Aileron
For the band with a similar name, see The Ailerons
Ailerons are hinged control surfaces attached to the trailing edge of the wing of a fixed-wing aircraft. They are used to control the aircraft in roll. The two ailerons are interconnected so that one goes down when the other goes up: the downgoing aileron increases the lift on its wing while the upgoing aileron reduces the lift on the other wing, producing a rolling moment about the aircraft's longitudinal axis. The word aileron is French for "little wing."
An unwanted side-effect of aileron operation is adverse yaw — a yawing moment in the opposite direction to the turn generated by the ailerons. In other words, using the ailerons to roll an aircraft to the right would produce a yawing motion to the left. It is caused by an increase in induced drag due to the greater effective camber of the wing with a downward-deflected aileron, and the opposite effect on the other wing. Modern aileron systems have minimal adverse yaw, such that it is barely noticeable in most turns. This may be accomplished by the use of differential ailerons, which have been rigged such that the downgoing aileron deflects less than the upward-moving one. Frise ailerons achieve the same effect by protruding beneath the wing of an upward deflected aileron, increasing drag on that side. Ailerons may also use a combination of these methods.
Adverse yaw is also caused by the wing on the outside of the turn traveling faster than the inside wing and thus having more lift and drag. Once the desired angle of bank (degree of rotation on the longitudinal axis) is obtained, the pilot uses opposite aileron to prevent the aircraft from continuing to roll due to this increased lift. This minor opposite use of the control must be maintained throughout the turn. The pilot also uses a slight amount of rudder in the same direction as the turn to counteract adverse yaw and to produce a "coordinated" turn where the fuselage is parallel to the flight path. A simple gauge on the instrument panel called the inclinometer, also known as "the ball", indicates when this coordination is achieved.
Modern airliners tend to have a second set of inboard ailerons much closer to the fuselage[citation needed], which are used at high speeds. If the wings swept and the aircraft enters a stall, the ailerons toward the fuselage will still be able to function as the stall will proceed from the tips of the wings to the body. In plane wings, the stall develops the other way so the ailerons are placed towards the tips of the wings. Large jet aircraft often have ailerons towards the tips of the wings to increase the moment of the aircraft so less force is required to roll the aircraft. Some aircraft use spoilers to achieve the same effect as ailerons.
Although the device first appeared on a monoplane, built by New Zealand inventor Richard Pearse in 1902, the first aircraft that flew using an aileron was 14 Bis by Santos Dumont.
It was later developed independently by the Aerial Experiment Association, headed by Alexander Graham Bell, and by Robert Esnault-Pelterie, a French aircraft builder. Ailerons superseded the earlier wing warping technique, developed by the Wright Brothers.
Another control surface that combines an aileron and flap is called a flaperon. A single surface on each wing serves both purposes: used as an aileron, the flaperons left and right are actuated differentially; when used as a flap, both flaperons are actuated downwards. As an example of an aircraft using flaperons, see this RJ.03 IBIS experimental aircraft. Please note that when a flaperon is actuated downwards (i.e. used as a flap) there is enough freedom of movement left to be able to still use the aileron function.
See also
External links
- NASA Glenn Research Center aileron article with Java demo and more pictures