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公开(公告)号:US20160251745A1
公开(公告)日:2016-09-01
申请号:US15033369
申请日:2014-10-10
CPC分类号: C23C24/04 , B05B7/205 , B05C19/008 , C23C4/073 , C23C4/129 , F01D5/288 , F05D2220/32 , F05D2230/90
摘要: The invention relates to a device for High Velocity Oxygen Fuel thermal spraying process for coating a component, especially a gas turbine component. The device includes a liquid fuel fired combustion chamber, a de-Laval section, a powder injector block with powder injectors and a barrel all arranged around and along an axis. The powder injector block includes at least four powder injectors arranged in an equal circumferential distance around the axis and an exchangeable hot gas section insert inside the powder injector block designed as a cylindrical bush with at least four openings, the openings being arranged in an equal circumferential distance around the axis in the cylinder, wherein the bush is fixed by the at least four powder injectors extending through said openings.
摘要翻译: 本发明涉及用于涂覆组分,特别是燃气轮机组件的用于高速氧燃料热喷涂方法的装置。 该装置包括液体燃料燃烧的燃烧室,脱拉瓦段,具有粉末喷射器的粉末喷射器块和全部沿轴线布置的筒体。 粉末喷射器块包括至少四个粉末喷射器,其围绕轴线以相等的圆周距离布置,并且粉末喷射器块内的可更换的热气体部分插入件设计成具有至少四个开口的圆柱形衬套,所述开口布置成相等的圆周 围绕圆柱体中的轴线的距离,其中衬套由延伸穿过所述开口的至少四个粉末喷射器固定。