Aero Electric Aircraft Sun Flyer

Aero Electric Aircraft Corp One was working on a solar powered all-electric two-seater called the Sun Flyer, along with its development partners Bye Aerospace and German PC Aero.

AEAC started conducting research and development flights with a single-seat technology demonstrator at Centennial Airport (APA) near Denver. The concept airplane first flew out of Munich, Germany, in mid-July. Meanwhile, AEAC has been working on the design of a two-seat prototype of the Sun Flyer, which it hopes to fly sometime during 2015.

The technology demonstrator is equipped with a Geiger Engineering motor that generates 32 kW of power. Power is stored in several battery packs and the airplane is capable of flying for two hours without the supplement of solar energy. AEAC engineers estimate that the two-seat Sun Flyer will be able to fly for three to four hour in bright sunshine. Configuration plans for the Sun Flyer call for a side-by-side arrangement with a similar battery and electric motor setup as the technology demonstrator.

In addition to lower cost and cleaner flight, benefits of the solar-electric powered concept that AEAC’s CEO George Bye said have been confirmed with the technology demonstrator include low-noise, recharging on the ground and in flight and reduced maintenance due to fewer moving parts.

While the FAA still prohibits training flights with electric powered airplanes, the Sun Flyer is targeted to the training market. AEAC is collaborating on a complete training system with Redbird Flight Simulations and Spartan Aeronautical College. The company had not decided whether to pursue certification under Part 23 or the light sport aircraft rules.

AEG Helicopter

The A.E.G. helicopter designed by R. Schmidt was attached to the ground by a system of three tethering cables which helped to stabilise. R. Schmidt worked from about 1933 and this work was finalised in 1940 in the shape of a tethered electric helicopter for use as an aerial observation or support post for the army.
The helicopter had two two-blade rotors mounted co-axially, one being attached to the shaft and one to the shell of an electric motor. Three fixed arms were attached above the upper rotor, and these arms not only supported the cabin below but served as the cable attachment points for tethering. In the event of engine failure, the observer escaped by using a parachute blown into the air by a powder charge.
The three tethering cables were also used to feed power to the motor from a ground source via the control panel located in the launching and transporting truck. It was driven by electric motors of 50, later 100 and 200 horsepower and had a lift ranging from 450 to 1250 kilograms. Despite successful trials, the AEG helicopter does not appear to have been adopted for military use.

Engine: 1 x 200hp electric motor
Rotor diameter: 7.92m
Weight fully loaded: 1225kg
Ceiling: 1000m
Seats: 1