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直八型多用直升机旋翼刹车材料的研制

A STUDY ON BRAKE MATERIALS FOR THE ROTATING WINGS OF Z-8 HELICOPTER

  • 摘要: 阐述了直八型直升机旋翼刹车材料的研究工艺;探讨了非金属基、铜基和铁基在相同条件下的摩擦性能;研究了润滑组元MoS_2、BN以及摩擦组元Sic对铁基摩擦材料性能的影响,并分析了其影响机理;指出非金属成分含量可以控制摩擦材料制动过程中摩擦力矩的峰比值,提高力矩的稳定性;同时也指出细片状珠光体组织的铁基材料耐磨性最好,并研制成功国内首次应用于直升机旋翼刹车装置的9-9铁基摩擦材料。

     

    Abstract: The technological process of brake materials for the rotating wings of z-8 helicopter was studied in the research,Frictional properties of nonmetal-base, coper-bake and iron-base brake materials were compared under same test conditions. The effects of lubricating components, MoS_2 and BN, and frictional materials of iron-base were discussed,The mechanism of this effects was also explained. The amount of nonmetal components may control the peak ratio of moment of frictional force in the braking process by friction materials. It may also increase the stability of moment.The iron-base materials with fine lamellar pearlite structure showed the best frictional properties. A "9-9 iron-base material" was successfully manufactured and firstly used in brake system of z-8 helicopter.

     

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