Nonconformance identification and visualization system and method

• US 10,481,768 B2
• Filed: 04/12/2013
• Issued: 11/19/2019
• Est. Priority Date: 04/12/2013
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Senesac, Christopher J., Heinefield, Ralph P., Honea, Michael
• Primary Examiner(s): Pan, Yongjia
• Application Number:
  US13/861,678
• Publication Number:
  US 20140310629A1
• Time in Patent Office: 2,412 Days
• Field of Search: None
• CPC Class Codes: G06F 3/0484 for the control of specific functions or operations, e.g. selecting or manipulating an object, an image or a displayed text element, setting a parameter value or selecting a range
• CPC Class Codes: G06Q 10/06 Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling

Abstract

A method and apparatus for analyzing nonconformances. A volume in an aircraft is identified. The nonconformances within the volume of the aircraft are identified. Graphical indicators are displayed indicating the nonconformances within the volume in a graphical user interface on a display device.

Claims

1. A method for graphically analyzing nonconformances on an entire build of an aircraft, the method comprising:

selecting from a graphic user interface, a model of the entire build of the aircraft from a depiction of objects located in a facility;

identifying, via a processor unit comprising an object manager comprising;

an object visualization system, a shop order visualization system, a noncomformace visualization system, and the graphic user interface, a volume in the model of the aircraft;

importing, via the nonconformance visualization system in the processor unit, the nonconformances associated with parts within the volume of the model of the aircraft by;

displaying, on a display device, an input data window such that the input data window displays the nonconformances in rows such that each row comprises;

a corresponding non-conformance, and a nonconformance type, and a position of the aircraft in the facility, such that the position of the aircraft in the facility indicates a state of assembly of the aircraft; and

responsive to a user selection of the nonconformance type, parsing the nonconformances associated with the parts within the volume in the model of the aircraft based on the nonconformance type;

displaying, in the graphical user interface on the display device, graphical indicators indicating the nonconformances within the volume in-the model of the aircraft;

determining, using the graphical indicators, density information for the nonconformances;

for the model of the aircraft, or cumulatively for;

any selected models of other aircraft in the facility, or for any aircraft located at the position of the aircraft in the facility over a selected period of time;

determining, using the density information, an area of interest.

2. The method of claim 1 further comprising:

displaying the graphical indicators to indicate a presence of a cluster of the nonconformances within the volume, wherein the cluster identifies nonconformances having parameters that relate the nonconformances to one another.

3. The method of claim 1, wherein the step of identifying the volume in the model of the aircraft comprises:

displaying sections of the model of the aircraft in the graphical user interface on the display device, wherein the sections correspond to the sections as manufactured for assembly of the aircraft and wherein the sections are selectable;

detecting a selection of a section from the sections displayed in the graphical user interface;

identifying the volume in the model of the aircraft corresponding to the section selected from the sections displayed in the graphical user interface; and

displaying the volume in the model identified for the section selected in the graphical user interface.

4. The method of claim 1, wherein the volume is selected from one of all of the model of the aircraft and a section of the aircraft as manufactured for assembly of the aircraft.

5. The method of claim 1 further comprising:

identifying parts in the volume; and

displaying the parts in the graphical user interface with the nonconformances.

6. The method of claim 5, wherein the parts are all of the parts in the volume.

7. The method of claim 5, wherein identifying the parts in the volume comprises:

identifying the state of assembly of the aircraft; and

identifying the parts as ones present in the model of the aircraft for the state of assembly of the aircraft.

8. The method of claim 7, wherein the state of assembly is a current state of assembly.

9. The method of claim 1, wherein the volume is a first volume and the aircraft is a first aircraft and the model is a first model, the method further comprising:

identifying a number of volumes for a number of models of aircraft in addition to the first volume for the model of the first aircraft.

10. The method of claim 1 further comprising:

managing assembly of the aircraft based on the nonconformances displayed within the volume of the model of the aircraft displayed in the graphical user interface.

11. The method of claim 1, wherein a graphical indicator in the graphical indicators is selected from at least one of a color, cross hatching, an icon, highlighting, animation, or a font.

12. The method of claim 1, further comprising:

displaying the graphical indicators indicating the nonconformances within the volume in the graphical user interface on the display device such that the graphical indicators indicate a presence of the area of interest.

13. The method of claim 1, further comprising:

displaying positions within the model of the aircraft; and

displaying a graphical indicator indicating the position of the model of the aircraft where the area of interest is present.

14. The method of claim 1, wherein determining the area of interest comprises:

identifying nonconformance records for other aircraft;

comparing the nonconformances in the aircraft with other nonconformances in other aircraft nonconformances present in a nonconformance data base, and forming a comparison; and

determining whether the area of interest is present from the comparison.

15. A method for graphically analyzing nonconformances on an entire build of every aircraft of:

a particular model, or in a facility, the method comprising;

selecting from a graphic user interface, a model of an entire build of any aircraft from a depiction of objects located in the facility;

identifying, via a processor unit comprising an object manager comprising;

an object visualization system, a shop order visualization system, a noncomformace nonconformance visualization system, and the graphic user interface, a volume in a model of an object;

importing, via the processor unit, nonconformances of parts within the volume of the model of the object by;

displaying, on a display device, an input data window such that the input data window displays the nonconformances in rows such that each row comprises;

a corresponding nonconformance, a nonconformance type associated with the corresponding nonconformance, and a position of an aircraft in the facility, such that the position of the aircraft in the facility indicates a state of assembly of the aircraft in the facility; and

responsive to a user selection of the nonconformance type, parsing the nonconformances associated with the parts within the volume in the model of the object based on the nonconformance type;

displaying graphical indicators indicating the nonconformances within the volume in a graphical user interface on the display device;

displaying the graphical indicators in the graphical user interface when the parts are contained within other parts or hidden from view;

determining, using the graphical indicators, cumulative density information for the nonconformances for the entire build of every aircraft;

of the particular model, or in the facility;

determining, using the cumulative density information, an area of interest; and

changing at least one of a design, an assembly process, a fabrication process, or a vendor of the parts within the area of interest.

16. The method of claim 15 further comprising:

displaying the graphical indicators to indicate a presence of a cluster of the nonconformances within the volume.

17. The method of claim 15, wherein the step of identifying the volume in the model of the aircraft comprises:

displaying sections of the model of the aircraft in the graphical user interface on the display device, wherein the sections correspond to the sections as manufactured for assembly of the aircraft and wherein the sections are selectable;

detecting a selection of a section from the sections displayed in the graphical user interface;

identifying the volume in the model of the aircraft corresponding to the section selected from the sections displayed in the graphical user interface; and

displaying the volume in the model identified for the section selected in the graphical user interface.

18. An apparatus that comprises:

a data processing system that comprises a processor configured to implement an object manager that comprises;

an object visualization system, a shop order status visualization system, and a nonconformance visualization system, the object manager configured to;

identify a volume in a model of an aircraft;

import nonconformances of parts within the volume of the model of the aircraft by;

displaying, on a display device, an input data window;

wherein each nonconformance is displayed in a row of information in the input data window; and

responsive to a user selection of;

a nonconformance type presented in the row, or a location of the model of the aircraft in a facility, parsing the nonconformances associated with the parts within the identified volume in the model of the aircraft based on the selected nonconformance type;

displays graphical indicators indicating the nonconformances within the volume in a graphical user interface on the display device;

determines, based on the graphical indicators in the graphical user interface, when the parts are contained within other parts or hidden from view;

determines, based on the graphical indicators, density information for the nonconformances;

determines, based on the density information, an area of interest; and

changes, at least one of a design, an assembly process, a fabrication process or a vendor of the parts within the area of interest.

19. The apparatus of claim 18, wherein the object manager is further configured to display the graphical indicators to indicate a presence of a cluster of the nonconformances within the volume.

20. The apparatus of claim 18, wherein in identifying the volume in the aircraft, the object manager:

displays sections of the model of the aircraft in the graphical user interface on the display device, wherein the sections correspond to sections as manufactured for assembly of the aircraft and wherein the sections are selectable;

detects a selection of a section from the sections displayed in the graphical user interface;

identifies the volume in the model of the aircraft corresponding to the section selected from the sections displayed in the graphical user interface; and

displays the volume in the model identified for the section selected in the graphical user interface.