The GH3536 alloy is an important structural material for the high-temperature components of aeroengines owing to its excellent high-temperature oxidation and corrosion resistances and good performance during cold and hot forming and welding. The traditional manufacturing method of GH3536 high-temperature components has the disadvantages of long production cycle, complicated procedures, and low yield. Therefore, its production applications are limited. This study provides a comprehensive introduction to the research progress of the laser powder bed fusion of the GH3536 alloy and clarifies its structure and strengthening mechanism. Meanwhile, relevant research results were systematically investigated, conventional methods were compared, and the preparation of GH3536 alloy by laser powder bed technology is comprehensively discussed from the aspects of technical principle, microstructure, and mechanical properties. Furthermore, the composite technology of additive and traditional manufacturing is investigated. Finally, the future application and development trends of the GH3536 alloy prepared by laser powder bed technology are discussed.