Only Fine Helis
50cc
Hey guys - 2 questions.
First, when a manufacturer recommends a certain minimum torque rating for a control surface on their plane, I'm assuming that they are talking about actual torque applied to the surface and not just rated servo torque?
For example, if they quote a required 200 oz/in of torque and you use a 200 oz/in rated servo with a 1 inch arm, you're good to go. However, if you need a 2 inch arm to get your desired throw, you now need a 400 oz/in servo to apply the same required 200oz/in to the control surface. So again, I'm assuming that they are discounting the needed servo arm length and are just talking about required torque to the control surface. Is this correct?
Secondly, I've been trying to find a formula or think about coming up with one to determine required torque to a control surface, but as you can imagine, it seems to be kind of tricky.
I know you would have to factor in the surface area of the control surface, the weight of the control surface, and the airspeed, but you would also have to consider the maximum g forces it would encounter to use as a factor into the weight.
Any thought?
Thanks!
First, when a manufacturer recommends a certain minimum torque rating for a control surface on their plane, I'm assuming that they are talking about actual torque applied to the surface and not just rated servo torque?
For example, if they quote a required 200 oz/in of torque and you use a 200 oz/in rated servo with a 1 inch arm, you're good to go. However, if you need a 2 inch arm to get your desired throw, you now need a 400 oz/in servo to apply the same required 200oz/in to the control surface. So again, I'm assuming that they are discounting the needed servo arm length and are just talking about required torque to the control surface. Is this correct?
Secondly, I've been trying to find a formula or think about coming up with one to determine required torque to a control surface, but as you can imagine, it seems to be kind of tricky.
I know you would have to factor in the surface area of the control surface, the weight of the control surface, and the airspeed, but you would also have to consider the maximum g forces it would encounter to use as a factor into the weight.
Any thought?
Thanks!