikus January 2, 2006 Rev 0.2.
Barry Barrios Structural Engineer Daniel Chaparro Structural Engineer Laura Garrity Propulsion Chad Lieberman Control Surfaces Adam Vaccaro Electrical.
Presents the ‘Easy-Bike’ Trevor Hennigar Hector MacQuarrie Paul Thompson David Smith (Absent) Supervisor: Peter Allen.
Final Presentation Crew: Mike Lanteigne Wallace Barkhouse Scott Donahoe Blair MacKay Captain: Dr. Jimmy Chuang April 4 th 2012.
Design Team #11 1.  Team Members Jeffery Aucoin Dima Eshtaya Sean Milley Jamie Zwicker  Team Supervisor Dr. Robert Bauer 2.
W IND –2– H 2 O MECH 4010: Design I Group 12: Jeffrey Allen Daniel Barker Andrew Hildebrand Supervised by: Dr. Alex Kalamkarov Client: Dr. Graham Gagnon.
Sail Away Group #11 Members: Scott Donahoe Mike Lanteigne Wallace Barkhouse Blair MacKay Supervisor Jimmy Chuang.
SEED David Millson Transportation Final Fall Presentation Daniel Sturnick Chris Abbot-Koch Lance Nichols.
Loading Apparatus for High Velocity Tissue Rupture Mechanical Engineering Dalhousie University Senior Design Project Winter 2010.
ZDC/Dummy Absorber Exchange Crane Proposal Paul Debbins Ianos Schmidt Univ. of Iowa - Nov. 5, 2007.
Flapping Wing MAV Group 13 – NASA Ames Parker Cook George Heller Joshua Nguyen Brittney Theis.
UCSD Human Powered Submarine Team – Odin’S Rage
 Model airplanes are sized down models of an aircraft  The calculations are easy and the importance is given to building of the plane.
Wave Power Generation Team #7 “Plugging into the Power of the Waves”
1 Air Jellyfish Design Team #1 Jacob Chard Ben Sponagle Chris Theriault Shane Yates Supervisor: Dr. Marek Kujath.
Choosing the electronics for RC planes By Rachit Aggarwal.
Automated Bridge Scour Inspection FSU/FAMU College of Engineering Team 7 Proposal 10/27/2010.
Unit 4: Mechanical Systems. Topic 2: The Wheel and Axle, Gears, and Pulleys.
Power An Introduction. Power  Learning Standard  ENGR-EP-1. Students will utilize the ideas of energy, work, power, and force to explain how systems.
William Enns Bray, Mitch Sharpe, Mike Kryski, Andrew Mattson, Nicole Marshall, Ashton Johnson Sponsor: Dr. Bertram Design Review 1.
BASICS OF RC PLANE. Overview  What is RC Plane?  RC Planes’ Parts and their Role  How planes fly?  Concepts and Terminologies of RC Plane  Stability.
RADIATION SOURCE Design Review Dmitry Gudkov BE-BI-ML.
SAND SAMPLING APPARATUS Eglin Air Force Base Gina Teofilak Richard Klimas Dan Mortensen Ruben De Sousa.
Interim Design Review Group 13 – Flapping Wing MAV NASA Parker Cook George Heller Joshua Nguyen Brittney Theis.
Students: Chen-Jay Xu Zheng-Xian Hung Advisor: Ru-Li Lin.
M icro A ir V ehicle Wing Deployment System April 7, 2005 MAV erick S olutions Todd Adkins Leroy Cohen Jr. Adam Hollrith Brian Moore Sponsored by: Eglin.
Topic 2: The Wheel and Axle, Gears, and Pulleys
Interim Design Team # 17 Michael Bunne, John Jagusztyn, and Jonathan Lenoff Department of Mechanical Engineering, Florida State University, Tallahassee,
AN EXPERIMENTAL STUDY OF FLEXIBLE MEMBRANE WINGS IN FLAPPING FLIGHT P SIVA KUMAR ROLL NO: 12M91D7607.
Automated slicing machine
The “Yarn Bully” Transport Cart
LESSON LD02 The Model Rocket
COSGC-Summer Internship 2010
LESSON LD02 The Model Rocket
COSGC-Summer Internship 2010
Presentation transcript:

1 The Air Jellyfish Group #1: Jacob Chard Ben Sponagle Chris Theriault Shane Yates Supervisor: Dr. Marek Kujath

 Introduction ◦ Inspiration ◦ Objectives ◦ Fall Term Testing and Calculations  The Design ◦ Alterations ◦ Fabrication  Budget  Testing and Evaluation  Conclusions and Recommendations 2

3 The Inspiration: Festo AirJelly  Remote-controlled airborne jellyfish  Central electric drive moves tentacles  Horizontal motion controlled by centre-of- mass-shifting pendulum Source:

 Mimic appearance of a jellyfish  Achieve flight  Create effective advertising medium 4

5 Fall Term Testing  Mock up Model ◦ Double Pulley Mechanism vs. Pulley/Spring Mechanism ◦ Flexible Legs vs. Hinged Paddles ◦ Oscillation Frequency  Calculations ◦ Torque Requirement ◦ Drag Forces ◦ Lift

6 Calculations: Drag Forces  Drag Forces were found to be small

7 Torque Requirement  Calculated to be 5.82 Nm  Motor selected based on torque requirement HG312 Geared Motor 312:1

8 Lift  2.1m diameter balloon produces 5kg Lift

 Frame  Vertical Propulsion Mechanism  Balloon  Motor/Crank  Steering Mechanism  Wireless Control  Circuitry 9

10 Carbon Fibre Tubes Rapid-Prototyped Joints Rapid-Prototyped Hinges Rapid-Prototyped Motor Platform Aluminum Tubes

11 Flexible flappers -Vinyl Beams -Foam Board Paddles Upward thrust throughout stroke

12

 Weather Balloon  Helium Used for Lift  Net/Ring Support 13

 Dual Propellers  Provide linear horizontal movement and turning capability 14

 FM transmitter and receiver  Servo motors activate on/off switches  Dedicated power supply 15

 Lithium-Polymer battery pack ◦ 3 cells (3.7 V each) ◦ 2600 mAh capacity  Provide ample power for >30 min of operation 16

17 ItemInitial DesignFinal Design Balloon attachment Nylon strapsCargo net over balloon; circular nylon strap around base of balloon AdvertisementsTBDPasted to paddles; banner attached to net FlappersTwo alternativesFlexible legs and rigid paddles Motor24 V DC12 V DC TransmissionSlider-rail “Scotch yoke” Crank with guide-holes for cables ControlElectronic speed controllers On/off switches flipped by servos

 Joints, hinges, and base of motor platform were rapid-prototyped  Frame assembled with press-fitting  Motor hub machined by Albert  Motor stand made of balsa; attached to base with epoxy  Sewn balloon attachment ring 18

ItemCost Helium$440 Rapid prototyping$440 Batteries and charger$400 Pulleys$130 Balloons$80 Frame rods$70 Primary motor$60 Flappers$30 Miscellaneous (fasteners, electrical parts, etc.)$120 Total$

 Three tests conducted in Sexton Gym  Number of tests limited by cost of helium (~$100 to fill balloon) 20

 Insufficient helium to achieve flight  Verified all mechanical systems ◦ Propellers moved device forward and provided turning capability ◦ Crank mechanism drove flappers with appropriate range of motion  Learned lessons concerning device assembly 21

 Achieved controllable flight ◦ Operated for over 30 minutes ◦ Reached height of 8 m ◦ Controlled from 28 m distance  Lessons learned ◦ Difficult to determine orientation of device from distance ◦ Helium leakage might limit run time 22

23

24

 Added advertisements and orientation indicators  Balloon ruptured during assembly 25

26 RequirementFulfilled Fit in a cube with 3m sides Generate vertical propulsion with flapping appendages Rise to a height of 8m Operate for a period of 30 minutes Be maneuverable in three dimensions Weigh less than 5 kg Be operational for a period of at least one day without maintenance

27 RequirementFulfilled Be safe to use. The building and testing of the prototype must also adhere to all safety procedures in accordance with Dalhousie University. * Be operational at a distance of 20 metres away from the operator. Have an attached advertisement that is interchangeable (i.e. the advertisement can be removed and replaced with a different advertisement). Function in an indoor and outdoor environment * Be aesthetically pleasing as it is to be used as an advertising medium to draw attention Be built under a budget of $ Be completed in conjunction with the deadlines set by the MECH 4010 syllabus.

Positives  Overall success  Most requirements met Negatives  Reliability issues ◦ Fragility of balloon  Time and effort for assembly  Cost of helium 28

 Balloon reliability enhancement ◦ Use a more rigid balloon ◦ Contain balloon in protective envelope  More advanced control system ◦ Height and obstacle detection ◦ Motor speed controllers  Organic steering mechanism 29

Sponsors  Shell Canada  Welaptega Marine  Air Liquide Individuals  Dr. Marek Kujath  Albert et al.  Dr. Julio Militzer  Peter Jones  Craig Arthur 30

31