| 摘要 |
PURPOSE:To improve retainability of the titled component being used and removability at the time of recorrection, by a method wherein a weight balance correction component for an aeroplane is constituted of an upper layer material made of a rubber composite of high specific gravity and a lower layer material made of a rubber composite of low tensile strength, and the lower layer material is made to adhere to the inner surface of the tire. CONSTITUTION:An upper layer material 6 having thickness of 2-10mm. is formed of a rubber composite having specific gravity of more than 1.5, a lower layer material 7 having thickness of 0.5-1.5mm. is formed of a rubber composite having tensile strength of 1-100kg/cm<2>, and a paste layer 8, such as an adhesive for rubber is formed. This component material 11 mounted on an inner plate layer 1 of an inner surface of a light weight part of a tire 10 placed on a cradle 9 by making the paste layer of the material 11 down is pressed and heated by a hot plate 12 for adherence. With this constitution, retainability of the component material being used is improved and it is easily removed off at the lower layer 7 part whose tensile strength is low. |
