Gas inlet cylinder of gas turbine and manufacturing process thereof
A technology of gas turbine and manufacturing process, which is applied in the direction of gas turbine devices, manufacturing tools, jet propulsion devices, etc., and can solve problems such as expensive castings, shrinkage cavities, and no effect
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Embodiment 1
[0011] Embodiment 1: A gas turbine intake cylinder, its chemical composition is: C≤0.25%, Si≤0.60%, Mn≤1.00%, P≤0.040%, S≤0.040%, Cr≤0.25%, Mo≤0.25%,
[0012] Ni≤0.50%, Cu≤0.50%. The gas turbine intake cylinder mechanical properties: Rm (MPa) ≥ 480, R P 0.2(MPa) ≥ 245, A ≥ 19%, Z ≥ 35%.
Embodiment 2
[0013] Embodiment 2: A manufacturing process for making gas turbine intake cylinders using the components of claim 1: 1. Determination of the casting process plan: the design of the casting process must ensure that there are no shrinkage cavities (looseness) in each part of the casting, and the casting of the gas turbine has many Thin-walled castings with curved surfaces and small wall thickness deviations but relatively complex structures. Castings with this structure are suitable for simultaneous solidification. However, if the casting process is prepared according to the principle of simultaneous solidification, looseness will inevitably occur in the middle of the casting wall thickness. Therefore, the following process design ideas are established: sequential solidification is mainly used to avoid shrinkage cavity (loose) defects of castings to ensure the internal quality of castings, and simultaneous solidification is supplemented To control the contact area between the ri...
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