propulsion presentation final [compatibility mode].pdf
TRANSCRIPT
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UAV EnginesBy: Nathaniel Crisler1, Onyewuchi Ebere2, Mahmoud Farhat 3, Natalie Marini 4, Janet
Massengale5, Kenneth McCloud6
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Unmanned Aerial Vehicle
► Commercial Applications:
Firefighting Oil and gas industry Agriculture Motion picture filming Journalism
► Military applications:
Surveillance Reconnaissance Striking Search and rescue Targets for training
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Common types
UAV type Engine Type Power Range (HP)
Micro Electrical 1
Mini Piston (2x2), Electrical 1-20
Tactical, Close range (75%) Rotary (Wankel) 20-90
MALE “medium alt. longend.” (15%)
Piston (4x4), Rotary 90-250
MALE Turbo-prop, turbo-jet >250
* Almost 90% of UAV engines requires power outputs from 20-250 hp
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Requirements
1. Long endurance - mission length of 20-50 hours
2. Compactness-High power/weight ratio, low volume.
3. Simple maintainability -Robustness, lower skills ground crews
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“The Wankel engine”
►A type of Internal Combustion Engine that uses a rotary design.
►Uses Four strokes cycle (Otto cycle).
►Developed in 1951 by Felix Wankel.
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Rotary Design
► 4 stroke engine (intake, compression, combustion, exhaust)
► Rotor on eccentric shaft.► Design to Minimize Volume
while Maximizing Compression ratio.
► Rotor – Triangular shaped with equaled width.
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Pros
►Much simpler comparing to its piston counterpart.
► Power to weight ratio is superior than piston engines.
► Smooth power flow and high RPM.
► Less mechanical losses
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Con
► Sealing, leaks from the apex seals greatly reduces efficiency of the engine.
► Poor emissions, unburntfuel is in the exhaust stream. Due to port overlap
► Low fuel efficiency and shorter engine life due to damaged seals.
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Performance Indicators
► Power to Weight Ratio► Fuel Type► SFC – specific fuel consumption
► BMEP – brake mean effective pressure►Engine’s capacity to do work independent of engine size
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Engine Comparison
EngineDisplacement(cc)
Maxpower(hp)
Maxtorque(lb-ft) BMEP (psi)
SFC(lb/HP/HR) Fuel
Weight(lbs) Cooling
300LCR 300 32 24.32 200.40 0.527 gas/avgas 26.2 liquid
300HFE 300 31 22.6 186.23 0.58 jp5/jp8/jet a1 27.1 liquid
600LCR 600 58 43.55 179.43 0.61 gas/avgas 46.7 liquid
600HFE 600 56 42 173.05 0.67 jp5/jp8/jet a1 46.7 liquid
AR731 208 38 26 154.50 0.57 avgas 21.7 air
• Rotron 300LCR chosen as best performing engine due to the BMEP and low SFC
• An engine must first provide the power needed for a specific application. Then BMEP and SFC are evaluated.
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Enhancing Performance
Increasing the fuel efficiency► Problem: Poor sealing between
the rotor and the chamber walls due to thermal expansion of engine block
► The engine block is constantly being heated where combustion is occurring and constantly being cooled near the intake
► Solution: design an exotic alloy or ceramic engine block that is more resistant to thermal expansion
► Result: increased torque and decreased SFC (for constant )
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Enhancing Performance
Increasing the fuel efficiency► Problem: High wear on the
inner wall of the engine block and poor sealing between rotor and chamber walls
► Solution: Use special cast iron apex seals
► Cast Iron is self-lubricating, reducing the amount of lubricating oil needed in the system
► Result: increased torque, decreased SFC, less emissions from burnt oil
Increasing the fuel efficiency► Problem: High wear on the
inner wall of the engine block and poor sealing between rotor and chamber walls
► Solution: Use special cast iron apex seals
► Cast Iron is self-lubricating, reducing the amount of lubricating oil needed in the system
► Result: increased torque, decreased SFC, less emissions from burnt oil
Increasing the fuel efficiency► Problem: High wear on the
inner wall of the engine block and poor sealing between rotor and chamber walls
► Solution: Use special cast iron apex seals
► Cast Iron is self-lubricating, reducing the amount of lubricating oil needed in the system
► Result: increased torque, decreased SFC, less emissions from burnt oil
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Enhancing Performance
Increasing the fuel efficiency► Problem: Incomplete burning
of fuel, large HC emissions► Solution: use fuel injectors to
control amount and timing of fuel supply
► Stratification techniques will increase the burning of fuel and decrease emissions
► Result: increased torque, decreased SFC, less emissions from unburnt fuel
Partial Direct Injection: Lean mixtureprovided by carburetor, rich mixture injected near spark plug
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Rotor Vs Piston
13B 1.3 Liters (146 hp @ 6500 rpm and 138 ft·lbf )
KA24DE 2.4 Liters (155 hp @ 5600 rpm and 160 ft·lbf)
Mazda Rx-7 (1989-1992) Nissan 240sx (1991-1994)
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QUESTIONS
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References► Nice, Karim. “How Rotary Engines Work”. http://auto.howstuffworks.com/rotary-
engine2.htm
► Karunakaran, K.P. "Application of Wankel Engine in Aircrafts and Ways of Increasing Its Fuel Efficiency.“
► "Rotary Engines for UAV Applications." Advanced Rotary Engine Technology. Rotron. Web. 1 Apr. 2015. <http://www.rotronuav.com/>.