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Prototype Fabrication, Economic, & Test Plan QDR

Purdue University AAE 451 Fall 2006 Team 4. Prototype Fabrication, Economic, & Test Plan QDR. Tung Tran Matt Drodofsky Haris Md Ishak Matt Lossmann. Mark Koch Ravi Patel Ki-Bom Kim Andrew Martin. Overall Schedule. Build Groups. Fuselage: (Ki-Bom Kim Tung Tran)

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Prototype Fabrication, Economic, & Test Plan QDR

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  1. Purdue University AAE 451 Fall 2006 Team 4 Prototype Fabrication, Economic, & Test Plan QDR Tung Tran Matt Drodofsky Haris Md Ishak Matt Lossmann Mark Koch Ravi Patel Ki-Bom Kim Andrew Martin

  2. Overall Schedule

  3. Build Groups • Fuselage: (Ki-Bom Kim Tung Tran) Construct main support and bulkheads Main wing attachment Main landing gear and attach points • Wing: (Andrew Martin Matt Lossmann) Main wing construction Flaperon construction Pitot tube routing Dihedral angle consideration • Tail Section: (Haris Md Ishak Ravi Patel) Horizontal and Vertical Fin construction Elevator and Rudder construction Tail wheel attachment • Propulsion and Component: (Matt Drodofsky Mark Koch) Assemble powerplant Develop wiring diagrams Determine control linkage layout Flightline

  4. Economic Plan • Company Overhead Purdue University is providing Build team with facilities, machine shop, and electrical power for testing. • Person-Hours for R&D Total Hours for Project: 1750 Hours Current Hours: 1009 Hours Groups having PDR presentations were opened for OT hours • Budget Cost (Allotment $250.00) Propulsion: $168.94 Landing Gear: $24.27 Control Linkage: $23.79 Fuselage: $33.00

  5. Flight Test Plan • Static Test (Purdue Airport Facility) power up the aircraft receiver and transmitter. Actuate all control surfaces to full deflection look for correct deflection movement, binding, and surface strikes • High Speed Taxi (McAllister Park) power up engine and run down runway to insure tail wheel controllability • Flight Test (McAllister Park) First flight: (Yaw feedback control off) Brief liftoff and land to feel initial handing qualities of aircraft. Second flight: Sustaining flight with turns to evaluate aircraft stability and control. Third flight: Go through procedures to set rate gyro gain. FULL THROTTLE FLIGHT!

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