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EagleR&D-Helicycle

EagleR&D-Helicycle


Eagle R & D Mission Statement Eagle R & D will design and produce a new generation Rotary Wing Aircraft which will provide more utility at less cost than any previous helicopter. Our goal in essence, is to create a single place quality equivalent of the Robinson R-22 for 1/5 the price. Good ha


PERFORMANCE:( Speed & Altitude ) The HELICYCLE in it's normal configuration is designed to cruise along side the industry standard R-22. Landings and take offs at above 9000 ft. are possible because of a 7.5/1 power to weight ratio. The same as the Hughes 500. FLIGHT STABILITY: ( Wind & Gust ) Aircraft stability is always challenged by adverse weather conditions. It is normally assumed that lighter aircraft will be further affected. The HELICYCLE at one half the weight of the R-22 is capable of being operated in the same weather conditions as the R-22, with no appreciable increase in pilot work load over that of the R-22. HANDLING QUALITIES The HELICYCLE has numerous design features which improve it's handling qualities. These include: 1. A fully harmonized rotor. 2. A modulated collective system. 3. Very low 2-per-rev vibration level due to elastomeric thrust bearings. 4. Generous flapping angle for low "G" and slope landing conditions. 5. Control friction devices. 6. Electronic throttle control.


EASE OF OPERATION : ( Leaning to fly ) The cyclic control in the HELICYCLE accurately models the feel of the R-22. With a high degree of control power, it provides a natural transition for the R-22 qualified student pilot. Low 2-per-rev vibration gives it a solid feel which is confidence inspiring during the transition. The modulated collective, automatic RPM control and R-22 equivalent foot pedal feel and response also help reduce that sweaty palm feeling on the first lift off. Preparing for autorotations is facilitated by practicing confidence inspiring throttle chops and quick stops which clearly show the lift and energy available in this rotor with the power off.


Helicycle規格與性能

 Modified Solar T62 turbine

 160 derated to 90 hp

 Single Seat

 220 lbs max

 Gross Weight

 850 lbs

 Empty Weight

 500 lbs

 Fuel Capacity (Note: Optional +5 only for 180lb & Less pilot weight)

 21 (16 + 5 reserve) US gal

 Range with reserve

 160 miles

 Rate of Climb

 900 fpm

 Hover IGE

 9,500 ft

 Service ceiling

 11,000 ft

 Normal cruise with doors

 95 mph

 Max airspeed at sea level @ standard conditions

 110 mph