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UAS Propulsion Research
A Central Oregon Center of Excellence
Chris Hagen, PhD, PE
Shyam Menon, PhD
Matt Smith (HatchPD)
Sean Brown
School of Mechanical, Industrial and Manufacturing Engineering,
Oregon State University, Bend, OR, USA
Autonomous Systems @ OSU
Corvallis, OR, June 30th 2015
The team
o Additionally ESL has a team of 5 student researchers and an automotive master technician
1
Chris Hagen,
Asst. Professor, MIME
PI, Energy Systems Laboratory
Energy systems
Advanced IC engines,
Fuels, Control systems
Shyam Menon,
Post-doctoral
scholar
Small IC engines,
Engine testing,
Reacting flow
simulations
Matt Smith
President, Hatch PD
UAV engine
development,
Technology
commercialization
Sean Brown,
Graduate student
Small engine
testing, Solid
rocket design,
Business
development
George Roe,
Research professor
OSU-Energy Systems Laboratory
Power generation,
Energy storage, Energy
management, UAV
mission development
Facilities and Research Interests
o Our facilities
• 10 hp small engine dynamometer test cell (under development)
• Access to COCC’s automotive tool room resources
• Workspace at Hatch PD with
• Machining/welding/rapid prototyping capabilities
• Access to UAV flight test ranges
o Our interests
• Novel hybrid powertrain designs
• Engine performance measurement and improvement
• Thermal and power management systems
• Vertical take-off and landing (VTOL) capable UAV aircraft development
2
NASA GL-10 Greased Lightning
Hybrid VTOL UAV
Krossblade all-electric VTOL UAV
UAS Propulsion Research
o What’s available today?
o What do we want from a UAV propulsion
system?
• Range/Endurance
• Versatility/Configurability/Scalability
• Operation in a variety of climates
• Quiet operation for urban environments
o How do we plan to achieve these?
• Develop hybrid power systems
• Improve engine performance
• Develop modular & scalable engine designs
• Improve manufacturing processes
• Rapid prototyping/ 3-D printing
1 Hiserote, R.M., MS thesis, AFRL, 2010
3
Internal combustion engines Electric motors
Higher energy & power density
(order of magnitude)
Higher efficiency
(>90%)
Higher range & endurance Design flexibility
Better cold weather
performance
Quiet operation
Wide torque band
Hybrid powertrain configurations1
Engine performance map
2 Menon, S., Phd Thesis, 2010
IC engine performance scaling2
Supercharged 2-stroke (Hatch PD)
Rapid prototyped V-twin UAV engine (Hatch PD)
4
Dynamometer testing
Engine/Motors/Powertrains
Engine development
Turbocharging/Fuel injection/
Compression Ignition
Hybrid powertrain development
Series/Parallel/Dual-hybrid
UAS Propulsion Research:
A Central Oregon Center of Excellence
UAS aircraft development
VTOL airframe & propulsion

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Chris Hagen

  • 1. UAS Propulsion Research A Central Oregon Center of Excellence Chris Hagen, PhD, PE Shyam Menon, PhD Matt Smith (HatchPD) Sean Brown School of Mechanical, Industrial and Manufacturing Engineering, Oregon State University, Bend, OR, USA Autonomous Systems @ OSU Corvallis, OR, June 30th 2015
  • 2. The team o Additionally ESL has a team of 5 student researchers and an automotive master technician 1 Chris Hagen, Asst. Professor, MIME PI, Energy Systems Laboratory Energy systems Advanced IC engines, Fuels, Control systems Shyam Menon, Post-doctoral scholar Small IC engines, Engine testing, Reacting flow simulations Matt Smith President, Hatch PD UAV engine development, Technology commercialization Sean Brown, Graduate student Small engine testing, Solid rocket design, Business development George Roe, Research professor OSU-Energy Systems Laboratory Power generation, Energy storage, Energy management, UAV mission development
  • 3. Facilities and Research Interests o Our facilities • 10 hp small engine dynamometer test cell (under development) • Access to COCC’s automotive tool room resources • Workspace at Hatch PD with • Machining/welding/rapid prototyping capabilities • Access to UAV flight test ranges o Our interests • Novel hybrid powertrain designs • Engine performance measurement and improvement • Thermal and power management systems • Vertical take-off and landing (VTOL) capable UAV aircraft development 2 NASA GL-10 Greased Lightning Hybrid VTOL UAV Krossblade all-electric VTOL UAV
  • 4. UAS Propulsion Research o What’s available today? o What do we want from a UAV propulsion system? • Range/Endurance • Versatility/Configurability/Scalability • Operation in a variety of climates • Quiet operation for urban environments o How do we plan to achieve these? • Develop hybrid power systems • Improve engine performance • Develop modular & scalable engine designs • Improve manufacturing processes • Rapid prototyping/ 3-D printing 1 Hiserote, R.M., MS thesis, AFRL, 2010 3 Internal combustion engines Electric motors Higher energy & power density (order of magnitude) Higher efficiency (>90%) Higher range & endurance Design flexibility Better cold weather performance Quiet operation Wide torque band Hybrid powertrain configurations1 Engine performance map 2 Menon, S., Phd Thesis, 2010 IC engine performance scaling2 Supercharged 2-stroke (Hatch PD) Rapid prototyped V-twin UAV engine (Hatch PD)
  • 5. 4 Dynamometer testing Engine/Motors/Powertrains Engine development Turbocharging/Fuel injection/ Compression Ignition Hybrid powertrain development Series/Parallel/Dual-hybrid UAS Propulsion Research: A Central Oregon Center of Excellence UAS aircraft development VTOL airframe & propulsion