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1.发明公开公开(公告)号：US20230341303A1
公开(公告)日：2023-10-26
申请号：US17726091
申请日：2022-04-21
Applicant: The Boeing Company
Inventor： Joseph D. Schaefer , Brian P. Justusson , Haozhong Gu
IPC: G01N3/08
CPC classification number: G01N3/08 , G01N2203/04 , G01N2203/0017
Abstract: A tension load fixture for applying tension or loading forces to a specimen comprises a pair of tension arms and an imaging device. The pair of tension arms are configured to releasably couple to opposite end regions of a specimen and to apply tension or loading forces to the specimen. The specimen is configured to be positioned between the pair of tension arms and defines a notch between the opposite end regions of the specimen. The notch extends from a side of the specimen to a middle region of the specimen. The imaging device is configured to capture one or more images of the middle region of the specimen and is configured to rotate about a central axis of the tension load fixture that is proximate to the middle region of the specimen to facilitate generation of a three-dimensional image of the middle region of the specimen as the specimen is subjected to tension or loading forces.
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2.发明申请公开(公告)号：US20200173881A1
公开(公告)日：2020-06-04
申请号：US16207311
申请日：2018-12-03
Applicant: The Boeing Company
Inventor： Joseph D. Schaefer , Brian P. Justusson
Abstract: A computer is configured to generate visual representations of a composite filler material, such as a noodle or a crossply laminate, for example, to determine the progressive creation, density, and spacing of a plurality of cracks in the filler material. The composite filler material is disposed at a connection interface between a load-bearing composite structural component, such as a stringer or a spar, for example, and the structural framework of a vehicle on which those structural components are utilized.
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公开(公告)号：US20180252680A1
公开(公告)日：2018-09-06
申请号：US15971937
申请日：2018-05-04
Applicant: The Boeing Company
Inventor： Hong Hue Tat , Yuan-Jye Wu , Joseph D. Schaefer , Anne Kao , Mary J. Mathews , Matthew G. Pike , Victor P. Pauca , Rongzhong Li
Abstract: An apparatus comprises an acoustic sensing system and an analyzer module. The acoustic sensing system is positioned relative to an object, wherein the acoustic sensing system detects acoustic emissions and generates acoustic waveform data for the acoustic emissions detected. The analyzer module is implemented in a computer system that receives load data and the acoustic waveform data for the object, generates a plurality of frequency distribution functions using the acoustic waveform data, and generates a frequency distribution function time evolution image containing a plurality of points of each of the plurality of frequency distribution functions.
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4.发明申请公开(公告)号：US20200257768A1
公开(公告)日：2020-08-13
申请号：US16274868
申请日：2019-02-13
Applicant: THE BOEING COMPANY
Inventor： Brian P. Justusson , Joseph D. Schaefer , Matthew Jeffrey Molitor
IPC: G06F17/50
Abstract: A method includes obtaining failure initiation characteristics of a bonding layer of one or more bonded structures and determining, based on the failure initiation characteristics, a first characteristic dimension for each analysis element of a first portion of a finite element analysis model. The method includes obtaining failure propagation characteristics of the bonding layer and determining, based on the failure propagation characteristics, a second characteristic dimension for each analysis element of a second portion of the model. The method includes assigning a first set of material parameters to analysis elements of the first portion of the model and assigning a second set of material parameters to analysis elements of the second portion of the model. The method includes evaluating failure modes of the one or more bonded structures based on a solution to the model, the first set of material parameters, and the second set of material parameters.
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5.发明申请公开(公告)号：US20200175132A1
公开(公告)日：2020-06-04
申请号：US16207281
申请日：2018-12-03
Applicant: The Boeing Company
Inventor： Joseph D. Schaefer , Brian P. Justusson
IPC: G06F17/50
Abstract: A computer is configured to generate a computer model to determine the progressive creation, density, and spacing of a plurality of cracks in a filler material, such as a “noodle,” for example, disposed at a connection interface between a load-bearing composite structural component, such as a stringer or a spar, for example, and the structural framework of a vehicle on which those structural components are utilized.
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Patent Agency Ranking
公开(公告)号：US10578528B2
公开(公告)日：2020-03-03
申请号：US15447245
申请日：2017-03-02
Applicant: THE BOEING COMPANY
Inventor： Joseph D. Schaefer , Brian P. Justusson , Brian Kasperson , David R. Barbee
Abstract: A compression test fixture including a first specimen engagement member having a first channel, the first channel having a first depth; a second specimen engagement member having a second channel having a second depth that is different than the first depth; and at least one coupling member engaged to both the first specimen engagement member and the second specimen engagement member such that a gap is defined between the first specimen engagement member and the second specimen engagement member, where the first channel and the second channel support the test specimen within the gap such that at least one opposing major surface of the test specimen is visible within the gap.
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公开(公告)号：US10564130B2
公开(公告)日：2020-02-18
申请号：US15971937
申请日：2018-05-04
Applicant: The Boeing Company
Inventor： Hong Hue Tat , Yuan-Jye Wu , Joseph D. Schaefer , Anne Kao , Mary J. Mathews , Matthew G. Pike , Victor P. Pauca , Rongzhong Li
Abstract: An apparatus comprises an acoustic sensing system and an analyzer module. The acoustic sensing system is positioned relative to an object, wherein the acoustic sensing system detects acoustic emissions and generates acoustic waveform data for the acoustic emissions detected. The analyzer module is implemented in a computer system that receives load data and the acoustic waveform data for the object, generates a plurality of frequency distribution functions using the acoustic waveform data, and generates a frequency distribution function time evolution image containing a plurality of points of each of the plurality of frequency distribution functions.
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公开(公告)号：US11846055B2
公开(公告)日：2023-12-19
申请号：US17399815
申请日：2021-08-11
Applicant: The Boeing Company
Inventor： Brian P. Justusson , Joseph D. Schaefer
Abstract: An example method includes determining, by a computing system, a dry thickness of a fabric preform. The method also includes determining, by the computing system, a debulked thickness of the fabric preform using the dry thickness of the fabric preform. In addition, the method includes determining, by the computing system, a stitch tension using the dry thickness of the fabric preform and the debulked thickness of the fabric preform. And the method includes causing, by the computing system, a stitching machine to apply a through-the-thickness stitch having the stitch tension to the fabric preform.
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公开(公告)号：US20230118613A1
公开(公告)日：2023-04-20
申请号：US17501798
申请日：2021-10-14
Applicant: The Boeing Company
Inventor： Joseph D. Schaefer , Brian P. Justusson
IPC: G06F30/20
Abstract: Systems, apparatuses and methods provides for technology that generates a plurality of discrete and finite elements associated with a component, where a number of the plurality of discrete and finite elements corresponds to a size of an estimated process zone. The technology further identifies material input properties of the component, models crack propagation throughout the plurality of discrete and finite elements based on the material input properties and models a release response in the plurality of discrete and finite elements based on the material input properties.
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公开(公告)号：US11379628B2
公开(公告)日：2022-07-05
申请号：US16584119
申请日：2019-09-26
Applicant: The Boeing Company
Inventor： Brian P. Justusson , Joseph D. Schaefer , Bryan W. Lilley
Abstract: A method, apparatus, and system for managing a composite structure. A set of component models is created for a set of components in the composite structure. A set of embedded reinforcement element models is placed within the set of component models for the set of components in the composite structure to form a composite structure model for the composite structure. The set of embedded reinforcement element models is for a set of embedded reinforcements embedded within the set of components in the composite structure. A structural analysis of the composite structure is performed using the composite structure model formed by the set of component models and the set of embedded reinforcement element models, wherein the set of embedded reinforcement element models enables modeling at least one of a deformation or a failure of embedded reinforcements.
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