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EZSolarGlider4

von Serge Encaoua
5

My previous solar gliders (EZSolarGlider 1 through 3) were designed with the solar cells inside the wing. I wanted to improve on that design, with the goal of both simplifying construction and improving performance, which led to the development of the EZSolarGlider4.


Design

It is a hybrid design: the upper surface consists of a 3-mm sheet of Depron, to which the solar cells will be attached and wired. The cells are not glued, but held in place by laminating film; this part is assembled flat.

This sheet then serves as the upper surface for a traditional construction made of balsa wood and carbon fiber reinforcements. The solar cells support the curvature of the upper surface.

The rest of the construction is standard: a balsa/carbon tube fuselage, and tail surfaces made of 6 mm Depron that are sanded and covered with laminating film.

There are many advantages to this type of construction:

  • ease of construction and wiring of the cell structures
  • good torsional stiffness of the wing
  • low weight
  • no obstruction of the cells by ribs or the leading edge.
  • Cell density: 8 full cells per meter of wingspan
  • maintains the wing’s upper surface profile, resulting in excellent gliding performance.
  • A lifting tailplane, which allows the center of gravity to be moved aft while maintaining a “nose” of reasonable length.

The production cost is less than €100, including the glider, motor, propeller, speed controller, and airframe (excluding servos and receiver).


Construction

The wings

Start by cutting out the sheet of Depron that will hold the cells, making sure to leave openings for the solder tape on the inner side. Attach the cells to the Depron using 43-micron laminating film. →


Key Features
Wingspan:1.10 m
Wing area:19 dm²
Weight:280 g
Wing loading:15 g/dm²
Motor:Hacker 10
, 6 A ESC
Propeller:5 × 3
Airfoil:flat
Servos:4 (elevator, rudder, and 2 for the ailerons).
Receiver:4-channel
mini receiver Battery capacity: 1S-200 mAh


We can then proceed with the welding operations. At this stage, the assembly should be electrically tested (voltage = 4 volts). The lower part of the wing has a traditional structure. Cut out the ribs and assemble the wing by installing the carbon stringers and the leading edge made of carbon rod.

Next, the Depron sheet is glued to the wing structure with the spars already in place. The spars support the wing’s curvature. Finally, the leading edge is sanded. The Depron is glued with cyanoacrylate and reinforced with laminating film. Next, the Depron winglets are installed.

The underside is covered with lightweight heat-shrink film or laminating film.



The ailerons are made of 6 mm Depron, sanded and covered with laminating film to stiffen them.

You can either mount a servo in the center of the wing (and cut a hole in the fuselage for the control lines) or mount two servos inside the wing. The control rods are made of carbon fiber and covered with heat-shrink tubing at the joints. Be sure to maintain the ailerons’ downward angle (to function as flaps).


The fuselage

Start by building the front section out of balsa and CTP, then attach the carbon tube, making sure it’s properly aligned.

The elevator and rudder control lines are made of Dacron thread and pass through the rear opening of the carbon tube. They are bent slightly to reach the control horns, but this isn’t a problem because the thread slides smoothly without friction.

The vertical tail is made of sanded Depron and covered with laminating film.

The horizontal tailplane is constructed in the same way using a flat profile. Two carbon rods serve as spars.


Electrical Installation

The motor is controlled by a 6 A ESC, which powers the motor directly. The receiver is powered separately by a 1S battery for safety.


Settings and Flight

For initial testing, the solar generator can be replaced with a 2S 300 mAh battery. Make sure the center of gravity is correctly positioned; to do this, adjust the position of the receiver battery.

Thanks to the density of the cells, the glider has a power-to-weight ratio of 94 W/kg under maximum lighting conditions, which is very good.


Control Surface Travel:

Depth: +/-25 degrees

Yaw: +/-30 degrees

Aileron: +15 degrees down, -25 degrees up (differential obtained directly from the yoke tilt)

The aircraft is fairly responsive to controls.

In practice, conditions for solar-powered flight are met as early as May in the Paris region, from 10:30 a.m. to 3:30 p.m. The season runs from May through September.

Light clouds or slightly overcast skies also allow for flying.

The first flight took place in mid-May around 11:30 a.m. in the Paris region, in full sunlight.

The climb rate is good. It climbs quickly and is a pleasure to fly. The controls are responsive.

Then a test was conducted in moderate wind (10–15 km/h), with the sun obscured by clouds: the climb remains easy, and with the engine off, the glide ratio proves to be very good—it easily covers the entire field.

The flight is as slow as you could wish for; it catches even the slightest thermal.

You can even attempt some basic aerobatics, as the wing is sturdy.





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