The Boeing Company

United Technologies Corporation

Theboeing Company

Roger W Engelbart

Reed Hannebaum

Christopher Mark Vaccaro

Tim Pollock

Steve Schrader

Nancy L Wood

Eric Rector

Scott T Holmes

Craig Thompson Walters

Richard J Steckel

April L Beisiegel

James William Fonda

Stanley Allen Lawton

Jeffrey J Kilwin

James Leonard Scherer

Taisia Tsukruk Lou

George E Bible

Frank Gregory Speno

Timothy J Pollock

Jeff Putnam

Brian Stutzman

Elizabeth Ann Paton

Bruce E McIlroy

Sam Orr

Arun Ayyagari

James C Kennedy

Brice Aaron Johnson

Michael Robert Chapman

Philip Lawrence Freeman

Jeffrey G Thompson

Allen James Halbritter

Jonathan Blake Vance

Steven J Burpo

Nathan Rylan Smith

Steven A Dorris

Loyal Bruce Shawgo

Douglas Duane Trimble

David E Corman

Eugene Arthur Myers

Michael P Renieri

John Robert Dworschak

Scott Edwin Black

John William Adams

Kathryn A Soucy

Ronald J Newcomer

David Fortner

Brian S Hensley

Taisia V Tsukruk

Jeffrey Haywood

Samuel D Orr

Ron Newcomer

Timothy T Pollock

William A Lane

James W Fonda

Douglas D Trimble

Apparatus, systems, and methods for the inspection of holes in transparent materials, the apparatus including a processor, an illumination probe, and a detection probe. The illumination probe includes a laser light source and a reflective surface and is configured to be inserted into a first hole in the transparent material. The detection probe includes a second reflective surface and a photodetector and is configured to be inserted in a second hole in the transparent material. Laser light is directed onto the first reflective surface within the first hole and is reflected through a wall of the first hole, into the transparent material, and reflected by the second reflective surface to the photodetector. The photodetector transmits a measured light intensity value to the processor, which compares the light intensity value to a standard intensity value to determine whether or not a crazing condition exists in the second hole.

Apparatus, systems, and methods for the laser inspection of holes in transparent materials

A method and system provide for reducing gaps between two mating parts. Either or both parts may be nondestructively inspected at a plurality of locations on a surface to gather a data set relating to the part thickness. The data set may be used to calculate a set of as-built thickness values for the part and a set of deviations from a design model. A mating area may be determined for mating surfaces of the parts. One or more layers of sacrificial material in the mating area may be prepared for any deviations greater than a design allowance. The system may include a ply cutting device and an additive manufacturing device coupled to a computer to receive the sacrificial material layer data and shim data and to cut the one or more layers of sacrificial material and to construct the shim. A shim may be constructed for any deviations equal to or greater than a minimum shim thickness. The one or more layers of sacrificial material may be applied to the part, cured, and machined to a desired thickness. The shim may be applied between the part surfaces. The parts may be fitted and assembled together.

Predictive surface adjustment for joint assembly

A system and method for nondestructive inspection of a unitized composite structures is provided. The system includes an infrared thermographic camera and a carriage that can be mounted on, for example, adjacent frames of the unitized composite structure. The carriage can move along the length of the frames while the infrared thermographic camera collects and analyzes thermographic images of the frame, skin, and stiffeners. The carriage can be moved to other frames and the inspection continued until the entire unitized composite structure has be inspected.

Robotic infrared thermographic inspection for unitized composite structures

A method, system and computer program product are provided in order to evaluate corrosion loss and to establish maintenance actions based thereupon. In the context of a method, a structure is inspected to generate corrosion information and a corrosion model of the structure is generated based upon the corrosion information. The method also includes generating a combined corrosion model based upon the corrosion model and a baseline model of the structure including material types and thicknesses at respective locations on the structure. The method further includes establishing maintenance actions including modification of an inspection interval based upon the combined corrosion model. Corresponding systems and computer program products are also provided.

Method and system for evaluating corrosion loss

A method and system may be provided for determining a set of parameters for preparing a skin for assembly to a substructure. The skin may be nondestructively inspected to gather a data set relating to the skin thickness. Sets of as-built thickness values for the skin and of deviations from a nominal map of the skin thickness may be calculated. A mating area for the skin and substructure and a set of one or more locations for fastener holes in the mating area may be determined. A set of parameters for the one or more fastener holes and a set of one or more fastener lengths may be generated using the deviations. A tool may cut the one or more fastener holes using the set of parameters and the skin and substructure may be fastened using fasteners selected according to the generated set of one or more fastener lengths. The system may be used with a numerically-controlled machine, a nondestructive inspection system, and may include a computer coupled to the nondestructive inspection system for calculating the parameters for preparing the holes and the lengths of the one or more fasteners.

Predictive preparation of material for joint assembly

Methods, systems, and apparatus for detection of a condition in a hole defined by a transparent material that is at least partially enclosed by one or more substantially opaque materials. The method may include positioning a light source in a first hole in the transparent material, directing light from the positioned light source through the transparent material and toward a second hole that is adjacent to the first hole. A prism may be positioned so that the light transmitted from the light source through the machined inner surface of the second hole is visible through a viewing face of the prism. By observing the transmitted light, a surface condition of the machined inner surface of the second hole may be determined.

Methods, apparatus, and systems for inspecting holes in transparent materials

A system comprises a laser projector, an automated material placement head, and a laser inspection system. The laser projector is configured to project boundary projection line onto a part. The automated material placement head is configured to lay down a course of composite material. The laser inspection system is connected to the automated material placement head and configured to project a laser beam into a laser line parallel to the motion of the automated material placement head in laying the composite material.

Measurement of ply boundaries

A method of thermographic inspection includes absorbing, at an applique applied to a test area of an article, light from a testing light source. The method further includes emitting, by the applique, thermal radiation directed to a capture device, the thermal radiation corresponding to at least a portion of the light absorbed by the applique.

Applique and method for thermographic inspection

A method and a system are provided for predicting and creating a shim for use in a joint where two parts, such as a skin and a substructure, are assembled together. Digital models for the skin and the substructure may be used as nominal maps of the outlines and profiles of the parts. The skin may be inspected, e.g., by nondestructive means, such as ultrasound, to determine as-built thickness profile for comparison to the skin's digital model of the thickness profile. Mating areas of the skin and substructure may be determined from their digital models of their outlines. Deviations in the mating areas of the as-built thickness of the skin from the digital model of the skin may be used to generate a digital model of a shim. The shim may be constructed from its digital model by additive manufacturing techniques that may involving machining or 3D printing.

Predictive shimming of joints

A method, system and computer-readable storage medium are provided to facilitate inspection of a composite part during manufacture. In the context of a system, a system for inspecting a composite part during manufacture is provided that includes an inspection system configured to detect an in-process anomaly with respect to a ply of the composite part during placement of the ply. The system also includes a computing system configured to determine part location coordinates of the in-process anomaly detected by the inspection system with respect to the ply of the composite part. The computing system is also configured to map the in-process anomaly to a digital part model based upon the part location coordinates. The system additionally includes a display, responsive to the computing system, configured to present a representation of the digital part model including an indication of the in-process anomaly relative thereto.

System and method for inspecting a composite part during manufacture

A method and apparatus for reworking an inconsistency on a part. Information about the inconsistency on the part may be identified using data generated by a nondestructive evaluation system. A portion of a section of the part in which the inconsistency is located may be removed based on the information about the inconsistency. A profile for the section of the part may be identified. Rework image data may be generated using the profile in which the rework image data comprises a number of patch images. The number of patch images may be projected onto a rework material as a number of patch projections for use in forming a patch to be applied over the section of the part.

Method and apparatus for reworking inconsistencies on parts

Provided are methods, systems, and computer program products for inspecting composite items. Specifically, a method involves analyzing an image of or, more generally, data characterizing condition of a top layer, which is disposed over a bottom layer. The method also involves performing a structural integrity check based on any anomalies detected in the top layer during this analysis as well as based on any anomalies previously detected in the bottom layer. As such, this structural integrity check accounts for characteristics of multiple layers, in some embodiments, all layers applied up to point of this inspection. In addition to the detected anomalies, the structural integrity check may account for previously performed repairs. The structural integrity check may be performed on individual portions of a composite item while, for example, other portions continue receiving a new composite layer, which may be referred to as an inline inspection.

Composite inspection and structural check of multiple layers

A method and system are provided for non-destructively evaluating a workpiece hidden by an overlying structure. In the context of a method, a workpiece is interrogated with radiation, such as x-ray radiation, that also propagates through the overlying structure. The method further includes collecting data representative of radiation backscattered from the workpiece. Based upon a thickness and material of the overlying structure, the method compares the data that has been collected from the workpiece with reference data representative of radiation backscattered from a standard that includes different respective material loss indicators hidden by an overlying structure of the same thickness and material. Each material loss indicator is a physical representation of a different amount of material loss. As a result of the comparison, the method estimates the material loss of the workpiece.

Method and system for non-destructively evaluating a hidden workpiece

A method and apparatus for inspecting a composite structure. A thickness profile of a portion of a region of a composite structure is identified. The region has a cross-section with non-parallel surfaces. An estimated thickness for a location within the region and outside of the portion is identified using the thickness profile. An indication of whether the location has undesirable porosity is generated based on information about attenuation of response sound signals and the estimated thickness for the location.

Porosity inspection system for composite structure with non-parallel surfaces

A method for reworking an inconsistency on a part. A location of the inconsistency is identified for the part in a model of the part. An image is generated for a rework for the part. The image is projected for the rework on the part based on the location identified for the inconsistency. The rework is performed for the inconsistency on the part using the image projected on the part.

Method for remote rework imaging for part inconsistencies

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St. Louis, MO, United States of America

Roger W Engelbart