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公开(公告)号：US20170327201A1
公开(公告)日：2017-11-16
申请号：US15151577
申请日：2016-05-11
Applicant: The Boeing Company
Inventor： Joseph D. Doyle , Christopher A. Greer , Brian D. Smith , Richard M. Wcislak
CPC classification number: B64C3/26 , B23P19/105 , B64F5/10 , G01B11/005 , G01B11/14 , G05B19/41805 , G06F17/5086 , G06F17/5095
Abstract: Methods for using predictive shimming to optimize part-to-part alignment. In accordance with one embodiment, the process uses measurement data acquired from mating surfaces and key features to virtually align two parts in a manner that optimizes the final orientation of the parts and determines the geometry of the shim needed to achieve this orientation during assembly.
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公开(公告)号：US09798836B2
公开(公告)日：2017-10-24
申请号：US14384422
申请日：2013-03-01
Applicant: JFE Steel Corporation
Inventor： Takanobu Saito
IPC: G06F17/50
CPC classification number: G06F17/50 , G06F17/5009 , G06F17/5086 , G06F17/5095 , G06F2217/08 , G06F2217/16
Abstract: An optimization analyzing apparatus, configured of a computer, includes: a part shape pattern setting device that divides a part of a structural body including a two-dimensional element and/or a three-dimensional element into a plurality of segments in an axis direction, changes a height or width of a cross section of each of the segments divided, and sets a part shape pattern; a rigidity analyzing device that performs plural kinds of rigidity analyses of the structural body; a multivariate analyzing device that obtains a multiple regression coefficient, and a coefficient of determination or an adjusted R-square; a rigidity analysis selection device that selects any having strong correlation from among the rigidity analyses of the plural kinds; and a cross-sectional shape determination device that determines a cross-sectional shape of each of the segments divided.
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公开(公告)号：US20170291369A1
公开(公告)日：2017-10-12
申请号：US15441649
申请日：2017-02-24
Applicant: United Technologies Corporation
Inventor： Sergei F. Burlatsky , Dmitri Novikov , William J. Brindley , David Ulrich Furrer
CPC classification number: B33Y10/00 , B22F3/1055 , B22F2003/1057 , B22F2999/00 , B29C64/153 , B29C64/393 , B29K2105/251 , B33Y30/00 , B33Y50/02 , G06F17/5086 , G06F2217/12 , Y02P10/295 , Y02P90/265 , B22F2003/1056 , B22F2203/03
Abstract: A method of evaluating and validating additive manufacturing operations includes generating a multidimensional space defined by a plurality of bounds, each of the bounds being defined on a distinct parameter of an additive manufacturing process and each of the bounds being directly related to the occurrence of a downskin roughness flaw, each of the parameters being a dimension in a multi-dimensional coordinate system, determining a coordinate position of at least one additive manufacturing operation within the multi-dimensional coordinate system, and categorizing the operation as free of downskin roughness flaws when the coordinate position is within the multi-dimensional space.
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公开(公告)号：US20170291365A1
公开(公告)日：2017-10-12
申请号：US15441607
申请日：2017-02-24
Applicant: United Technologies Corporation
Inventor： Sergei F. Burlatsky , Dmitri Novikov , William J. Brindley , David Ulrich Furrer
CPC classification number: B33Y10/00 , B22F3/1055 , B22F2003/1057 , B22F2999/00 , B29C64/153 , B29C64/393 , B29K2105/251 , B33Y30/00 , B33Y50/02 , G06F17/5086 , G06F2217/12 , Y02P10/295 , Y02P90/265 , B22F2003/1056 , B22F2203/03
Abstract: A method of evaluating and validating additive manufacturing operations includes generating a multidimensional space defined by a plurality of bounds, determining a coordinate position of at least one additive manufacturing operation within the multi-dimensional coordinate system, and categorizing the operation as flaw free when the coordinate position is within the multi-dimensional space. Each of the bounds is defined on a distinct parameter of an additive manufacturing process, each of said parameters being a dimension in a multi-dimensional coordinate system
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公开(公告)号：US20170286591A1
公开(公告)日：2017-10-05
申请号：US15086009
申请日：2016-03-30
Applicant: NHK SPRING CO., LTD.
Inventor： Yoshio KOBAYASHI , Shinichi NISHIZAWA , Nobuhisa YASUDA
CPC classification number: G06F17/5086 , E05F1/1238 , E05Y2201/624 , E05Y2900/548 , G06F17/5018
Abstract: In a design method of torsion bars used for a trunk lid, free shapes of the torsion bars unhitched from the trunk lid are designed. A center line model of the initial free shape is geometrically and statically created on the basis of a design specification. The center line model of an open shape is created from the free shape model and is deformed into a center line model of a closed modified shape. The center line models of the analyzed closed shape and the target closed shape is compared with each other to obtain a difference torque and a difference vector occurring between corresponding nodes on the center lines. The center line model is so changed as to decrease the difference torque and the difference vector.
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Patent Agency Ranking
公开(公告)号：US20170284676A1
公开(公告)日：2017-10-05
申请号：US15085203
申请日：2016-03-30
Applicant: Siemens Energy, Inc.
Inventor： Andrew J. North , Juan Enrique Portillo Bilbao , Walter Ray Laster , Joseph Meadows
IPC: F23R3/28 , B22F5/00 , B23K15/00 , G06F17/50 , B23K26/70 , B33Y10/00 , B33Y50/02 , B33Y80/00 , B22F3/105 , B23K26/342
CPC classification number: F23R3/28 , B22F3/1055 , B22F5/009 , B23K15/0026 , B23K15/0086 , B23K15/0093 , B23K26/342 , B23K26/702 , B23K2101/001 , B23K2103/26 , B33Y10/00 , B33Y80/00 , F23R3/425 , G06F17/5086 , Y02P10/295
Abstract: Method and computer-readable model for additively manufacturing an injector assembly or a ducting arrangement including such assembles, as may be used in a combustion system of a gas turbine engine. The injector assembly may include a reactant-guiding structure (42) that may be configured to define a curvilinear flow path (47) to route a flow of reactants from a first flow direction (50) to a second flow direction (52) toward a cross-flow of combustion gases (60). A cross-flow guiding structure (54) may further define a flow path (58) to route a portion of the cross-flow of combustion gases toward an outlet side of the cross-flow guiding structure. Disclosed injector assemblies can be configured to reduce pressure loss while providing an effective level of mixing of the injected reactants with the passing cross-flow. Respective injector assemblies or the entire ducting arrangement may be formed as a unitized structure, such as a single piece using a rapid manufacturing technology, such as 3D Printing/Additive Manufacturing (AM) technology.
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公开(公告)号：US20170255719A1
公开(公告)日：2017-09-07
申请号：US15445352
申请日：2017-02-28
Applicant: XARKIN SOFTWARE
Inventor： MICHAEL KELLY
IPC: G06F17/50
CPC classification number: G06F17/5009 , G06F17/5086
Abstract: The simulation of motion for articulated assemblies is important within a range of industries from computer gaming, virtual reality through to android/robot developments and exoskeletons/prosthesis for individuals. However, even low complexity systems with only a small number of moving parts are computationally intractable with respect to analytic solutions. Accordingly, simulations are employed which are themselves complex. It would be beneficial therefore to provide a means of creating actuation and motion sequences for an articulated assembly from a description of the properties of the assembly, the properties of the desired motion, the properties of the terrain over which the assembly will move, and a set of physical laws governing the motion. By framing desired motion within the input parameters allows creation of actuation and motion sequences conforming to the target based upon these four input elements within tolerances which are defined for one or more of input elements or combinations of them.
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公开(公告)号：US09744727B2
公开(公告)日：2017-08-29
申请号：US14243274
申请日：2014-04-02
Applicant: Autodesk, Inc.
Inventor： Karl Willis
CPC classification number: B29C64/393 , B33Y50/00 , B33Y50/02 , G06F17/5086
Abstract: A computer-implemented layout tool includes a mechanical design engine for configuring mechanical design components to be included in a design, an electrical design engine for configuring electrical components to be included in the design, a constraint engine for identifying a 3D printer to be used to print the design and to provide design constraints including feedback for inoperative or impermissible configurations of one or more mechanical components or electrical pathways associated with the design; and a simulation engine for simulating, at least, electrical performance of the design based on one or more electrical components added to the design after printing and proposed electrical pathways.
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公开(公告)号：US09727688B2
公开(公告)日：2017-08-08
申请号：US14525838
申请日：2014-10-28
Applicant: Vinlocks LLC
Inventor： John Overman , Joey Hendrich
CPC classification number: G06F17/5086 , G05B15/02 , G06F15/00 , H04L9/0822 , H04L9/0866 , H04L2209/84 , Y02T10/82
Abstract: A computer program, method, and system for locksmithing. The computer program, method, and system receive vehicle information, obtain a key code for a lock based on the vehicle information, decrypt the key code to determine key specification data, and provide the key specification data to a user, such that a duplicate key corresponding to the lock can be formed.
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公开(公告)号：US20170206303A1
公开(公告)日：2017-07-20
申请号：US14995781
申请日：2016-01-14
Applicant: Rolls-Royce Engine Services Oakland, Inc.
Inventor： Bradley W. Burkett
CPC classification number: G06F17/5086 , F01D9/041 , F01D21/003 , F05D2260/80 , F05D2260/81 , F05D2270/8041 , G01B11/24
Abstract: A computing device for determining effective flow areas of a turbine or turbine engine includes optically scanning and digital modeling of turbine components to produce virtual vanes, virtual vane segments, and virtual ring assemblies. The computing device determines both individual effective flow areas between vanes and the total effective flow area of a vane ring assembly. Based on the virtual vanes and determined effective flow areas, the computing device may compare one or more turbine components to a reference turbine to determine whether the turbine is out of specification and aid in repair, modification, or reassembly of the turbine or turbine engine.
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