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Section 11.5  Casting Techniques for Single crystal Components  2


                I l.5   Casting Techniques for Single-crystal Components

                The characteristics of single-crystal and polycrystalline structures in metals were
                described in Section 1.3. This section describes the techniques used to cast single-
                crystal components (such as gas turbine blades), which generally are made of nickel-
                based superalloys and used in the hot stages of the engine. The procedures involved
                also can be used for other alloys and components.

                Conventional Casting of Turbine Blades.  The conventional-casting process uses a
                ceramic mold. The molten metal is poured into the mold and begins to solidify at the
                ceramic walls. The grain structure developed is polycrystalline, similar to that
                shown in Fig. 1O.2c. However, the presence of grain boundaries makes this structure
                susceptible to creep and cracking along the boundaries under the centrifugal forces
                and elevated temperatures commonly encountered in an operating gas turbine.

                Directionally Solidified Blades.  The directional-soIidi]?cation process (Fig. 11.25a)
                was first developed in 1960. The ceramic mold is preheated by radiant heating, and
                the mold is supported by a water-cooled chill plate. After the metal is poured into the
                mold, the chill-plate assembly is lowered slowly. Crystals begin to grow at the chill-
                plate surface and on upward, like the columnar grains shown in Fig. 10.3. The blade
                thus is solidified directionally, with longitudinal, but no transverse, grain boundaries.
                Consequently, the blade is stronger in the direction of centrifugal forces developed in
                the gas turbine.

                Single-crystal Blades.  In crystal growing, developed in 1967, the mold has a con-
                striction in the shape of a corkscrew or helix (Figs. 11.25 b and c). The cross section
                is so small that it allows only one crystal to fit through. The mechanism of crystal
                growth is such that only the most favorably oriented crystals are able to grow (a sit-
                uation similar to that shown in Fig. 1O.3) through the helix, because all others are
                intercepted by the walls of the helical passage.
                    As the assembly is lowered slowly, a single crystal grows upward through the
               constriction and begins to grow in the mold. Strict control of the rate of movement
               is important. The resultant casting is a single-crystal blade. Although these blades



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                                                          "'  $  Radiant i
                                                                hnai
                    Heat
                  bafiles         dlam






                                                      Coll.
               Columnaf                                cry:              ;triction
                 crystals
               chin plate                       cm

                                  (H)                           (D)                        (C)
               FIGURE ll.25  Methods of casting turbine blades: (a) directional solidification; (b) method
               to produce a single-crystal blade; and (C) a single-crystal blade with the constriction portion
               still attached. Source: (a) and (b) After B.H. Kear, (c) Courtesy of ASM International.
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