To improve the wear resistance of aluminum alloy frictional parts, Ti B_2 particles reinforced Ni-base alloy composite coatings were prepared on aluminum alloy 7005 by laser cladding. The microstructure and tribological properties of the composite coatings were investigated. The results show that the composite coating contains the phases of Ni Al, Ni_3Al, Al_3Ni_2, TiB_2, TiB, TiC, CrB, and Cr_(23)C_6.Its microhardness is HV_(0.5)855.8, which is 15.4 % higher than that of the Ni-base alloy coating and is 6.7 times as high as that of the aluminum alloy. The friction coefficients of the composite coatings are reduced by 6.8 %–21.6 % and 13.2 %–32.4 % compared with those of the Ni-base alloy coatings and the aluminum alloys, while the wear losses are 27.4 %–43.2 % less than those of the Ni-base alloy coatings and are only 16.5 %–32.7 % of those of the aluminum alloys at different loads. At the light loads ranging from 3 to 6 N, the calculated maximum contact stress is smaller than the elastic limit contact stress. The wear mechanism of the composite coatings is micro-cutting wear, but changes into multi-plastic deformation wear at 9 N due to the higher calculated maximum contact stress than the elastic limit contact stress. As the loads increase to 12 N, the calculated flash temperature rises to 332.1 °C.The composite coating experiences multi-plastic deformation wear, micro-brittle fracture wear, and oxidative wear. To improve the wear resistance of aluminum alloy frictional parts, Ti B_2 particles reinforced Ni-base alloy composite coatings were prepared on aluminum alloy 7005 by laser cladding. The microstructure and tribological properties of the composite coatings were investigated. The results show that the composite coating contains the phases of NiAl, Ni_3Al, Al_3Ni_2, TiB_2, TiB, TiC, CrB, and Cr_ (23) C_6.Its microhardness is HV_ (0.5) 855.8, which is 15.4% higher than that of the Ni-base alloy coating and The 6.7 times as high as that of the aluminum alloy. The friction coefficients of the composite coatings are reduced by 6.8% -21.6% and 13.2% -32.4% compared with those of the Ni-base alloy coatings and the aluminum alloys, while the wear losses are 27.4% -43.2% less than those of the Ni-base alloy coatings and are only 16.5% -32.7% of those of the aluminum alloys at different loads. At the light loads ranging from 3 to 6 N, the calculated maximum contact stress is smaller than the elastic limit contact stress. The wear mechanism of the composite coatings is micro-cutting wear, but changes into multi-plastic deformation wear at 9 N due to the higher calculated maximum contact stress than the elastic limit contact stress. 12 N, the calculated flash temperature rises to 332.1 ° C. The composite coating experiences multi-plastic deformation wear, micro-brittle fracture wear, and oxidative wear.