发明名称 Solidifying and compressing a thin-walled metallic component e.g. gas turbine blade, by introducing the component into pressure-stable and liquid-tight container, and filling off remaining cavity of the component with liquid medium
摘要 <p>The method comprises introducing a thin-walled metallic component into a pressure-stable and liquid-tight container, filling off a remaining cavity of the component with a liquid medium such as water or hydrated liquid up to a predetermined height within the container, which has an increase in volume during transition of the liquid into solid aggregation state, and cooling the medium and/or cooling the container up to freezing the medium using liquid nitrogen in a shock-like manner. The solidification and compression of the component are carried out through the volume expansion of the medium. The method comprises introducing a thin-walled metallic component into a pressure-stable and liquid-tight container, filling off a remaining cavity of the component with a liquid medium such as water or hydrated liquid up to a predetermined height within the container, which has an increase in volume during transition of the liquid into solid aggregation state, and cooling the medium and/or cooling the container up to freezing the medium using liquid nitrogen in a shock-like manner. The solidification and compression of the component are carried out through the volume expansion of the medium during freezing. A cooling device is integratedly formed in the container. The process steps are repeatedly carried out. After each process cycle, the solidified medium is transferred again into the liquid aggregate condition by a heat supply. The container has several partial chambers for receiving a number of components. An independent claim is included for a component.</p>
申请公布号 DE102008021052(A1) 申请公布日期 2009.10.29
申请号 DE20081021052 申请日期 2008.04.26
申请人 MTU AERO ENGINES GMBH 发明人 BAYER, ERWIN;HUTTNER, ROLAND
分类号 C21D7/04 主分类号 C21D7/04
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