Nonconformance visualization system
First Claim
1. A method for recording a nonconformance in an aircraft, the method comprising:
- identifying a model for the aircraft;
displaying sections of the aircraft in a graphical user interface on a display device, wherein the sections correspond to sections as manufactured for assembly of the aircraft and wherein the sections are selectable;
identifying a location of a nonconformance of a part in the aircraft;
displaying graphical representations of parts in a volume in the model in the graphical user interface on the display device from a selection of a section in the sections, wherein the volume corresponds to the location of the nonconformance in the aircraft;
identifying the nonconformance for a part from a selection of a graphical representation of the part from the graphical representations of the parts, wherein the nonconformance of the part in the aircraft is identified prior to the identification of the part from the selection of the graphical representation of the part from the graphical representation of parts; and
recording the nonconformance that was identified.
1 Assignment
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Accused Products
Abstract
A method and apparatus for recording a nonconformance in an aircraft. A model is identified for the aircraft. Sections of the aircraft are displayed in a graphical user interface on a display device. The sections correspond to sections as manufactured for assembly of the aircraft. The sections are selectable. Graphical representations of parts are displayed in a volume in the model in the graphical user interface on a display device from a selection of a section in the sections. The volume corresponds to a location of the nonconformance in the aircraft. The nonconformance for a part is identified from a selection of a graphical representation of the part from the graphical representations of the parts. The nonconformance that was identified is recorded.
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Citations
18 Claims
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1. A method for recording a nonconformance in an aircraft, the method comprising:
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identifying a model for the aircraft; displaying sections of the aircraft in a graphical user interface on a display device, wherein the sections correspond to sections as manufactured for assembly of the aircraft and wherein the sections are selectable; identifying a location of a nonconformance of a part in the aircraft; displaying graphical representations of parts in a volume in the model in the graphical user interface on the display device from a selection of a section in the sections, wherein the volume corresponds to the location of the nonconformance in the aircraft; identifying the nonconformance for a part from a selection of a graphical representation of the part from the graphical representations of the parts, wherein the nonconformance of the part in the aircraft is identified prior to the identification of the part from the selection of the graphical representation of the part from the graphical representation of parts; and recording the nonconformance that was identified. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8)
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9. A method for recording a nonconformance in an object, the method comprising:
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displaying sections of the object in a graphical user interface on a display device, wherein the sections correspond to sections as manufactured for assembly of the object and wherein the sections are selectable; identifying a location of a nonconformance in the object; displaying graphical representations of parts in a volume in a model of the object in the graphical user interface on the display device from a selection of a section in the sections, wherein the volume corresponds to the location of the nonconformance in the object; identifying the nonconformance for a part from a selection of a graphical representation of the part from the graphical representations of the parts in response to the identification of the location of the nonconformance in the object, wherein the nonconformance of the part in the object is identified prior to the identification of the part from the selection of the graphical representation of the part from the graphical representation of parts; and storing the nonconformance that was identified. - View Dependent Claims (10)
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11. An apparatus comprising:
an object manager configured to; identify a model for an aircraft; display sections of the aircraft in a graphical user interface on a display device, wherein the sections correspond to sections as manufactured for assembly of the aircraft, and wherein the sections are selectable; identify a location of a nonconformance in the aircraft; display graphical representations of parts in a volume in the model in the graphical user interface on the display device from a selection of a section in the sections, wherein the volume corresponds to a location of nonconformance in the aircraft; identify the nonconformance for a part from a selection of a graphical representation of the part from the graphical representations of the parts, wherein the nonconformance of the part in the aircraft is identified prior to the identification of the part from the selection of the graphical representation of the part from the graphical representation of parts; and store the nonconformance that was identified. - View Dependent Claims (12, 13, 14, 15, 16)
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17. A manufacturing system comprising:
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a control system configured to control manufacturing equipment configured to manufacture an aircraft; and an object manager in the control system, wherein the object manager is configured to; identify a model for the aircraft; identify a location of a nonconformance in the aircraft; display sections of the aircraft in a graphical user interface on a display device, wherein the sections correspond to sections as manufactured for assembly of the aircraft, wherein the sections are selectable, wherein graphical representations of parts are displayed in a volume in the model in the graphical user interface on the display device from a selection of a section in the sections, and wherein the volume corresponds to a location of the nonconformance in the aircraft; identify the nonconformance for a part from a selection of a graphical representation of the part from the graphical representations of the parts, wherein the nonconformance of the part in the aircraft is identified prior to the identification of the part from the selection of the graphical representation of the part from the graphical representation of parts; and store the nonconformance that was identified. - View Dependent Claims (18)
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Specification