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Hovercraft Design. TEAM 1. Introduction. Team Members: Brandon Fichera Dave Rabeno Greg Pease Sean Gallagher. Sponsor: Dr. Stephanie Wright Delaware Aerospace Academy Advisor: Dr. Michael Keefe. Mission Statement:
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Hovercraft Design TEAM 1
Introduction Team Members: Brandon Fichera Dave Rabeno Greg Pease Sean Gallagher Sponsor: Dr. Stephanie Wright Delaware Aerospace Academy Advisor: Dr. Michael Keefe Mission Statement: To design a two person hovercraft for the Delaware Aerospace Academy that will demonstrate the scientific principles of a hovercraft, foster teamwork between students, and provide a fun, safe, and educational environment for all students involved.
Introduction Team, Sponsor, Advisor Problem/Mission Statement Background Concept Generation Selection Summary • Customers, Wants, Constraints • Benchmarking • System • Functional • Concept Development • Test Results, Modifications • Recommendations • Prototype Evaluation • Budget • Construction hours • Engineering Hours • Prototype Cost • Metrics • Target Values
Problem Background Delaware Aerospace Academy: • Sponsor of past UD senior design projects. • Specializes in teaching kids about technology • involved in the space program. Hovercrafts: • New and exciting technology that has yet to be • widely distributed. • Interesting tool for teaching scientific principles • to children
Customers • DAA • Dr. Stephanie Wright • Robert Bloom (Aerospace Engineer) • Students • High School Students • Junior High School - Eric Rabeno • Middle School - Ted & Elizabeth Pease • Teachers • High School - Martin Rabeno • Junior High School - Selina DiCicco • Industry • Ron Perkins - Educational Innovations • School System • Mark Ellison - Principle High/Jr High School
Wants • Educational • Demonstrate Hovercraft Principles to Children • Recreational • Make it fun, Cool Looking • Operational • - Maneuverable - Durable • - Reliable - Transportable • - Reproducible • Economical • - Low Cost
Constraints • Size of door in Spencer Lab (4.5’ by 6.3’) • Allowable Funds (~$2000) • Number of pilots (must be 2) • Operation (must be able to hover)
System Benchmarking • Triflyer - Hovercraft Design • Pegasus - Hovercraft Design • Universal Hovercraft - Hovercraft Construction Kits • Hover Club - Hovercraft Articles • Science Project - Laboratory Experiments
Smithsonian Air&Space Museum use videos to excite peoples interest Six Flags Amusement Parks use acceleration and jerk for fun Briggs and Stratton Engines HP, RPM and price Elibra / Hovertech Magnetic levitation Grainger Industrial Equipment Electric Motors RPM, HP and price Universal Hovercraft Fans for personal hovercrafts Northern Tool and Equipment Co. Gas Motors, price comparison Functional Benchmarking
Metrics & Corresponding Target Values 1) Number of Principles Taught - 3 2) Performance on lab experiment - average score = 80% 3) Height of hovering (Object Clearance) - ~6” 4) Skirt to ground clearance - 1/2” 5) Speed of Vehicle - 5 - 10 mph 6) Acceleration - 1 mph/s 7) Directions of Horizontal Travel - 360 degrees 8) Travel Range - limited by fuel capacity alone 9) Turning Radius - 15 ft 10) Fuel Efficiency/Capacity - 3 1/2 hrs 11) Cost - $2000 12) Weight - 1000 lbs.
Education & Recreation 1) Smithsonian Approach: use a video or descriptive poster to explain the principles to the children 2) Amusement Park Approach - just let children operate it and then attempt to explain how it works Operation 1) Means of Lift: 2) Power Supply: 3) Thrust Magnetic Levitation Electric Engine/Fan Fan(s) and Air Cushion Liquid Fuel Human Power Suspension Fuel Cells Rocket Thrust Concept Generation & Evaluation Against Metrics What are the different aspects of our project? Education, Operation, Recreation How can we satisfy our mission statement in various ways?
Concept Generation & Evaluation Against Metrics 1) With regard to Education & Recreation: - Choose Smithsonian Approach: - videos and posters allow for easy explanation 2) With regard to Operation: - Choose a fan/motor lift and thrust system - Magnetic Levitation = too expensive - Suspension System = too bulky, doesn’t demonstrate hovering principles - Human Power for thrust is a viable alternative - Choose Liquid Fuel: - engines are relatively inexpensive • Doesn’t demonstrate appropriate principles Choose: Fans and Air Cushion
Concept Selection: Mathematical Models (Lift) Steady-Flow Energy Equation Bernoulli’s Equation
Concept Selection: Mathematical Models (Lift) From Energy Equation: From Bernoulli’s Equation:
Concept Selection: Mathematical Models (Lift & Thrust) W = 1000lbs.(from Metrics) l = 10 ft w = 6 ft Pressure Required = 0.116 psi W = 1000lbs.(from Metrics) a = 1.5 ft/s2 (from Metrics) go = 32.2 ft/s2 (from Metrics) Thrust Force Required = 60lbs.
Final Concept Selection 1) Educational Poster (education) a) Discusses uses of Hovercraft as it relates to the Delaware Aerospace Academy b) Discusses Construction Design c) Explains principles of: - Lift - Thrust 2) Laboratory Experiment (education) - Students learn about lift first hand - Hands on approach similar to Smithsonian museum 3) Prototype HovercraftDemonstration (fun) - Students get to operate a working hovercraft
VIDEO Hovercraft Specs. Shape: Rectangular (10’ x 6’) - most stable - ease of construction Fan System Lift - 8 hp lift engine - 4 blade 26” diameter fan Thrust - 3.5 hp thrust - 2 blade 34” diameter fan Weight - empty weight of 450 lbs.
Test Results: Education • Lab: • Experiment and laboratory model brought into classroom and demonstrated to a class • All students were overwhelmingly enthusiastic about the lab and interested in the hovercraft • Students demonstrated understanding of principles by discussing them • Students wanted to build their own model “hovercrafts”. Asked how to build one
Modifications • Thrust Fan Replacement • Add collar to Lift Motor Shaft • Apply protective screens prior to delivery • Add ballast to the front of craft
Recommendations • Safety • Eye and Ear protection for pilots and operators • Familiarization of Safety manual • Run only under adult supervision • Perform safety check before and after operation • Maintenance • Familiarization of Operation manual • Check skirt for holes and tears
Budget • Materials (Wood, Hardware) - $ 734.45 • Lift fan, Skirt, Hub - $ 361.22 • 8hp Lift Engine - $ 358.70 • Thrust Fan - $ 157.00 • 3.5hp Thrust Engine - $ 167.99 TOTAL: $1779.36
Development and Fabrication Time • Engineering Concept Development • 110 hours • Fabrication • 610 hours • Redesign and Modification • 20 hours TOTAL: 740 hours
Projected Production Costs • Total Material Costs: • $1779.36 • Estimated Production Hours: • 200 hours • $25/hr • Projected Cost = $5000 + $1779.36 = $6779.36