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Future Aircraft System Division Korea Aerospace Research Institute
KARI Proprietary Information : The information contained in this document, without the permission of KARI, shall not be used or disclosed for any purpose other than KARI’s UAV Development.
Tilt-rotor UAV System to Monitor Illegal Fishing
2015. 12. 09.
Youngshin Kang
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Contents
Introduction Tilt-rotor Family of KARI Merit of Tilt-rotor Innovative Concept of TR-60 WE
R&D and Operation Plan
R&D Roadmap Development for Civil Operation
Conclusions
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Tilt-Rotor Family of KARI
TR-100 (Smart UAV) TR-60
TR-40 TR-60 TR-100 Smart UAV
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Merit of Tilt-Rotor
Comparison to Helicopter Can Fly Faster, Higher, and Farther even More Quietly
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Concept of TR-60 WE
TR-60 + Wing Extension
TR-60 WE
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TR-60 vs TR-60 WE
TR60 TR60 WE MTOW (kg) 200 same Payload (kg) 20 same Powerplant 55hp Rotary same Overall Length (m) 3.0 same Wing Span (m) 3.0 4.8 Wing Area (m2) 1.5 2.0 Rotor Radius (m) 1.1 same Blade Twist (deg) 29.0 same Disk Loading (kg/m2) 52.6 same Max Speed (km/h) 240.0 220 Loitering Speed (km/h) 160.0 140.0 Max Altitude (km) 4.0 same Endurance (hrs) 5.0 6.0 Fuselage Upswept aft fuselage same Landing Gear 3 pts fixed tricycle same
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Flow Visualization
FLUENT Analysis
-8 -6 -4 -2 0 2 4 6 8 10 12 14 16 18-0.5
0.0
0.5
1.0
1.5
2.0
2.5
TR60 TR60 Subwing
CL
AOA (deg)
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Flight Control System
Upgrade of Flight Control Hardware
Avionics Bay of TR-60 Avionics Bay of TR-60 WE
• Hardware come from TR-100 • Communication Rage < 5km • GPS/INS
• Optimized for TR-60 Series • Communication Rage < 50km (~ 200km) • Relative GPS/INS for Deck Operation
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Flight Test Results
Flight Test Results
-1500 -1000 -500 0 500
-800
-600
-400
-200
0
200
400
600
800
1000
1200
East
Nor
th
OXTOLD
Wind Estimation - 2D
Track2DW2DWF
Preprogram on a map Trajectory and wind estimation
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R&D Roadmap
Development Plan Personnel Air Vehicle
MILITARY
CIVIL
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Development for Operation
Monitor Illegal Fishing
200km Identification of
Illegal Boats
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Development for Operation
Monitor Illegal Fishing
AIS+V⋅PASS
Electronic Mapping Display
Data Link Interface
Development
Integrated Small/Light Weight
Identification System
Improved Video Display
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Accomplishments TR-60 WE was successfully developed
To increase endurance in airplane mode World 1st design concept for performance enhancement of tilt-rotor
Series of Tilt-rotor UAV showed the possibility of Commercial Operation
TR-40 TR-100 TR-60 and TR-60WE
Next Plans
Co-Development of production type TR-6X with Korean Air TR-80 will be considered for another Production Type Initial operation of TR-60 to monitor illegal fishing
Conclusion
![NASA - [Aerospace History 17] - The History of the XV-15 Tilt Rotor Research Aircraft, From Conce.pdf](https://img.pdfslide.net/doc/110x75/55cf8d1e5503462b139235cc/nasa-aerospace-history-17-the-history-of-the-xv-15-tilt-rotor-research.jpg)
