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9/30/2013 Systems Level Design ReviewP14462 Single Line Tethered Glider Team P14462 Sub-System Level Design Review Jon Erbelding Paul Grossi Sajid Subhani Kyle Ball Matthew Douglas William Charlock
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Team Introduction Team MemberMajor Sajid SubhaniIndustrial Engineer - Team Lead Paul GrossiMechanical Engineer Matt DouglasMechanical Engineer Jon ErbeldingMechanical Engineer Kyle BallMechanical Engineer Bill CharlockMechanical Engineer
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Agenda ●Project Description Review ●Engineering Requirements Review ●Functional Decomposition Review ●Top 3 Concepts from Last Review ●Concept Feasibility ●Glider Analysis and Feasibility ●Base Station Analysis and Feasibility ●Project Planning ●Work Breakdown Structure
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Project Description Review ●Goal: Design, build, and test a tethered, small-scale, human-controlled glider. ●Critical Project Objectives: ○ Maintain maximum tension on the tether ○ Sustaining horizontal and vertical flight paths ○ Measure and record tether tension and position ○ Understand the influential parameters for sustained, tethered, unpowered flight Glider Tether Base Station Operator w/ controller
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Engineering Requirements
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Functional Decomposition
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Review of Top 3 System Concepts 3 Single Axis Load Cell IMU with Single Axis Load Cell 2 Potentiometers with Single Axis Load Cell
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Glider Analysis
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Choosing the Glider Bixler v1.1 EPO Foam Wing span: 1.4 [m] Chord length: 0.2 [m] Mass: 0.65 [kg] Middle mounted propeller Only EPO Foam Phoenix 2000 EPO Foam Wing span: 2 [m] Chord length: 0.3 [m] Mass: 0.98 [kg] Front mounted propeller Reinforced
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Choosing the Glider The smaller Bixler glider creates less tension for a larger operating range Able to operate with an affordable load cell
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Flight Orientation
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Flight Analysis Wind Speed: ~ 11 mph
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Flight Analysis Wind Speed: ~ 22 mph
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Flight Analysis Wind Speed: ~ 44 mph
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Qualitative DOE Slower wind speed: lower tension Larger flight path radius: lower tension Beta angle peaks: ~ 94-95° Tension peaks: ~ 20 [m] tether length Tension must be less than 5000 [N] (1100 lbs)
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Quantitative DOE Choosing flight configuration Inputs Maximum allowable tension Observed wind speed Outputs Beta angle Tether length Flight path radius
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Bridle and Tether Setup Use a tension of 3000 lbs as an overestimate. Maximum allowable stress for Bixler glider: 30 MPa Bridle attached at two points on the fuselage causes structural failure at the wing root with 180 MPa
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Proposed Tether and Bridle Design
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Ideal Bridle Location Analysis Optimum tether location: 0.51 m from root. Optimum tether angle: 54 deg from airplane
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Wing Stress Analysis
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Maximum stress: 15 MPa
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Fuselage Stress Analysis
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Tether and Bridle Configuration
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Base Station Analysis and Feasibility
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2 Potentiometers and Single-Axis Load Cell Concept 1
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Vertical Rotation
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Static Analysis
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Dynamic Analysis
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Dynamic Analysis Continued
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Horizontal Rotation
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Static Analysis
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3 Single-Axis Load Cells Concept 2
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CAD Model ●Created 3-D model of the system in SolidWorks ●Works well when the ball joints are kept in tension as seen in Fig 1. ●Ball joints fail when they are put into compression as seen in Fig 2. Fig. 1 Fig. 2
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Base Station Equipment Phidgets 3140_0 – S Type Load CellBourns 3540S-1-103L Potentiometer
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Initial Base Station Budget Comparison P14462 Purchase List for 3 Load Cell Base Station Part DescriptionUnit PriceQtyIndividual Total Phidgets 3140_0 - S Type Load Cell503150.00 Ball End Joint Rod3.78622.68 Shipping 0.00 Total Order Price 172.68 P14462 Purchase List for Potentiometer Base Station Part DescriptionUnit PriceQtyIndividual Total Phidgets 3140_0 - S Type Load Cell50150.00 Bourns 3540S-1-103L Potentiometer20240.00 Miniature Aluminum Base-Mounted Stainless Steel Ball Bearings— ABEC-314.92229.84 Flanged Open 1/2 Inch Ball and Roller Bearing7.611 Shipping 0.00 Total Order Price 127.45
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Project Planning
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Work Breakdown Structure (10-12) ●Paul: ●Jon: ●Kyle: ●Matt: ●Saj: ●Bill:
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Questions?
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References http://www.hobbyking.com/hobbyking/store/__13994__Phoenix_2000_EPO_Composite_R_C_Glider_Plug_Fly_.html http://www.youtube.com/watch?v=ZfqGrzCKauw&list=PL0F209186D3388842
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