发明名称 BLADE FOR TURBOMACHINE AND METHOD OF SAID BLADE MAKING
摘要 FIELD: machine building.SUBSTANCE: turbomachine blade from composite material with matrix and reinforcement, containing mesh includes front and rear edges, as well as backet and back surfaces, passing from front to rear edge. Mesh forms three-dimensional structure, which passes over blade thickness major part between backet surface and back surface and/or over blade length major part between leading edge and trailing edge. Three-dimensional reinforcement structure comprises rods, interconnected by their connecting units, embedded into matrix and having rough surface with projecting grains. Number of rods connected to connecting units is variable. During composite blade making containing mesh reinforcement is produced, reinforcement is inserted into die casting mold and perform resin die casting into die casting mold for filling of mesh. Then resin is polymerized in casting mold and composite blade is extracted from mold. Reinforcement is made by layer-by-layer additive extension method, and mesh forms three-dimensional structure, which contains rods connected to each other by means of their connection assemblies and having rough surface with projecting grains.EFFECT: group of inventions provides higher strength of turbomachine composite blade.28 cl, 7 dwg
申请公布号 RU2602316(C2) 申请公布日期 2016.11.20
申请号 RU20140135165 申请日期 2014.08.28
申请人 TECHSPACE AERO S.A. 发明人 Rafael PEREZ
分类号 F01D5/14;F01D5/28 主分类号 F01D5/14
代理机构 代理人
主权项
地址