Abstract: A user experience repository may contain base layouts and variant metadata for applications of an enterprise. An application design platform may receive, from a designer, an indication of a selected base layout for a selected application and interact with the designer to create a user experience variant (e.g., a page layout). The designer may then define an assignment rule for the user experience variant, the assignment rule including custom logic and multiple user parameters (e.g., a user role, country, language, etc.), and the system may store information about the user experience variant and assignment rule. An enterprise application service platform may determine that a user is accessing the selected application and evaluate the custom logic of the assignment rule based on user parameters of the user accessing the selected application. In accordance with the evaluation, the system may arrange to provide the appropriate user experience variant to the user.

Abstract: A stiffened structural component for an aircraft includes a first material sheet with a first surface, and at least one elongate bulge that bulges out in a direction transverse to the first surface in order to stiffen the structural component, wherein each of the at least one bulge comprises two edges that extend along the first surface, wherein a continuous bulging surface extends between the edges, and wherein the bulges are formed integrally into the first material sheet through pressing.

Abstract: A stiffened structural component for an aircraft includes a first material sheet with a first surface, and at least one elongate bulge that bulges out in a direction transverse to the first surface in order to stiffen the structural component, wherein each of the at least one bulge comprises two edges that extend along the first surface, wherein a continuous bulging surface extends between the edges, and wherein the bulges are formed integrally into the first material sheet through pressing.

Abstract: A load bearing element for attachment of a heat generating unit to a heat sensitive supporting structure, wherein said load bearing element includes at least one body integrally formed by additive layer manufacturing, ALM. The body is adapted to provide a controlled heat transfer from said heat generating unit to said heat sensitive supporting structure.

Abstract: An airframe component includes a skin panel, a plurality of stringers attached to the skin panel, and at least one former running substantially perpendicular to the plurality of stringers on the skin panel, the at least one former being generatively formed on the skin panel by an Additive Manufacturing (AM) method.

Abstract: A load bearing element for attachment of a heat generating unit to a heat sensitive supporting structure, wherein said load bearing element includes at least one body integrally formed by additive layer manufacturing, ALM. The body is adapted to provide a controlled heat transfer from said heat generating unit to said heat sensitive supporting structure.

Abstract: A business object model, which reflects data that is used during a given business transaction, is utilized to generate interfaces. This business object model facilitates commercial transactions by providing consistent interfaces that are suitable for use across industries, across businesses, and across different departments within a business during a business transaction. In some operations, software creates, updates, or otherwise processes information related to a business partner relationship and a business partner hierarchy business object.

Abstract: The present disclosure relates to methods, systems, and software for performing parallel processing on a set of business object actions forming a batch process. The batch process may be performed by compiling a group of independent work packages, each work package representing a discrete business object action. The work packages are clustered and an individual session for each work package is created. The work packages are then executed in parallel by a framework for parallel processing, external of an application requesting the batch process. Each session is closed after processing of the work package is completed, and the cluster is closed after processing of the work packages is completed.

Abstract: The invention relates to the fuselage structure of an aircraft with an outer skin (1) which is reinforced by several vertically aligned transverse ribs (7) and several horizontally aligned longitudinal ribs (8) wherein the outer skin (1) has several windows (5) which each comprise a window frame (6). In order to be able to have a free and flexible choice regarding both the size and arrangement of view or access openings in the fuselage shell it is proposed according to the invention that at least one transverse rib (7) runs through the window frame (6) of a window (5) so that the transverse rib ends in an upper section (9) of the window frame (6) and in a lower section (10) of the window frame (6).

Abstract: The present disclosure relates to methods, systems, and software for performing parallel processing on a set of business object actions forming a batch process. The batch process may be performed by compiling a group of independent work packages, each work package representing a discrete business object action. The work packages are clustered and an individual session for each work package is created. The work packages are then executed in parallel by a framework for parallel processing, external of an application requesting the batch process. Each session is closed after processing of the work package is completed, and the cluster is closed after processing of the work packages is completed.