Functional description of the dive
of the ornithopter model EV8
When using a ball screw drive the direction of the motor rotation must change with every reversal of the wing flap direction. At first, it seems to be a little unfavourable. But if the reversal of rotation is largely affected by mechanical forces from the outside, losses of the motor are kept within limits.
The advantage of this drive technology lies in a relatively high degree of efficiency in the center part of the stroke.
Also at the previous EV-mechanism the drive motor was not very effective in the range of the final stroke position (no-load operation).
At the EV8, the reversal of motion of the rotating drive- and wing masses is mainly affected by mechanical and aerodynamically forces:
- in the lower final wing stroke position by the lift forces of the wing and
- in the upper final wing stroke position by the so-called
end position spring
While reversing, the electromechanical forces should support the reversal of motion only a little
Reversal of motion in the lower
final wing position
For illustrating the internal initial load the wing framework is shown in cantilever supine position on the marginal photo.
This initial load is important for the reversal of the motion in the lower final stroke position.
The reversal happens approximately like this:
(Numbering, Please look at the functional diagram)
The change-over of the motor happens when the wings reach their lower pre-final position during the downstroke. At first, due to the delay of time the speed controller works like a switch-off.
The lift at the wing is directed towards the still running downstroke. Thereby, the moved masses become slower. The lift force and the wing twisting become decreased, too.
If the downstroke comes to standstill in the lower final position, theoretically the wing twist equals the one in gliding flight. Also the lift force. Now it accelerates the wing upwards again.
Approximately at the same time the electrical run-up of the motor in the new rotation direction is getting started. But it still works without loading to a large extent. Via the ball screw drive the acceleration of the motor is mainly affected by the wing forces.
With increasing upstroke speed the lift forces continue to decrease. More and more the wing takes on the maximum upstroke twisting position. It is reached approximately in the lower pre-final position.
There, the motor has reached the full rotation speed. With its electromechanical force it now takes over the drive for the next upstroke of the wing and the tensioning of the compensating spring.
For the whole procedure the high efficiency of the ball screw drive is very important when converting a linear motion into a rotating motion.
The reversal of motion work - also of the rotating drive components - is primarily affected by the wing lift force.
Among the rotating drive components are the ball screw drive, timing belt pulleys and the motor (rotor). Because of its high rotation speed the angular momentum of the motor is considerable.
Also, you can support the reversal motion of the wing in the lower final
position by a
end position spring (as
at the EV7). This would be without importance
for generating thrust, but unfavourable for the lift.
Reversal of the motion in the upper final
Instead of the wing lift a so-called
end position spring
made of steel takes over the positive and negative acceleration
of the masses in this range. Else, the motion sequence works
analogically to aforesaid.
In the area of the upper final wing position there even during the upstroke decreasing lift always works against the reversal of motion. Hence, the end position spring also must overcome this force. Accordingly strong is its dimension (spring force max. 976 N).
If the energy recirculation of the wing mass momentum via the ball screw drive and the speed control in the accumulator are effective, the end position spring can later be designed frailer.
The flow of energy of the oscillating flapping wing mass is specified in the handbook, chapter 5.3.
To test the drive functions of interacting electronics and mechanism there was built a test rig.
The pendulum hanging downwards has the same mass moment of inertia as the two flapping wing halves. The aerodynamically forces of up- and downstroke are roughly reproduced by adjustable dashpots.
But some questions remain open till the practical testing of power flight.
To the Control of flight speed