There has been a lot of discussion on the trim system of the 4 place and a little bit discussion of the trim system on the patrol. People talk about how sensitive the trim is and far aft CG loading the pitch becomes a bit sensitive. There has also been discussion about how the trim becomes very sensitive at higher speeds. Most of this information has been around the 4 place.
I have a few questions for you Patrol flyers.
1) How much is the trim lever typically moved from takeoff to cruise and then cruise to landing?
2) How much trim change is needed for power changes?
3) At cruise speed how sensitive is the trim lever?
I am in have been considering building an electric trim for the patrol but I am not willing to give up the manual trim. I agree with Mark Goldberg that the aircraft would be a real handful and respect his opinion that it might be uncontrollable with a run away trim situation if you had not manual override. I prototyped up an electronic trim system that also allowed me to use the manual trim lever. I am using a Dynon autopilot servo as the donor power control unit. I am attaching this to the trim cables in the ceiling behind the baggage compartment. The Dynon servo was the choice because it uses a stepper motor and has a fairly low power off idle resistance so that I can still use the manual trim lever when the power to the servo is off. As an added advantage the idle resistance is not zero so it adds a little drag to the system so the trim will not slip when the servo is off. Also with stepper motors and good stepper motor controllers like the one I am using (TC78H670FTG) I can control both the torque and the speed from very very slow to fairly fast. I can also still keep the torque so that I can always override it manually if I have to. I ripped out the electronics and replacing it with my own circuit board. The circuit board has two trim switch inputs. One for the trim on the stick and one from an auto trim on an auto pilot. There is also a RS-232 input for GPS ground speed so I can scale the speed of the trim to the airspeed (shower at cruise and faster at slow air speeds). It also allows the safety mechanism of maximum of 3 seconds of switch activation to help catch a runaway trim situation. It worked well on the bench with proto boards and I should get my custom bare circuit board that replaces the Dynon board Friday. I will post pictures when I get the board populated.
I have a few questions for you Patrol flyers.
1) How much is the trim lever typically moved from takeoff to cruise and then cruise to landing?
2) How much trim change is needed for power changes?
3) At cruise speed how sensitive is the trim lever?
I am in have been considering building an electric trim for the patrol but I am not willing to give up the manual trim. I agree with Mark Goldberg that the aircraft would be a real handful and respect his opinion that it might be uncontrollable with a run away trim situation if you had not manual override. I prototyped up an electronic trim system that also allowed me to use the manual trim lever. I am using a Dynon autopilot servo as the donor power control unit. I am attaching this to the trim cables in the ceiling behind the baggage compartment. The Dynon servo was the choice because it uses a stepper motor and has a fairly low power off idle resistance so that I can still use the manual trim lever when the power to the servo is off. As an added advantage the idle resistance is not zero so it adds a little drag to the system so the trim will not slip when the servo is off. Also with stepper motors and good stepper motor controllers like the one I am using (TC78H670FTG) I can control both the torque and the speed from very very slow to fairly fast. I can also still keep the torque so that I can always override it manually if I have to. I ripped out the electronics and replacing it with my own circuit board. The circuit board has two trim switch inputs. One for the trim on the stick and one from an auto trim on an auto pilot. There is also a RS-232 input for GPS ground speed so I can scale the speed of the trim to the airspeed (shower at cruise and faster at slow air speeds). It also allows the safety mechanism of maximum of 3 seconds of switch activation to help catch a runaway trim situation. It worked well on the bench with proto boards and I should get my custom bare circuit board that replaces the Dynon board Friday. I will post pictures when I get the board populated.
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