Abstract: An assembly (10) that can be both joined and parted by temperature processing. A parting member (20) captured between two members of the assembly exhibits a state change as a function of temperature such that the two members can be joined with a meltable joining material (18) at a joining temperature, operated at an operating temperature lower than the joining temperature, and then separated at a parting temperature higher or lower than the operating and joining temperatures as a result of a parting force caused by the state change of the parting member. In one embodiment, the parting member has a coefficient of thermal expansion higher than a coefficient of thermal expansion of the assembly members such that differential thermal expansion causes the parting member to expand across the interface (16) between the members to generate the parting force.

Abstract: An assembly (10) that can be both joined and parted by temperature processing. A parting member (20) captured between two members of the assembly exhibits a state change as a function of temperature such that the two members can be joined with a meltable joining material (18) at a joining temperature, operated at an operating temperature lower than the joining temperature, and then separated at a parting temperature higher or lower than the operating and joining temperatures as a result of a parting force caused by the state change of the parting member. In one embodiment, the parting member has a coefficient of thermal expansion higher than a coefficient of thermal expansion of the assembly members such that differential thermal expansion causes the parting member to expand across the interface (16) between the members to generate the parting force.

Abstract: The invention concerns a Ni based alloy suitable for single 5 crystalline, directionally solidified or polycrystalline components to be used at high temperatures. The alloy is a?/ alloy and consists of different alloying elements within defined ranges. Among other defined ranges of elements, the alloy contains Pd in a significant amount sufficient to provide the alloy with an improved resistance against hydrogen embrittlement. The invention also concerns a component designed for use as a component in a high temperature environment. Furthermore, the invention concerns a gas turbine arrangement. Moreover, the invention concerns the use of Pd for providing an alloy with improved resistance against hydrogen embrittlement. The inclusion of two or more rare earth elements in the alloy provides enhanced bondcoat compatibility.

Abstract: The invention concerns a Ni based alloy suitable for single 5 crystalline, directionally solidified or polycrystalline components to be used at high temperatures. The alloy is a?/ alloy and consists of different alloying elements within defined ranges. Among other defined ranges of elements, the alloy contains Pd in a significant amount sufficient to provide the alloy with an improved resistance against hydrogen embrittlement. The invention also concerns a component designed for use as a component in a high temperature environment. Furthermore, the invention concerns a gas turbine arrangement. Moreover, the invention concerns the use of Pd for providing an alloy with improved resistance against hydrogen embrittlement. The inclusion of two or more rare earth elements in the alloy provides enhanced bondcoat compatibility.

Abstract: An improved nickel-based superalloy having high corrosion and oxidation resistance and good compatibility with a thermal barrier coating. The enhanced oxidation resistance and compatibility with the thermal barrier coating results from the inclusion of two or more rare earth elements. The superalloy is useful for the fabrication of components for a gas turbine.

Abstract: The invention relates to a nickel-base superalloy. The alloy according to the invention is characterized by the following chemical composition (details in % by weight): 7.7-8.3 Cr, 5.0-5.25 Co, 2.0-2.1 Mo, 7.8-8.3 W, 5.8-6.1 Ta, 4.9-5.1 Al, 1.3-1.4 Ti, 0.11-0.15 Si, 0.11-0.15 Hf, 200-750, preferably 200-300 ppm of C, 50-400, preferably 50-100 ppm of B, remainder Ni and production-related impurities. It is distinguished by very good castability and a high resistance to oxidation.

Abstract: The invention relates to a nickel-base superalloy. The alloy according to the invention is characterized by the following chemical composition (details in % by weight): 7.7-8.3 Cr, 5.0-5.25 Co, 2.0-2.1 Mo, 7.8-8.3 W, 5.8-6.1 Ta, 4.9-5.1 Al, 1.3-1.4 Ti, 0.11-0.15 Si, 0.11-0.15 Hf, 200-750, preferably 200-300 ppm of C, 50-400, preferably 50-100 ppm of B, remainder Ni and production-related impurities. It is distinguished by very good castability and a high resistance to oxidation.