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公开(公告)号：US12194557B2
公开(公告)日：2025-01-14
申请号：US16517068
申请日：2019-07-19
Applicant: The Boeing Company
Inventor： Stefanie Anita Meier , Don Browder
Abstract: A fixture holds a specimen during electrical discharge machining of the specimen and prevents tensile test samples cut from the specimen from bending or curving during the electrical discharge machining. The fixture has first engagement surfaces that clamp to one end of the specimen and has second engagement surfaces that clamp to the opposite end of the specimen during electrical discharge machining of the specimen. The fixture clamping to opposite ends of the specimen prevents the tensile test samples cut from the specimen from bending during electrical discharge machining of the specimen.
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公开(公告)号：US20250013956A1
公开(公告)日：2025-01-09
申请号：US18889243
申请日：2024-09-18
Applicant: THE BOEING COMPANY
Inventor： Andrea SANZONE , Millie STERLING , Rahul ASHOK , Rowena LOH
IPC: G06Q10/0631 , G06Q10/087
Abstract: The present disclosure provides for using machine learning to evaluate flight demographics and predict part consumption. Historical aircraft part consumption data indicating prior consumption of aircraft parts is accessed, and historical aircraft flight demographics associated with the historical aircraft part consumption data are determined. A machine learning model is trained based on the historical aircraft part consumption data and the historical aircraft flight demographics, and the machine learning model is deployed to predict future aircraft part consumption.
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公开(公告)号：US20250012761A1
公开(公告)日：2025-01-09
申请号：US18348505
申请日：2023-07-07
Applicant: The Boeing Company
Inventor： Brian Patrick Justusson , Joseph Daniel Schaefer
Abstract: A method of analyzing a composite structure for damage tolerance. The method includes obtaining a structural configuration and determining at least one metric of interest for the structural configuration. A dent depth meta-model is developed based on the structural configuration, the at least one metric of interest, and information obtained from a machine learning algorithm. The at least one metric of interest provides a constraint for the dent depth meta-model and the machine learning algorithm is trained based on a historical physical test dataset of a plurality of composite components. The dent depth meta-model is utilized to estimate an impact energy to establish a threshold dent depth in the structural configuration. A computer-based simulation is performed with the structural configuration utilizing the impact energy from the dent depth meta-model. At least one design value is determined for the structural configuration based on output data generated from the computer-based simulation.
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公开(公告)号：US20250010333A1
公开(公告)日：2025-01-09
申请号：US18348459
申请日：2023-07-07
Applicant: The Boeing Company
Inventor： Jeffrey H. Olberg , Sean D. Morden , Bradley G. Silva
Abstract: An applicator tool for coating a bore includes a tubular body and an inflatable bladder. The tubular body includes a proximal end and a distal end opposing the proximal end along a longitudinal axis. The tubular body also includes an expansion portion proximate the distal end and an internal volume in relation to the expansion portion. The inflatable bladder disposed within the internal volume of the tubular body in relation to the expansion portion. A method for coating a bore includes inserting an expansion portion of an applicator tool into the bore. A coating material having been previously disposed on the expansion portion. The method also includes applying a pressurized fluid to the applicator tool to expand the expansion portion within the bore and rotating the applicator tool to apply the coating material from the expansion portion to the bore. A system that includes the applicator tool is also disclosed.
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125.发明授权公开(公告)号：US12190470B2
公开(公告)日：2025-01-07
申请号：US17816775
申请日：2022-08-02
Applicant: The Boeing Company
Inventor： Jeremiah Scott , Robert Stephen Kanematsu Baker , Bryan James Beretta , Michael Louis Bernardoni
IPC: G06T3/4038 , G06T19/00
Abstract: Visualization within a spherical space is provided. The method comprises capturing a number of images from a common three-point coordinate capture location and creating a sphere of projected coordinates based on the capture location. Three-point coordinates of reference locations corresponding to the images are translated into spherical coordinates on the sphere. The spherical coordinates of the reference locations are translated into tour scene coordinates. The tour scene coordinates of the reference locations are then translated into equirectangular Cartesian coordinates. The images are displayed in a user interface according to the reference locations from the perspective of the capture location.
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Patent Agency Ranking
公开(公告)号：US12189376B2
公开(公告)日：2025-01-07
申请号：US17654087
申请日：2022-03-09
Applicant: The Boeing Company , University of Washington
Inventor： Mohammed H. Kabir , Alan Douglas Byar , John J. Dong , Alexandru I. Stere , Todd Clayton DePauw , Christina M. Doty , Ashith Paulson Kunnel Joseph , Navid Zobeiry
IPC: G05B19/418 , G06F18/2433
Abstract: A method, apparatus, system, and computer program products for managing a set of outliers in test data. A computer system analyzes a set of features derived from the test data using different outlier detection methods to generate a result of the set of outliers identified by the different outlier detection methods. The test data is obtained from testing a physical structure. The computer system determines a causality for the set of outliers in the result. The physical structure is retested with a set of changes determined using the causality identified for the set of outliers. The retesting generates new test data for the physical structure.
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公开(公告)号：US12189137B2
公开(公告)日：2025-01-07
申请号：US17678716
申请日：2022-02-23
Applicant: THE BOEING COMPANY
Inventor： Edwin P. Walker , Steven F. Griffin , Sudhakar Prasad
Abstract: A system and method are provided for super-resolution imaging beyond the Rayleigh spatial resolution limit of an optical system. In the context of a system, first and second pinhole assemblies are configured to be controllably positioned. The first and second pinhole assemblies define respective pinholes and being configured to be backlit. The system also includes a collimating lens configured to collimate at least a portion of the signals passing through the respective pinholes of the first and second pinhole assemblies. The system further includes an amplitude/phase mask configured to provide amplitude and phase modulation to signals received from the collimating lens and an imaging lens configured to focus the signals received from the amplitude/phase mask upon an image plane to permit objects to be separately identified.
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公开(公告)号：US12188511B2
公开(公告)日：2025-01-07
申请号：US17702612
申请日：2022-03-23
Applicant: THE BOEING COMPANY
Inventor： Samuel L. Block , Colin L Farr
Abstract: A nut cap assembly for securing an internal component to an external component includes a seal cap having a base and a shroud extending from the base. The base includes a mounting flange configured to be mounted to the internal component. The base includes an opening at a mounting end of the base configured to be mounted to the internal component. The base includes a seal groove surrounding the opening configured to receive a seal. The seal groove is open at the mounting end to interface the seal with the internal component. The shroud includes a nut pocket has a cap anti-rotation feature. The nut cap assembly includes a nut received in the nut pocket. The nut includes a threaded bore configured to threadably receive a threaded fastener used to secure the internal component to the external component. The nut includes a nut anti-rotation feature interfacing with the cap anti-rotation feature.
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公开(公告)号：US12187458B2
公开(公告)日：2025-01-07
申请号：US16184326
申请日：2018-11-08
Applicant: The Boeing Company
Inventor： Bryan R. Durr , Timothy Edward Jackson , Eric Scott Gubler
Abstract: A method, apparatus, and system for testing a fuel tank for an aircraft. Electrical power is sent to an optical data concentrator for the fuel tank for the aircraft from a power supply such that the optical data concentrator sends optical signals to optical sensors inside the fuel tank through optical fibers connecting the optical data concentrator to the optical sensors. The electrical power is sent during a phase of manufacturing of the aircraft. Test data is received from the optical data concentrator by a computer system. The test data is based on optical response signals received from the optical sensors. A determination of states for the optical sensors is made by the computer system using the test data. A graphical indication of the states determined for the optical sensors inside the fuel tank is displayed by the computer system in a graphical user interface on a display system.
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130.发明授权公开(公告)号：US12187429B2
公开(公告)日：2025-01-07
申请号：US17721074
申请日：2022-04-14
Applicant: THE BOEING COMPANY
Inventor： Curtis L. Hall, Jr. , David Lutz
Abstract: The present disclosure provides an insert that includes a locking mechanism that may either be formed integrally to the component or attached separately to the insert body. The top of the locking mechanism is offset from the first surface by an offset distance to enable the insert to be coupled to a recess of a component such as an aircraft component. An aperture formed in a top surface of the first portion is configured to allow additional elements to be coupled to the aircraft component. The coupling of the insert to the aircraft component is further promoted by a compression mechanism that forces the locking mechanism to couple to an overhang portion of the top layer after the force applied to the insert once it is positioned in the recess is removed, such that the top surface of the insert is co-planar with an outermost surface of the aircraft component.
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