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METHOD FOR MANUFACTURING MONOBLOCK BLADES BY CUTTING BY ABRASIVE WATER JET

机译:用磨料射流切割法制备单块叶片的方法。

摘要

1. A method of manufacturing a monoblock blade disc (1), including:! - the step of cutting out material from the block (100) with an abrasive water jet, carried out in such a way as to obtain blanks (102) of the blades extending in the radial direction from the disk (4); then! - the stage of milling the blanks (102) of the blades. ! 2. A method according to claim 1, wherein at the step of cutting material from the block (100), at least 50 wt% of said block (100) is removed by an abrasive water jet. ! 3. A method according to claim 1, wherein said step of milling the blade blanks (102) is carried out so as to obtain profiling of the blade blank (202), this step is followed by a finishing step by milling the blade blanks (202) to obtain the blades (2) final profile. ! 4. A method according to claim 1, wherein the diameter of said monoblock blade disk is equal to or greater than 800 mm. ! 5. A method according to claim 1, wherein the thickness (e) of the disc (4) of said monoblock blade disc is greater than or equal to 100 mm. ! 6. A method according to claim 1, wherein the blades (2) of the monoblock blade disk are twisted. ! 7. The method according to claim 1, wherein said block (100) of material is made of titanium or its alloys. ! 8. The method of claim 1, wherein said monoblock blade is a monoblock blade for an aircraft gas turbine engine. !nine. The method of claim 1, wherein said monoblock blade is a monoblock blade of a turbine or compressor rotor of an aircraft gas turbine engine.
机译:1.一种制造整体式刀片盘(1)的方法,包括:! -用磨料射流从块体(100)上切下材料的步骤,以从圆盘(4)获得沿径向延伸的叶片的坯料(102)的方式进行;然后! -研磨叶片的坯件(102)的阶段。 ! 2.根据权利要求1所述的方法,其中,在从所述块体(100)切割材料的步骤中,通过研磨水射流去除至少50重量%的所述块体(100)。 ! 3.根据权利要求1所述的方法,其中,执行所述铣削所述叶片坯料(102)的步骤,以获得对所述叶片坯料(202)的轮廓,在该步骤之后是通过铣削所述叶片坯料(20)的精加工步骤。 202)以获得叶片(2)的最终轮廓。 ! 4.根据权利要求1所述的方法,其中,所述整体式叶片盘的直径等于或大于800mm。 ! 5.根据权利要求1所述的方法,其中,所述整体式叶片盘的盘(4)的厚度(e)大于或等于100mm。 ! 6.根据权利要求1所述的方法,其特征在于,所述整体式叶片盘的叶片(2)是扭曲的。 ! 7.根据权利要求1所述的方法,其中,所述材料块(100)由钛或其合金制成。 ! 8.根据权利要求1所述的方法,其中,所述整体式叶片是用于飞机燃气涡轮发动机的整体式叶片。 !九。 2.根据权利要求1所述的方法,其中,所述整体式叶片是飞机燃气涡轮发动机的涡轮或压缩机转子的整体式叶片。

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