I had a question about how I did my electric trim, so though I’d post the answer/pictures to make use of the new forum.
My key design parameter was to preclude welding or other mods to the frame.
I have an electric servo driving a pushrod to the stock-standard trim horn in the tail cone. I have no additional welding, you can see here how I attached the servo with a bolted arrangement:
20120916_105554.jpg
You will see I kept a service loop in the wire, and installed a plug which mounts on a bracket to avoid vibration loosening of the terminals. This is to allow removal of the servo if necessary for maintenance.
You can also see the aft end of my baggage tube (very heavy design, to be redone in carbon fibre), and the profiled horisontal stabiliser rib.
In this picture, you can see the inspection ports I installed to allow generous access to the tail area and trim arrangement - I have been endlessly thankful for these since covering the fuselage.
20130307_111404.jpg
The end of the pushrod can be seen here, note the bolts are overlength - temporary install only:
20120916_105853.jpg
This servo is controlled by dual stick grip buttons, which activates a power relay, drawing directly off the master bus. All RAC components.
I am going to add a DPDT safety switch which open circuits the stick grip switches and transfers control to a manual trim switch in the panel. This is because an earth fault in either stick grip or any wiring results in trim runaway. The safety switch provides n-1 redundancy in the control circuits in the event.
Edit: Upon flight testing the system, we found trim runaway was not uncontrollable. It made for more work at 100kts + but slowing the aircraft would obviously allow for a safe precautionary landing.
Another edit: The question of trim travel comes up a lot, here are some photos of the trim at both limits.
NOTE these photos are taken with the pushrod on the lowest hole on the trim tab, which maximises servo action but minimises trim tab travel. In practice I've moved the pushrod to the top hole for the opposite effect, minimum servo action and maximum tab travel.
20120916_105619.jpg
20120916_105714.jpg
My key design parameter was to preclude welding or other mods to the frame.
I have an electric servo driving a pushrod to the stock-standard trim horn in the tail cone. I have no additional welding, you can see here how I attached the servo with a bolted arrangement:
20120916_105554.jpg
You will see I kept a service loop in the wire, and installed a plug which mounts on a bracket to avoid vibration loosening of the terminals. This is to allow removal of the servo if necessary for maintenance.
You can also see the aft end of my baggage tube (very heavy design, to be redone in carbon fibre), and the profiled horisontal stabiliser rib.
In this picture, you can see the inspection ports I installed to allow generous access to the tail area and trim arrangement - I have been endlessly thankful for these since covering the fuselage.
20130307_111404.jpg
The end of the pushrod can be seen here, note the bolts are overlength - temporary install only:
20120916_105853.jpg
This servo is controlled by dual stick grip buttons, which activates a power relay, drawing directly off the master bus. All RAC components.
I am going to add a DPDT safety switch which open circuits the stick grip switches and transfers control to a manual trim switch in the panel. This is because an earth fault in either stick grip or any wiring results in trim runaway. The safety switch provides n-1 redundancy in the control circuits in the event.
Edit: Upon flight testing the system, we found trim runaway was not uncontrollable. It made for more work at 100kts + but slowing the aircraft would obviously allow for a safe precautionary landing.
Another edit: The question of trim travel comes up a lot, here are some photos of the trim at both limits.
NOTE these photos are taken with the pushrod on the lowest hole on the trim tab, which maximises servo action but minimises trim tab travel. In practice I've moved the pushrod to the top hole for the opposite effect, minimum servo action and maximum tab travel.
20120916_105619.jpg
20120916_105714.jpg
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