TotalBeginner
5th Mar 2005, 11:58
Can anyone help me out
I am trying to understand exactly how the stabilizer is used on modern airliners to keep the aircraft in trim.
I understand the concept of trim tabs used on light aircraft to remove control forces, but moving the whole stabilizer will surely have no affect on the neutral position of the stick if the evevators are connected to it?
e.g. If the control column is left in the neutral position, but the stab is moved up or down. Will the elevator remain flush with the stabilizer or will it remain flush with the longitudinal axis of the aircraft???
Does Stab Trim feel the same as elevator trim in light aircraft? i.e If the control column is held back to maintain a given attitude, does moving the stab remove the aerodynamic force, or does the control column then have to be released back to the neutral position once the aircraft is in trim???
I am trying to understand exactly how the stabilizer is used on modern airliners to keep the aircraft in trim.
I understand the concept of trim tabs used on light aircraft to remove control forces, but moving the whole stabilizer will surely have no affect on the neutral position of the stick if the evevators are connected to it?
e.g. If the control column is left in the neutral position, but the stab is moved up or down. Will the elevator remain flush with the stabilizer or will it remain flush with the longitudinal axis of the aircraft???
Does Stab Trim feel the same as elevator trim in light aircraft? i.e If the control column is held back to maintain a given attitude, does moving the stab remove the aerodynamic force, or does the control column then have to be released back to the neutral position once the aircraft is in trim???