发明名称 SHAFT OF A GAS TURBINE ENGINE IN HYBRID DESIGN
摘要 A shaft of a turbine engine made from fiber-composite material, having a sinusoidal inner profile which extends over the entire length of the shaft on its inner wall, where a first inner layer forms the sinusoidal inner profile and has fibers arranged at ±45° relative to the axial direction, where the concave outer areas of the first layer are filled with fibers parallel to the center axis by a second layer to form a cylindrical outer contour. The second layer extends in the circumferential direction only in the concave area. A third layer with fibers arranged at ±30° relative to the axial direction is provided on the second layer A fourth layer with fibers arranged at ±88° relative to the axial direction is provided on the third layer. An intermediate layer is formed between the second and third layers from fibers parallel to the axial direction.
申请公布号 US2016230805(A1) 申请公布日期 2016.08.11
申请号 US201615018182 申请日期 2016.02.08
申请人 Rolls-Royce Deutschland Ltd & Co KG 发明人 BUSCH Christoph
分类号 F16C3/02 主分类号 F16C3/02
代理机构 代理人
主权项 1. A shaft of a turbine engine made from fiber-composite material, having a sinusoidal inner profile which extends over the entire length of the shaft on its inner wall, where the shaft has a constant cross-section over its length, where a first inner layer forms the sinusoidal inner profile and consists of fibers arranged at ±30° to ±60°, in particular ±45° relative to the axial direction of the shaft, where the concave outer areas of the first layer are filled with fibers parallel to the center axis by means of a second layer in order to form a cylindrical outer contour, where the second layer in each case extends in the circumferential direction only in the concave area, where a third layer with fibers arranged at ±20° to ±45°, in particular ±30° relative to the axial direction of the center axis is provided on the second layer and where a fourth layer with fibers arranged at ±80° to ±90°, in particular ±88° relative to the axial direction is provided on the third layer, wherein between the second layer and the third layer, an intermediate layer formed from fibers parallel to the axial direction is arranged and extends over the entire circumference of the shaft.
地址 Blankenfelde-Mahlow DE