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Aircraft trim holds control surfaces (rudder, elevator, or ailerons) in a specific position, requiring less manual input from the pilot to maintain a desired flight attitude. Trim either moves entire control surfaces (like on a stabilator) or is installed as a separate trim tab (like on an elevator).
19 sty 2024 · Aircraft trim is an adjustable surface that applies a force on a control surface (like the elevator) to keep it in position. It works by redirecting airflow – just like the control surface itself. The force created by the redirected airflow forces the control surface into a specific position.
Aircraft must be loaded in way that ensures maximum allowable weights are not exceeded and the centre of gravity remains withing the prescribed limits. The process is documented by completing a Load and trim sheet.
18 maj 2022 · The tail section has two primary objectives: (1) to provide stability in the longitudinal (pitch) and directional (yaw) plane, and (2) to control the aircraft’s pitch and yaw response through movable control surfaces attached to the horizontal and vertical stabilizers.
28 gru 2017 · The trim is generally adjusted any time the aircraft transitions flight phase (climb to cruise, cruise to decent etc) or when the power setting is changed or periodically in cruise if the CG is greatly effected.
Trim Systems are considered to be a "secondary" flight control system. By definition, to "trim" an aircraft is to adjust the aerodynamic forces on the control surfaces so that the aircraft maintains the set attitude without any control input.
7 maj 2021 · What is the purpose of trim on an aircraft? Trim Systems are considered to be a “secondary” flight control system. By definition, to “trim” an aircraft is to adjust the aerodynamic forces on the control surfaces so that the aircraft maintains the set attitude without any control input.
