Abstract: A decorative add-on in accordance with an exemplary embodiment of the present invention is structured and arranged to be attached to an article such as a shoe. The decorative add-on includes an aesthetic portion and an attachment portion. Typically, the aesthetic portion is prominently or noticeably 3D. The attachment portion is removably attached to the shoe. The attachment portion has a medial section, and two elongate insert sections at opposite sides of the medial section. The medial section is fixed to an inner side of the aesthetic portion. The insert sections are slidingly engaged in two matching elongate sheaths provided on the shoe. The attachment portion can be made of flexible resilient material. This facilitates convenient insertion of the insert sections into the sheaths, and secure retention of the insert sections in the sheaths. Further or alternatively, the insert sections can include magnetic material and flexible, resilient material.

Abstract: A decorative add-on in accordance with an exemplary embodiment of the present invention is structured and arranged to be attached to an article such as a shoe. The decorative add-on includes an aesthetic portion and an attachment portion. Typically, the aesthetic portion is prominently or noticeably 3D. The attachment portion is removably attached to the shoe. The attachment portion has a medial section, and two elongate insert sections at opposite sides of the medial section. The medial section is fixed to an inner side of the aesthetic portion. The insert sections are slidingly engaged in two matching elongate sheaths provided on the shoe. The attachment portion can be made of flexible resilient material. This facilitates convenient insertion of the insert sections into the sheaths, and secure retention of the insert sections in the sheaths. Further or alternatively, the insert sections can be interferingly engaged in the sheaths.

Abstract: A method for fabricating a rotor assembly for a turbine, the turbine including a central rotational axis is provided. The method includes forging a first rotor component from a first material, separately forging a second rotor component from a second material, and coupling the second rotor component to the first rotor component at a location radially inward of the first rotor component. The second rotor component is coupled to the first rotor component in at least one axial-circumferential plane that is at least one of substantially parallel and obliquely oriented with respect to the central rotational axis.

Abstract: One embodiment of a body material designated as a stripe or design (4) which contiguously mates couples and attaches to FIGS. 1 and 2 respectively. In addition 5 and 6 may also attach to FIG. 1 and FIG. 2 in areas 1, 2 and 3 by means of Velcro. Other embodiments are described and shown.

Abstract: A method for fabricating a rotor assembly for a turbine, the turbine including a central rotational axis is provided. The method includes forging a first rotor component from a first material, separately forging a second rotor component from a second material, and coupling the second rotor component to the first rotor component at a location radially inward of the first rotor component. The second rotor component is coupled to the first rotor component in at least one axial-circumferential plane that is at least one of substantially parallel and obliquely oriented with respect to the central rotational axis.

Abstract: A method, schema, and computer-readable medium provide various means for load balancing computing devices in a multi-server environment. The method, schema, and computer-readable medium for load balancing computing devices in a multi-server environment may be utilized in a networked server environment, implementing a spreadsheet application for manipulating a workbook, for example. The method, schema, and computer-readable medium operate to load balance computing devices in a multi-server environment including determining whether a file, such as a spreadsheet application workbook, resides in the cache of a particular server, such as a calculation server. Upon meeting certain conditions, the user request may be directed to the particular server.

Abstract: A forging blank of a forging nickel-base superalloy is forged in a forging press having forging dies made of a die nickel-base superalloy. The forging is accomplished by heating the forging blank to a forging-blank starting temperature of from about 1850° F. to about 1950° F., heating the forging dies to a forging-die starting temperature of from about 1500° F. to about 1750° F., placing the forging blank into the forging press and between the forging dies, and forging the forging blank at the forging-blank starting temperature using the forging dies at the forging-die starting temperature, to produce a forging.

Abstract: A forging blank of a forging nickel-base superalloy is forged in a forging press having forging dies made of a die nickel-base superalloy. The forging is accomplished by heating the forging blank to a forging-blank starting temperature of from about 1850° F. to about 1950° F., heating the forging dies to a forging-die starting temperature of from about 1500° F. to about 1750° F., placing the forging blank into the forging press and between the forging dies, and forging the forging blank at the forging-blank starting temperature using the forging dies at the forging-die starting temperature, to produce a forging.