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X-006  Mana Simo Alberti Presenting to  Boeing Huntington Beach CA November 20 th  , 2009
Design Goal ,[object Object],[object Object],[object Object],Alberti  -
CONOPS ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Alberti  -
Advanced Technologies ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Alberti  -
Fuselage Trade Study Alberti  -  Fuselage 3-3 2-2-2 2-4-2 Dimensions w: 12.5’ h: 15’ l: 117’ w: 15.5’ h: 15.5’ l: 105’ w: 16’ h: 16’ l: 90’ Cost 20 2 3 1 Drag C D 30 1 0.0062 2 0.0066 2 0.0067 Comfort/Space 10 3 1 2 Windowless 10 3 2 1 Stretchability 15 3 2 1 Loading Time 10 3 1 2 Innovation 5 2 1 1 100 57.5/100 59/100 75/100
Engine Trade Study Alberti  -  Engine Cycle CFM UDF CFM LeapX PW1000G RB2011 Readiness 5 4 2 1 4 Fuel Burn 35 1 4 2 3 Noise 20 4 1 1 3 Emissions 10 1 1 1 1 Thrust Range 5 2 2 1 2 Future 15 1 4 2 1 Weight/Size 10 3 2 1 3 100 72/100 52.5/100 75/100 50.5/100
Engine Layout Choice ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Alberti  -
2 Turbofans + 1 Unducted Fan ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Alberti  -  Thrust Lapse TSFC Unducted Fan 0.233 0.458 Turbofan 0.300 0.699 1/3 UDF Hybrid 0.278 0.578
Modified engine deck ,[object Object],[object Object],[object Object],Alberti  -
Constraint Diagram Alberti  -
Alberti  -  Legend 100 % Turbofan 100% Unducted Fan Hybrid Propulsion
Design Point Alberti  -  ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Wing  Loading Thrust to  Weight Take off  Weight Empty  Weight Fuel  Weight 145 0.25 146,000 73,000 36,000 120 0.21 142,000 71,000 34,000 106 0.18 145,000 72,000 35,000
Aircraft Sizing ,[object Object],[object Object],[object Object],[object Object],Alberti  -  % of fuel
3-View -change Alberti  -  92 ft 45 ft 118 ft
Wing ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Alberti  -
V Tail ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Alberti  -
Aerodynamic Analysis ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Alberti  -
Parasite Drag Buildup Alberti  -  ,[object Object],Effect of HLFC on Drag
X63T18S  Airfoil ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Alberti  -  NASA - W. Pfenninger
Alternative Fuels ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Alberti  -
Noise and Emissions ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Alberti  -  Hackmod.com
Ground Integration Alberti  -
Questions? Alberti  -

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Aircraft Design for Boeing Phantom Works

  • 1. X-006 Mana Simo Alberti Presenting to Boeing Huntington Beach CA November 20 th , 2009
  • 2.
  • 3.
  • 4.
  • 5. Fuselage Trade Study Alberti - Fuselage 3-3 2-2-2 2-4-2 Dimensions w: 12.5’ h: 15’ l: 117’ w: 15.5’ h: 15.5’ l: 105’ w: 16’ h: 16’ l: 90’ Cost 20 2 3 1 Drag C D 30 1 0.0062 2 0.0066 2 0.0067 Comfort/Space 10 3 1 2 Windowless 10 3 2 1 Stretchability 15 3 2 1 Loading Time 10 3 1 2 Innovation 5 2 1 1 100 57.5/100 59/100 75/100
  • 6. Engine Trade Study Alberti - Engine Cycle CFM UDF CFM LeapX PW1000G RB2011 Readiness 5 4 2 1 4 Fuel Burn 35 1 4 2 3 Noise 20 4 1 1 3 Emissions 10 1 1 1 1 Thrust Range 5 2 2 1 2 Future 15 1 4 2 1 Weight/Size 10 3 2 1 3 100 72/100 52.5/100 75/100 50.5/100
  • 7.
  • 8.
  • 9.
  • 11. Alberti - Legend 100 % Turbofan 100% Unducted Fan Hybrid Propulsion
  • 12.
  • 13.
  • 14. 3-View -change Alberti - 92 ft 45 ft 118 ft
  • 15.
  • 16.
  • 17.
  • 18.
  • 19.
  • 20.
  • 21.

Editor's Notes

  1. Simo Alberti
  2. 18% more weight 40% more fuel Simo Alberti