Patent application number | Description | Published |
20120109892 | PARTITIONING ONLINE DATABASES - The present invention extends to methods, systems, and computer program products for partitioning online databases. Online database operations, such as, for example, SPLIT, MERGE, and DROP, are used to alter the arrangement of partitions in a federated database. A SPLIT operation splits rows at one partition across a plurality of other partitions. A MERGE operation merges rows at a plurality of partitions in to one partition. A DROP operation shifts responsibility for rows of data from one partition to another partition and then drops the rows from the one partition. | 05-03-2012 |
20120109926 | SCOPED DATABASE CONNECTIONS - The present invention extends to methods, systems, and computer program products for scoping the context used to access a database partition. Embodiments of the invention enable data isolation using partitions in multi-tenant databases, while relieving client applications from dealing with the partitions. For example, a computer system that includes a distributed database system comprising a plurality of database partitions in a federation receives a context to use when performing database access operations within the distributed database system. The context identifies specified relevant portion of the federation. The computer system also receives a database access operation that is associated with the context. The computer system modifies the semantics of the database access operation in accordance with the associated context, to direct application of the database access operation to the specified relevant portion of the federation. | 05-03-2012 |
20140344221 | PARTITIONING ONLINE DATABASES - Methods, systems, and computer program products are provided for partitioning online databases. Online database operations, such as, for example, SPLIT, MERGE, and DROP, are used to alter the arrangement of partitions in a federated database. A SPLIT operation splits rows at one partition across a plurality of other partitions. A MERGE operation merges rows at a plurality of partitions in to one partition. A DROP operation shifts responsibility for rows of data from one partition to another partition and then drops the rows from the one partition. | 11-20-2014 |
Patent application number | Description | Published |
20090159750 | HOLDER FOR FIXING COMPONENTS, IN PARTICULAR LINES, INSIDE AN AIRCRAFT WITHOUT USING HOLES - Disclosed is a holder for fixing all types of component, in particular lines, without using holes and largely without using tools inside a conventional fuselage structure of an aircraft with stringers and annular formers, the formers each being provided with an angle bracket at crossing points between a stringer and an annular former. The holder is configured so as to be split in two with a lower part and an upper part which can be connected thereto, the lower part being slidable onto an angle bracket. By attaching the upper part to the lower part, the holder is positionally fixed at the crossing point in the top region of an annular former. It is fixed in its final position by connecting the holder to a transverse line holder as a function element by means of an expansion pin or other connection elements. Other alternative function elements for fixing the components, such as a longitudinal line holder, a transverse batten or a longitudinal batten for specific installation requirements, may, if necessary, be combined with at least one holder so as to form holder arrangement with any desired degree of complexity. | 06-25-2009 |
20100107375 | HOLDER ARRANGEMENT FOR AN AIRCRAFT OR A SPACECRAFT AND AN AIRCRAFT OR A SPACECRAFT - In a holder arrangement of an aircraft or spacecraft comprising a structural member, a holder comprising at least one lower part and at least one upper part is provided, and these are formed so as to be able to be clamped together to be attached with a non-positive fit to a fastening portion of the structural member. The fastening portion can be clamped between the lower part and the upper part. The holder arrangement is characterised by at least one fixing strip which can be connected to the fastening portion of the structural member in the longitudinal direction thereof and which comprises a fixing profile for fixing the holder to the structural member in the longitudinal direction of the structural member with a positive fit. An aircraft or spacecraft has at least one holder arrangement of this type. | 05-06-2010 |
20100294896 | HOLDING DEVICE FOR MOUNTING PARTS INSTALLED INSIDE AN AIRCRAFT FUSELAGE - A holding device for a mounting part installed inside an aircraft fuselage having a lining including an insulating mat, the holding device includes a fastening part attached to the aircraft fuselage and protruding through an opening in the insulating mat; a sealing disk; and a holding part configured to attach the mounting part and being disposed on an inner side of the aircraft fuselage and cooperating with the fastening part configured to attach the mounting part so as to simultaneously fix the insulating mat between the fastening part and the holding part, wherein the holding part extends through the opening in a sealed manner, and wherein a lower surface of the sealing disk contacts and seals an edge region of the opening when the holding part is installed on the fastening part. | 11-25-2010 |
20100320327 | INSTALLATION SYSTEM FOR THE CONNECTION OF SYSTEMS TO A STRUCTURE OF AN AIRCRAFT, A MEASUREMENT SYSTEM AND A METHOD - An installation system includes a structure for an aircraft, at least one carrier for an arrangement of at least one device of the aircraft, at least two attachment elements configured to attach the at least one carrier to the structure, and at least one mounting having an adjustable reception element receiving one of the at least two attachment elements. | 12-23-2010 |
20110031350 | COMPONET, IN PARTICULAR A SHELL COMPONENT, WHICH CAN BE JOINED THERMALLY AND/OR MECHANICALLY, FOR BUILDING A FUSELAGE SECTION OF AN AIRCRAFT - A component for building a fuselage section of an aircraft includes a border area connectable to a corresponding further border area of a further component so as to form an electrically conductive joint, wherein the component includes a composite structure | 02-10-2011 |
20110266392 | PASSENGER SUPPLY ARRANGEMENT FOR AN AEROPLANE - A passenger supply arrangement provides a communications system and comfort system for a passenger of an aeroplane. The passenger supply arrangement includes a presentation surface configured to be integrated into a backrest of a passenger seat of an aeroplane and a passenger supply module configured to be disposed above the passengers seats of the aeroplane. The passenger supply module includes at least one projector configured to project an image onto the presentation surface. The image includes a monitoring area for playback of video and an operating area for displaying and for actuation of operating elements of the passenger supply module. | 11-03-2011 |
20120012698 | AIRCRAFT COMPRISING AN INSULATION SYSTEM FOR THERMAL AND ACOUSTIC INSULATION - The invention relates to an aircraft comprising an insulation system for thermal and acoustic insulation. Said insulation system includes a cabin, an outer skin, a sound insulating unit, and a heat insulating unit. The sound insulating unit is designed to acoustically insulate the aircraft. The heat insulating unit is designed to thermally insulate the aircraft. The sound insulating unit and the heat insulating unit are arranged between the cabin and the outer skin. | 01-19-2012 |
20120187248 | METHOD AND DEVICE FOR THE INSTALLATION OF SYSTEMS, AND A FREIGHT LOADING SYSTEM - Disclosed is a method for the installation of systems in an aeroplane fuselage | 07-26-2012 |
20120213955 | METHOD FOR MANUFACTURING A SHELL BODY AND CORRESPONDING BODY - In a method for manufacturing a shell, at least two shell sections are fabricated out of a composite fiber material, at least one compensation body of a plastically deformable material is secured to at least one limiting edge of at least one shell section, the shell sections are overlapped to form the shell, yielding flat seams between respectively adjacent shell sections. The at least one compensation body is arranged on at least one of the seams. In order to compensate for dimensional deviations in each overlap, the shape of the corresponding compensation bodies is changed, and the shells sections are joined together at the seams. | 08-23-2012 |
20120228427 | PRESSURE FUSELAGE OF AN AIRCRAFT WITH DOME-SHAPED PRESSURE BULKHEAD - A pressure fuselage of an aircraft, which fuselage in longitudinal direction comprises several fuselage sections, wherein at least one rear dome-shaped pressure bulkhead is provided to form an aircraft-internal pressurized region, with a ring-shaped frame element profile being provided for radially outward attachment of said dome-shaped pressure bulkhead to at least one fuselage section, wherein the frame element profile on the side of the dome-shaped pressure bulkhead comprises a U-shaped profile section whose first end-side limb is attached towards the back on the dome-shaped pressure bulkhead by way of connecting means, and whose elongated radially outward extending second limb establishes a connection to the at least one fuselage section in such a manner that it is possible for the connecting means to be installed solely from the aircraft-internal pressurized region. | 09-13-2012 |
20130115404 | LIGHTWEIGHT STRUCTURE, PARTICULARLY PRIMARY AIRCRAFT STRUCTURE OR SUBASSEMBLY, AS WELL AS METHOD FOR THE MANUFACTURE THEREOF - A lightweight structure at least sectionally composed of a plurality of connected mosaic elements and/or skin mosaic elements. The lightweight structure allows an essentially load-appropriate arrangement of the mosaic elements and/or the skin mosaic elements including the optional skin. The lightweight structure requires a significantly reduced number of connecting elements, such that the assembly effort can be reduced and an additional weight reduction can be achieved. Also, two variations of a method for manufacturing a lightweight structure are provided. Large-format lightweight structures such as, for example, an aircraft fuselage cell or partial shells thereof can also be manufactured in a reliable and dimensionally accurate fashion because only mosaic elements and skin mosaic elements, with relatively small dimensions, need to be handled. Other applications of the lightweight structure include launch vehicles, rocket stages, space stations, space station modules, satellites and masts or towers of wind power plants. | 05-09-2013 |
20130216850 | STRUCTURAL COMPONENT FOR AN AIRCRAFT OR SPACECRAFT - A structural component for an aircraft or spacecraft having an outer skin, comprising at least one former element for reinforcing the outer skin. The former element is arcuately curved in accordance with an inner contour of the outer skin | 08-22-2013 |
20140158279 | Attachment arrangement and installation method - An arrangement for attaching a system to a structure having a base element to retain the system, a positioning element to position the base element at a location on the structure and a fixation device to fix the base element at the location on the structure. The base element has a section for holding the system and a section for being clamped to the structure. The clamping section has an element for alignment on the positioning element. The positioning element has a surface for being bonded to the structure and a positioning section for acting together with the alignment element. The fixation device has a counter element with a clamping area for being positioned on an opposite side of the structure from the clamping section and a fastener for clamping the base element and the counter element to the structure. An installation method for such an attachment arrangement is provided. | 06-12-2014 |