Systems and methods for manufacturing components for gas turbine engines

    公开(公告)号:US11566298B2

    公开(公告)日:2023-01-31

    申请号:US16406129

    申请日:2019-05-08

    Abstract: Methods and masks for manufacturing component of gas turbine engines are described. The methods include applying a mask to a protected surface of the component, the component having a designated surface to be treated by a shot peen operation. The mask includes a full masking portion configured to prevent a shot peen media from impacting the protected surface. A masking control region is arranged around the designated surface. The masking control region is configured to control an amount of force imparted to the component by shot peen media during the shot peen operation, wherein the masking control region extends from the full masking portion to the designated surface. The designated surface is shot peened with shot peen media to form a compressive stress region within the component proximate the designated surface and a tapering transition of compressive forces within the component proximate the masking control region.

    HIGH-STRENGTH BLACKPLATE AND MANUFACTURING METHOD THEREFOR

    公开(公告)号:US20230017796A1

    公开(公告)日:2023-01-19

    申请号:US17784452

    申请日:2020-12-16

    Applicant: POSCO

    Inventor: Jai-Ik Kim

    Abstract: The present invention provides a high-strength tin blackplate and a manufacturing method therefor.
    The tin blackplate according to an exemplary embodiment of the present invention includes: by wt %, 0.03 to 0.09% of carbon (C); 0.2 to 0.4% of manganese (Mn); 0.01 to 0.06% of aluminum (Al); 0.15 to 0.45% of chromium (Cr); 0.05 to 0.25% of copper (Cu); 0.03 to 0.08% of titanium (Ti); and the balance of iron (Fe) and inevitable impurities, and has a yield strength of 570 to 700 MPa.

    Producing a partially hardened formed part

    公开(公告)号:US11555224B2

    公开(公告)日:2023-01-17

    申请号:US16740587

    申请日:2020-01-13

    Abstract: A process of producing a partially hardened metallic formed part comprises: heating a semi-finished product of hardenable hot-formable steel sheet to a hardening temperature; hot-forming the heated semi-finished product in a combined hot-forming cutting device into a three-dimensional formed part; cutting the formed part in the combined hot-forming cutting device; pressure-hardening the formed part in the hot-forming cutting device into a hardened formed part such that a first partial region is hardened by rapid cooling and that a second partial region of the formed part is heat-treated so as to comprise a greater ductility and a lower strength than the first partial region, wherein the operation of cutting the formed part takes place at least in one of the first and second partial region. A combined hot-forming cutting device can be used to produce a metallic formed part.

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