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The JENTEC Gyrodrone
Un-Manned Autogyro
Dale Lawrence Jensen, P.E.
Executive Engineer, JENTEC
P.O. Box 694
Lawndale Ca. 90260
310-371-8469
Introduction
• There has been emphasis on developing
short take-off & landing un-manned aircraft..
• Extant aircraft designs;
Helicopters
Thrust diversion
• Over looked design
Autogyros
• Autogyros have advantages similar to
helicopters without some of the drawbacks.
Autogyro Advantages
• Simpler, safer, & less expensive
• Short take-off; vertical in 20 knot wind
• Inherent autonomous vertical landing
• Spectacular manuever capability
• Operation in restricted quarters
• Speed comparable to fixed wing design
• Always in auto-rotate mode
Kellett Autogyro
Amelia Earhart & Her Autogyro
Bensen Autogyro
Groen Autogyro
Mission Requirements
• Pre-programmed flight pattern
• 1 pound camera payload
• Short take-off & landing
• Operate from shipboard & un-improved
areas
• Operate in restricted space
Design Requirements
• Maximum speed 100 m.p.h.
• Cruise speed 80 m.p.h.
• Loiter 20 m.p.h.
• Service ceiling 12,000 feet
• Range15 miles
• Endurance one half hour
• Weight 12 - 13 pounds
• Rotor loading, 3.5 pounds per square foot
• Manuever load factor, plus 2.5 to minus 1
• Command & control through radio link
Gyrodrone Port Side Elevation
Weight Estimate
Autogyro Comparison Parameter Gyrodrone Bensen Kellett Pitcairn
Weight, lbs. 15 425 2205 3300
Rotor area, sq. ft. 2.5 12 60 112
Horse power 0.75 72 225 422
Speed, max., m.p.h. 100 85 128 140
Speed, cruise, m.p.h. 80 60 103 115
Speed, min., m.p.h. 15 23 17 25
Rotor load, lbs./ sq. ft. 6 36 38 29
Power load, lb. / h.p, 20 6 10 8
Rotor span, feet 4 20 40 50
Rotor chord, inches 5 7 12 18
Number of blades 4 2 3 3
Fuel, gal. (2 tanks) 0.86 6 30 66
Fuel, lbs. 0.29 36 180 396
Endurance, hours 0.5 1.7 2 3.25
Aerodynamics
• Aspect Ratio 8
• Chord 5 inches
• Span 4 feet
• Drag, CDo, 0.13
• Lift curve slope, CLa, 0.098
• Rotor lift area, 6.67 feet
Parasite Drag
Eq.flat Plate vs. Wetted Area
0.007 0.005
0.1
1
10 100
Wetted Area, sq.ft.
Eq
. F
lat
Pla
te, sq
.ft.
Wetted Area, 17.98 square feet
Equivalent flat plate area, 0.13
Polar Plot, CD versus CL
Power vesus Velocity
Comparison of Drag versus Speed
Weight versus Rotor Area
Autonomous Gudance, Navigation,
& Flight Control
Schematic Diagram
Autonomous Navigation, Guidance, & Control
Conclusions
• Autonomously operating gyrodrone has
unique capability
• Less complex, safer, & less expensive
than helicopter
• Operate from unprepared areas,
shipboard, & manuever restricted zones
• Employable in hazardous situations
without exposure of personnel to risk
Status
• Prototype Under Construction
Planking needs to be completed
Rotor to provide lift remains to be
fabricated
• Test flying to follow
• Prototype wind tunnel testing to follow
• Questions?
Recommendation
• Build wind tunnel model for testing
• Building prototype for demonstration
• Thank you for listening
• Questions?
HG 1700 Inertial Measuring Unit
Development Schedule
Development Organization