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PEN N S TATE 1 8 5 5 Small Propulsion Systems A 19 lbs thrust “small turbo-jet turbo-shaft gas turbine” Unusual engines for UAV/MAV applications Dr. Cengiz Camci
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Small Propulsion Systems
A 19 lbs thrust “small turbo-jet turbo-shaft gas turbine”
Unusual engines for UAV/MAV applications
Dr. Cengiz Camci
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A 19 lbs thrust “small turbo-jet turbo-shaft gas turbine”
Unusual IC engines for UAV/MAV applications
A MIGRATING COMBUSTION CHAMBER ENGINE (MCC)
A ROTATING CYLINDER/VALVE ENGINE
WANKEL (ROTARY) ENGINES
Various conventional IC engines
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High specific power Fuel efficientLight weight SilentSmooth running ReliableEasy to maintain Low production cost
UAVPROPULSION
SYSTEM
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A “small scale”turbo-jetturbo-shaft gas turbinedesign course
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Aero-thermo-mechanical Design of Small Gas Turbine Systems for
Unmanned-Aerial Vehicle (UAV) andEnvironmental Applications
(AERSP 597/497-K)
A three credit design course by:
Dr. Cengiz Camci 153-E Hammond Building
814 865 9871
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Introduction to Small Scale Turbomachinery systems (2)Fluid Mechanics and Thermodynamics of Turbomachinery
for Unmanned Aerial Vehicles (UAV) (4)Turbomachinery Component Design
Centrifugal compressor design (emphasize reduced size and use of light materials) (6)A single stage axial flow turbine design (6)Mechanical aspects of shaft and rotor disk design (3)Design of a low cost and efficient combustor (6)Inlet, diffuser and nozzle design system (6)
Gas Turbine Component Matching (3)Gas Turbine Health Monitoring and Control Mechanisms (3)Presentations and lab activities (6)
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Why is this design course offered?Small gas turbine systems with a maximum diameter of less than 10 inches have a tremendous application potential in Aerospace and Mechanical engineering systems. In Aerospace engineering, Unmanned-Aerial Vehicles (UAV) using small gas turbine systems are designed and operated for reconnaissance&surveillance, battle damage assessment, targeting and communications relay.
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UAV’s will also be highly effective in future Environmental Engineering applications for sensing chemical, nuclear and biological hazards. Collecting atmospheric/meteorological information using real time imaging and sensing devices is also possible by using UAV’s powered by small gas turbine systems.
Successful implementation of small gas turbines in ground based applications is also likely in the next century. Hybrid electric car recharging its batteries using a miniature gas turbine is an excellent automotive concept helping to effectively reduce environmental pollutants released to the atmosphere.
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SMALL SCALE TURBO JET ENGINECURRENTLY OPERATIONAL IN THE
DEPT.THRUST=19 lbs WEIGHT=3.1 lbs
1472 F exhaust 270 cc/min (9 oz.)
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WILLIAMS INTERNATIONALWR2 550 NEWTONS THRUST (120 LBS) 60,000 RPM 1 Kg/sPR=4.1 DIAM=274 MM 13 Kg mass
Used in CANADAIR C189 DRONE
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900 lbs thrust
1000 LBS THRUST
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Unusual engines forUAV/MAV applications ERICKSON MCC ENGINE (MIGRATING COMBUSTION CHAMBER)
ROTARY CYLINDER VALVE ENGINE
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ERICKSON MCC ENGINE (MIGRATING COMBUSTION CHAMBER)
DUAL MIGRATINGCOMBUSTION CHAMBERS
TWO STROKE CYCLE19.7 cm3 (1.2 cu.in)2.2 HP @ 7000 rpmCompression = 7.39Weight = 38.7 oz.1 oz./min
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Instant starting ability
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ROTARY CYLINDER VALVE ENGINE
SINGLE CYLINDER4-STROKE CYCLE20.02 cm3 (1.2 cu.in.) weight = 37.1 oz.Compression = 10.51.8 HP @ 5,800 rpm.85 oz/min
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ROTARY CYLINDER VALVE ENGINE
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500 HP CLASS
EXISTING TURBO-SHAFT
ENGINES
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P&WC PT6 500 HP
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GARRETT TPE 331 500 HP
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LYCOMING T-53 500 HP
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NAVAL POSTGRADUATE SCHOOLMONTEREY CA
GARTH HOBSON’S (PSU 1988)PROPULSION LAB
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QuickTime™ and aYUV420 codec decompressor
are needed to see this picture.
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QuickTime™ and aYUV420 codec decompressor
are needed to see this picture.
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Small Propulsion Systems
A 19 lbs thrust “small turbo-jet turbo-shaft gas turbine”
Unusual engines for UAV/MAV applications
Dr. Cengiz Camci
PENNSTATE1 8 5 5
