the subject of the invention is a tire is intended for use in aircraft wheels. on the side surface of the tyre (1) are peripherally arranged in the form of wzgu00f3rku00f3w steering pad (2), which is shaped like a cream bars.the shape of this follows from the fact that the foothills (2) has one side (3) gently out and be comfortable along the perimeter of the surface of the sidewall of the tyre (1) and (2) has the shape of a cross section wzgu00f3rku00f3w segment wheels, with the section of the wheel is arc surface sidewall (1). the second protuberance (2) constitutes a steep slope wall (4), which is located in the place where the foothills (2) have the greatest height.such a wzgu00f3rku00f3w (2) implies that during the descent to landing, when the landing gear is released, the air leads to assign turnover kou0142om plane. the foothills (2) act as a wind turbine blades saveniusa and wheel turns under the influence of air movement in her direction.the direction of this follows from the fact that the air pressing on steep walls (4), which during the landing at the bottom of the tyre and are are facing wall (4) in the direction of landing. the air flows along the gentle slopes (3) wzgu00f3rku00f3w (2), which are at the top of the tyre during the landing.
展开▼
