The invention discloses acrylate coating for aircraft propeller blades. The acrylate coating comprises the following raw materials in parts by weight: 70-80 parts of a main material, 1-4 parts of a core-shell toughening agent, 1-4 parts of a vermiculite powder, 2-4 parts of fly ash, 1-4 parts of graphene, 1-4 parts of calcined kaolin, 2-4 parts of active carbon, 1-3 parts of nonylphenol polyoxyethylene ether, 2-8 parts of vinyl triamine, 1-2 parts of a copper antifoulant, 1-2 parts of a thixotropic agent, 1-2 parts of a dispersing agent, 1-2 parts of a defoaming agent and 50-120 parts of deionized water, wherein the core-shell toughening agent is prepared by the following technology: mixing butyl acrylate, hydroxyethyl acrylate, sodium lauryl sulphate, ammonium persulfate and water, and heating while stirring to obtain a core layer emulsion; mixing vinyl chloride, hydroxypropyl acrylate, polyvinyl alcohol, benzoyl peroxide and water, and heating while stirring to obtain a shell layer emulsion; mixing the core layer emulsion and the shell layer emulsion, heating, dropwise adding an aqueous formaldehyde solution, continuously stirring after dropwise addition, cooling, and filtering to obtain the core-shell toughening agent.