发明名称 SHROUD DEVICE OF A JET ENGINE
摘要 A shroud device of a jet engine, including a radially internal shroud appliance and a radially external shroud appliance. The internal shroud appliance is embodied with a radially internal ring-shaped shroud part and a radially external ring-shaped shroud part. The internal shroud appliance includes multiple blades that extend substantially in the radial direction between the internal shroud part and the external shroud part. The radially external shroud appliance is embodied with a radially internal ring-shaped shroud part and a radially external ring-shaped shroud part. The external shroud appliance includes multiple blades that extend substantially in the radial direction between the internal shroud part and the external shroud part. The internal shroud appliance is embodied as a first one-piece cast structural component and the external shroud appliance is embodied as a second one-piece cast structural component.
申请公布号 US2016069216(A1) 申请公布日期 2016.03.10
申请号 US201514847596 申请日期 2015.09.08
申请人 Rolls-Royce Deutschland Ltd & Co KG 发明人 HENKEL Martin;SOLA-PARDO Igor;MANIG Matthias
分类号 F01D25/24;F01D25/00;F02C3/04 主分类号 F01D25/24
代理机构 代理人
主权项 1. A shroud device of a jet engine, comprising a radially internal shroud appliance and a radially external shroud appliance, wherein the internal shroud appliance is embodied with a radially internal ring-shaped shroud part and a radially external ring-shaped shroud part, which in the installation position of the shroud device limit a core stream channel of the jet engine at least in certain parts, and wherein the internal shroud appliance has multiple blades that extend substantially in the radial direction of the shroud device between the internal shroud part and the external shroud part, wherein the radially external shroud appliance is embodied with a radially internal ring-shaped shroud part and a radially external ring-shaped shroud part, which in the installation position of the shroud device at least in certain areas limit a bypass duct of the jet engine, and wherein the external shroud appliance has multiple blades which extend substantially in the radial direction of the shroud device between the internal shroud part and the external shroud part, wherein the internal shroud appliance is embodied as a first one-piece cast structural component and the external shroud appliance is embodied as a second one-piece cast structural component.
地址 Blankenfelde-Mahlow DE