1. Small Propulsion Systems  A 19 lbs thrust “small turbo-jet turbo-shaft gas turbine”  Unusual engines for UAV/MAV applications Dr. Cengiz Camci

2. 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

3. High specific powerFuel efficient Light weightSilent Smooth runningReliable Easy to maintainLow production cost UAV PROPULSION SYSTEM

6. A “small scale” turbo-jet turbo-shaft gas turbine design course

7. Aero-thermo-mechanical Design of Small Gas Turbine Systems for Unmanned-Aerial Vehicle (UAV) and Environmental Applications (AERSP 597/497-K) A three credit design course by: Dr. Cengiz Camci 153-E Hammond Building 814 865 9871

8. 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)

9. 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.

10. 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.

11. SMALL SCALE TURBO JET ENGINE CURRENTLY OPERATIONAL IN THE DEPT. THRUST=19 lbs WEIGHT=3.1 lbs 1472 F exhaust 270 cc/min (9 oz.)

18. WILLIAMS INTERNATIONAL WR2 550 NEWTONS THRUST (120 LBS) 60,000 RPM 1 Kg/s PR=4.1 DIAM=274 MM 13 Kg mass Used in CANADAIR C189 DRONE

19. 900 lbs thrust 1000 LBS THRUST

20. Unusual engines for UAV/MAV applications ERICKSON MCC ENGINE (MIGRATING COMBUSTION CHAMBER) ROTARY CYLINDER VALVE ENGINE

21. ERICKSON MCC ENGINE (MIGRATING COMBUSTION CHAMBER) DUAL MIGRATING COMBUSTION CHAMBERS TWO STROKE CYCLE 19.7 cm3 (1.2 cu.in) 2.2 HP @ 7000 rpm Compression = 7.39 Weight = 38.7 oz. 1 oz./min

22. Instant starting ability

29. ROTARY CYLINDER VALVE ENGINE SINGLE CYLINDER 4-STROKE CYCLE 20.02 cm3 (1.2 cu.in.) weight = 37.1 oz. Compression = 10.5 1.8 HP @ 5,800 rpmHP @ 5,800.85 oz/min

30. ROTARY CYLINDER VALVE ENGINE

33. 500 HP CLASS EXISTING TURBO-SHAFT ENGINES

34. P&WC PT6 500 HP

35. GARRETT TPE 331 500 HP

36. LYCOMING T-53 500 HP

38. NAVAL POSTGRADUATE SCHOOL MONTEREY CA GARTH HOBSON’S (PSU 1988) PROPULSION LAB

43. Small Propulsion Systems  A 19 lbs thrust “small turbo-jet turbo-shaft gas turbine”  Unusual engines for UAV/MAV applications Dr. Cengiz Camci