Charlie Rush Zheng Wang Brandon Wedde Greg Wilson

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Presentation transcript:

Charlie Rush Zheng Wang Brandon Wedde Greg Wilson System Definition Review AAE 451 Team V Stephen Beirne Miles Hatem Chris Kester Jim Radtke Charlie Rush Zheng Wang Brandon Wedde Greg Wilson The Flying V Barn Owl

Outline Target Market Current Design Requirements Trade Studies Sizing Cost Concept Development Current Design Alternative Fuel Concept Evaluation 13 May 2019 AAE 451 Team V

General Aviation Market Review Product 4 Seat Single Engine Piston Aircraft for Hobbyists, Training Fleets, and Fixed Base Operators Powered by an Alternate Fuel Customer Needs 100LL Replacement Current staple fuel for GA piston engines Production uncertain after 2015 Provides opportunity to be first to market Petroleum fuel alternative for post peak oil 13 May 2019 AAE 451 Team V

Current Design Requirements ≤ 1500 ft takeoff distance to clear a 50 ft obstacle 600 lb payload with max fuel 150 kts max cruise speed 600 nm range ≥ 48”x46” cabin height x width Estimated GTOW of 2780 lbs Estimated base price of ~$316,000 ($2006) 13 May 2019 AAE 451 Team V

Trade Studies All trade studies were done assuming by varying one of the following and keeping the remainder at the base value shown Range (600nmi) Cruise Speed (150 kts) L/D (12) Payload weight (450 lbs, +150 for pilot) Prop efficiency (0.9) bhpSFC (0.42) Empty weight fraction was based on a nonlinear regression curve fit of a database of similar aircraft Fuel fraction was calculated from a series of weight fractions for our design mission 13 May 2019 AAE 451 Team V

Trade Studies (cont.) 13 May 2019 AAE 451 Team V

Trade Studies (cont.) 13 May 2019 AAE 451 Team V

Trade Studies (cont.) 13 May 2019 AAE 451 Team V

Acquisition Cost Trade Study Three cost estimating relationships: GA Plane Library Modified DAPCA Airframe Weight Relationship. Average yields purchase price of ~$316,000.00 13 May 2019 AAE 451 Team V

Acquisition Cost 13 May 2019 AAE 451 Team V

Concept Generation and selection Pugh’s method List criteria Brainstorm concepts Evaluate and iterate Criteria: Engine Power GTOW Cruise Speed Safety Airport Compatibility Price Payload Pizzazz™ Stability Fuel Consumption Aesthetically Pleasing 13 May 2019 AAE 451 Team V

A Few Initial Concepts 13 May 2019 AAE 451 Team V

Concepts Generated after two Pugh Iterations   Concept A Concept B Landing Gear Fixed Gear/Faring Tricycle Gear Wing Low Wing Low Wing with Winglets Straight Wing Tail Conventional Tail Cockpit Avionics Analog Cockpit Glass Cockpit Construction Al Al frame composite skin Propeller Fixed Pitch Variable Pitch Fuel Bio Diesel 13 May 2019 AAE 451 Team V

Current Main Concept Three View 13 May 2019 AAE 451 Team V

Cabin Three View 13 May 2019 AAE 451 Team V

Fuel Choice SFC Numbers for selected Alternative Fuels Bio-Diesel is our fuel of choice!! Fuel SFC (lbs/hp*hour) Diesel #2 0.37516 Bio-Diesel B100 0.42518 Ethanol 0.53829 Methanol 0.7067 Liquid Hydrogen 0.1269 13 May 2019 AAE 451 Team V

Information From Existing Diesel Engines Range of Brake Specific Fuel Consumption: 0.36 – 0.40 lbs/hp*hr Weights range from 185 lbs – 350 lbs Power ranges from 135 hp – 300 hp 13 May 2019 AAE 451 Team V

Relationship between Engine Weight and Power 13 May 2019 AAE 451 Team V

Design Space Determination Design Point 13 May 2019 AAE 451 Team V

Current Design GTOW (lbs) 2780 LOA (ft) 26 Wingspan (ft) 36 Swing (ft^2) 115 W/S (lb/ft^2) 24.1 P/W (ft/s) 0.0706 sTO (ft) 740 Vcruise (kts) 150 horsepower ~200 Acquisition Cost $316,000 Bio-diesel powered Low tapered wing with winglets Conventional tail 5 deg tail upsweep 13 May 2019 AAE 451 Team V

Concept Evaluation Design Requirements Concept A Concept B Cirrus SR 22  T/O Distance <1500 + - 600 lb Payload  150 kts cruise speed  600 nm range  48”x46” cabin dim.  <2800 lb GTOW Acq. Cost <$300k  -   - 13 May 2019 AAE 451 Team V

Synopsis Four-Seat Single-Engine Piston Prop GA Aircraft Bio-Diesel Fueled Low Wing (Possibly With Winglets) Conventional Tail Fixed Tricycle Gear 13 May 2019 AAE 451 Team V

Charlie Rush Zheng Wang Brandon Wedde Greg Wilson This Concludes Our System Definition Review AAE 451 Team V Stephen Beirne Miles Hatem Chris Kester Jim Radtke Charlie Rush Zheng Wang Brandon Wedde Greg Wilson The Flying V Barn Owl

slide left intentionally blank 13 May 2019 AAE 451 Team V

3 View of Diesel Engine 13 May 2019 AAE 451 Team V

Diesel Cycle vs. Otto Cycle Engines 13 May 2019 AAE 451 Team V