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Group 2 conceptual

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Teklemichael Ghirmay
Teklemichael Ghirmay
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Design Group 2 Kat Donovan - Team Leader Andrew DeBerry Mike Kinder John Mack Jeff Newcamp Andrew Prisbell Nick Schumacher Conceptual Design for AME 441 Spring 2004
Group 2 – Ducted Design
Overview ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Aircraft Configuration (Requirements) ,[object Object],[object Object],[object Object],[object Object],[object Object],Design Drivers ,[object Object],[object Object]
Comparison Aircraft * Information from http://www.aerospaceweb.org/aircraft/bomber/yb49/ † Information from http://www.aerospaceweb.org/aircraft/bomber/b2/ ‡ Information from Design and Construction of a Remote Piloted Flying Wing , May 2, 1994
CAD Models Electronics Box Battery Pack (x2) Circuit Card Servo GPS Receiver Modem
CAD Models - Dimensions
[object Object],[object Object],[object Object],Airfoil Choice
Sample Lift Estimation http://www.grc.nasa.gov/WWW/K-12/airplane/foil2.html
Engine Selection: Astro Cobalt 15 9 oz Gear Motor Weight Data from www.astroflight.com 1/4 inch Prop Shaft Diameter 5/32 inch Motor Shaft Diameter 1.3 inches Motor Diameter 3.3 inches Gear Motor Length 400 watts Maximum Continuous Power 25 amps Maximum Continuous Current 2 amps No Load Currrent 8 to 12 volts Voltage Range 2.17 in-oz /amp Geared Torque 0.91 in-oz /amp Motor Torque/amp 652 rpm/volt Geared Motor Speed 1488 rpm/volt Motor Speed Ball Bearings Bearings Sm Cobalt Magnet Type 0.069 ohms Armature Resistance 7 turns Armature Winding 2.38 to 1 Gear Ratio 05 Geared Name p/n 615G Model No. ,[object Object],[object Object]
Power Estimate
Thrust Estimates
Thrust, Drag, Estimates
Weight & Drag Estimates 8.36 Total: 0.65 Main Battery 0.08 Speed Controller 1.5 Electronics Box 0.5 GPS & Transmitter 0.25 Receiver & Battery 0.32 Servo (x4) 0.06 Propeller 0.56 Engine (Cobalt 15) 0.6 Landing Gear 3.84 Structure Aircraft Weights (lbs)
Static Stability 2.910884 0.97 m.a.c. (ft) 8.307692 0.461538 L_ctr (x/L) Wing Center of Lift 2 L (f) Fuselage Length
Conclusions & Lessons Learned ,[object Object],[object Object],[object Object],[object Object],[object Object]
Design & Build Schedule 26 February: Present Detailed Design 4 March: Complete Parts List 16 March: Fabrication 6-9 April: Ground Tests 13-22 April: Flight Tests
Questions? Group 2: Nick Schumacher Andrew DeBerry Andrew Prisbell Jeff Newcamp Kat Donovan Mike Kinder John Mack

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Group 2 conceptual

  • 1. Design Group 2 Kat Donovan - Team Leader Andrew DeBerry Mike Kinder John Mack Jeff Newcamp Andrew Prisbell Nick Schumacher Conceptual Design for AME 441 Spring 2004
  • 2. Group 2 – Ducted Design
  • 3.
  • 4.
  • 5. Comparison Aircraft * Information from http://www.aerospaceweb.org/aircraft/bomber/yb49/ † Information from http://www.aerospaceweb.org/aircraft/bomber/b2/ ‡ Information from Design and Construction of a Remote Piloted Flying Wing , May 2, 1994
  • 6. CAD Models Electronics Box Battery Pack (x2) Circuit Card Servo GPS Receiver Modem
  • 7. CAD Models - Dimensions
  • 8.
  • 9. Sample Lift Estimation http://www.grc.nasa.gov/WWW/K-12/airplane/foil2.html
  • 10.
  • 14. Weight & Drag Estimates 8.36 Total: 0.65 Main Battery 0.08 Speed Controller 1.5 Electronics Box 0.5 GPS & Transmitter 0.25 Receiver & Battery 0.32 Servo (x4) 0.06 Propeller 0.56 Engine (Cobalt 15) 0.6 Landing Gear 3.84 Structure Aircraft Weights (lbs)
  • 15. Static Stability 2.910884 0.97 m.a.c. (ft) 8.307692 0.461538 L_ctr (x/L) Wing Center of Lift 2 L (f) Fuselage Length
  • 16.
  • 17. Design & Build Schedule 26 February: Present Detailed Design 4 March: Complete Parts List 16 March: Fabrication 6-9 April: Ground Tests 13-22 April: Flight Tests
  • 18. Questions? Group 2: Nick Schumacher Andrew DeBerry Andrew Prisbell Jeff Newcamp Kat Donovan Mike Kinder John Mack