Trim System

I didn’t have much time this week, but I was able to get the trim system working correctly.

Using the laptop and a long Ethernet cable I was able to use the VPX configurator tool on my laptop to send power to the trim motors. I was pleasantly surprised that both the roll and pitch servos worked correctly. I carefully verified that the orientation was correct. It would be easy to reverse either one. For example, the elevator trim tab moves up and down just like the elevator, but it has the opposite effect from the elevator itself. Pitching “up” causes the elevator trailing edge to move up. Trimming “up” causes the elevator trim tab to move down, not up. It moves opposite the elevator, providing a force that moves the elevator to change the aircraft’s pitch.

After confirming the motors were working, I was able to set the correct max, min, and midpoint settings for both servos.

I then worked on mounting the aileron trim brackets on the right wing aileron pushrod. These connect the springs from the servo control arm to the pushrod, actuating the aileron.

Aileron trim servo. The servo mounts onto the access panel at this point. Springs will attach to the holes in the end of the arm, and extend to the brackets on the pushrod.
Diagram of the aileron trim system showing the springs and how they connect to the pushrod and servo arm
Using the laptop to run the trim motors and to set the trim limit parameters
VPX config tool. The whole electrical system can be configured and activated from the laptop. The blue Ethernet cable is a 50 foot cable that plugs into the VPX box behind the panel
Due to interference between the springs and the pushrod, I bent the servo arm to gain some clearance
Springs attached to the servo arm.
One last picture before closing this up. Note, the d-sub connector is safety wired together