System and methods for managing changes to a product in a manufacturing environment including conversion of an engineering bill of material to a manufacturing bill of material
First Claim
1. A manufacturing process management (MPM) computer device comprising a processor and at least one non-transitory memory device, wherein said processor is in communication with said at least one non-transitory memory device, said MPM computer device configured to:
- store an engineering bill of materials for an aircraft to be assembled including a first plurality of parts;
determine based on lead times and a change among the first plurality of parts, that a bottleneck exists in the engineering bill of materials;
store a manufacturing bill of materials, for a first configuration of the aircraft to be assembled, including a second plurality of parts and a status of the change, wherein the change includes a plug insertion at a location corresponding to a station line, a water line or a buttock line of the aircraft;
receive schedule information on first and second production lines configured to manufacture the aircraft at different speeds based on the manufacturing bill of materials;
determine a first production schedule for the first production line based on the manufacturing bill of materials and the received schedule information;
after production has begun on the first production line to manufacture a complete version of the first configuration of the aircraft, receive a second manufacturing bill of materials for a second configuration of the aircraft;
determine a second production schedule for the second production line based on the second manufacturing bill of materials and the received schedule information, wherein the second production line is configured to manufacture a complete version of the second configuration of the aircraft by extending the first configuration from the location of the plug insertion;
compare the engineering bill of materials with the manufacturing bill of materials, and based on the comparison;
determine that the aircraft of the first configuration will be completed on the first production line after the aircraft of the second configuration on the second production line based on the different manufacturing speeds in the first and second production lines;
identify respective differences between each of the first plurality of parts and the second plurality of parts;
generate a three dimensional view of an area of the first configuration of the aircraft and the second plurality of parts;
trigger the change, in the three dimensional view based on the plug insertion;
determine a first grid overlay, for the first configuration, from a nose of the aircraft to a tail of the aircraft;
determine a second grid overlay for the second configuration;
display the second configuration including the second grid overlay;
shift a part of the first configuration and further shift the changed three dimensional view together with the shifted part, wherein the shifted three dimensional view is associated with a part of the second plurality of parts included in the three dimensional view; and
further shift the three dimensional view when displaying the second configuration of the aircraft to correspond to the associated part, wherein the displayed second configuration includes a zoom-in of a location of installation of the associated part from an overhead view of the aircraft by referencing to the station line, the water line, or the buttock line of the aircraft in order to differentiate the associated part from other multiple parts of a same part number.
1 Assignment
0 Petitions
Accused Products
Abstract
A manufacturing process management (MPM) computer device is provided. The MPM computer device is configured to store an engineering bill of materials for a product to be assembled including a first plurality of parts, store a manufacturing bill of materials for the product to be assembled including a second plurality of parts and a status, receive a request from a user to change the status of the manufacturing bill of materials, compare the first plurality of parts with the second plurality of parts, determine whether the first plurality of parts matches the second plurality of parts based on the comparison, if the comparison matches, change the status of the manufacturing bill of materials, and if the comparison does not match, prevent the status of the manufacturing bill of materials from changing.
46 Citations
21 Claims
-
1. A manufacturing process management (MPM) computer device comprising a processor and at least one non-transitory memory device, wherein said processor is in communication with said at least one non-transitory memory device, said MPM computer device configured to:
-
store an engineering bill of materials for an aircraft to be assembled including a first plurality of parts; determine based on lead times and a change among the first plurality of parts, that a bottleneck exists in the engineering bill of materials; store a manufacturing bill of materials, for a first configuration of the aircraft to be assembled, including a second plurality of parts and a status of the change, wherein the change includes a plug insertion at a location corresponding to a station line, a water line or a buttock line of the aircraft; receive schedule information on first and second production lines configured to manufacture the aircraft at different speeds based on the manufacturing bill of materials; determine a first production schedule for the first production line based on the manufacturing bill of materials and the received schedule information; after production has begun on the first production line to manufacture a complete version of the first configuration of the aircraft, receive a second manufacturing bill of materials for a second configuration of the aircraft; determine a second production schedule for the second production line based on the second manufacturing bill of materials and the received schedule information, wherein the second production line is configured to manufacture a complete version of the second configuration of the aircraft by extending the first configuration from the location of the plug insertion; compare the engineering bill of materials with the manufacturing bill of materials, and based on the comparison; determine that the aircraft of the first configuration will be completed on the first production line after the aircraft of the second configuration on the second production line based on the different manufacturing speeds in the first and second production lines; identify respective differences between each of the first plurality of parts and the second plurality of parts; generate a three dimensional view of an area of the first configuration of the aircraft and the second plurality of parts; trigger the change, in the three dimensional view based on the plug insertion; determine a first grid overlay, for the first configuration, from a nose of the aircraft to a tail of the aircraft; determine a second grid overlay for the second configuration; display the second configuration including the second grid overlay; shift a part of the first configuration and further shift the changed three dimensional view together with the shifted part, wherein the shifted three dimensional view is associated with a part of the second plurality of parts included in the three dimensional view; and further shift the three dimensional view when displaying the second configuration of the aircraft to correspond to the associated part, wherein the displayed second configuration includes a zoom-in of a location of installation of the associated part from an overhead view of the aircraft by referencing to the station line, the water line, or the buttock line of the aircraft in order to differentiate the associated part from other multiple parts of a same part number. - View Dependent Claims (2, 3, 4, 5, 6, 7)
-
-
8. A computer implemented method comprising:
-
storing, by a processor, an engineering bill of materials for an aircraft to be assembled including a first plurality of parts; determining, by the processor, based on lead times and a change among the first plurality of parts, that a bottleneck exists in the engineering bill of materials; storing, by the processor, a manufacturing bill of materials for a first configuration of the aircraft to be assembled including a second plurality of parts and a status of the change, wherein the change includes a plug insertion at a location corresponding to a station line, a water line or a buttock line of the aircraft; receiving, by the processor, schedule information on first and second production lines configured to manufacture the aircraft at different speeds based on the manufacturing bill of materials; determining, by the processor, a first production schedule for the first production line based on the manufacturing bill of materials and the received schedule information; after production has begun on the first production line to manufacture a complete version of the first configuration of the aircraft, receiving, by the processor, a second manufacturing bill of materials for a second configuration of the aircraft; determining, by the processor, a second production schedule for the second production line based on the second manufacturing bill of materials and the received schedule information, wherein the second production line is configured to manufacture a complete version of the second configuration of the aircraft by extending the first configuration from the location of the plug insertion; comparing, by the processor, the engineering bill of materials with the manufacturing bill of materials, and based on the comparison; determining, by the processor, that the aircraft of the first configuration will be completed on the first production line after the aircraft of the second configuration on the second production line based on the different manufacturing speeds in the first and second production lines; identifying, by the processor, respective differences between each of the first plurality of parts and the second plurality of parts; generating, by the processor, a three dimensional view of an area of the first configuration of the aircraft and the second plurality of parts; triggering, by the processor, the change, in the three dimensional view based on the plug insertion; determining, by the processor, a first grid overlay, for the first configuration, from a nose of the aircraft to a tail of the aircraft; determining, by the processor, a second grid overlay for the second configuration; displaying, by the processor, the second configuration including the second grid overlay; shifting, by the processor, a part of the first configuration and further shift the changed three dimensional view together with the shifted part, wherein the shifted three dimensional view is associated with a part of the second plurality of parts included in the three dimensional view; and further shifting, by the processor, the three dimensional view when displaying the second configuration of the aircraft to correspond to the associated part, wherein the displayed second configuration includes a zoom-in of a location of installation of the associated part from an overhead view of the aircraft by referencing to the station line, the water line, or the buttock line of the aircraft in order to differentiate the associated part from other multiple parts of a same part number. - View Dependent Claims (9, 10, 11, 12, 13, 14)
-
-
15. A non-transitory computer-readable storage media having computer-executable instructions embodied thereon, which, when executed by a processor, cause said processor to:
-
store an engineering bill of materials for an aircraft to be assembled including a first plurality of parts; determine based on lead times and a change among the first plurality of parts, that a bottleneck exists in the engineering bill of materials; store a manufacturing bill of materials for a first configuration of the aircraft to be assembled including a second plurality of parts and a status of the change, wherein the change includes a plug insertion at a location corresponding to a station line, a water line or a buttock line of the aircraft; receive schedule information on first and second production lines configured to manufacture the aircraft at different speeds based on the manufacturing bill of materials; determine a first production schedule for the first production line based on the manufacturing bill of materials and the received schedule information; after production has begun on the first production line to manufacture a complete version of the first configuration of the aircraft, receive a second manufacturing bill of materials for a second configuration of the aircraft; determine a second production schedule for the second production line based on the second manufacturing bill of materials and the received schedule information, wherein the second production line is configured to manufacture a complete version of the second configuration of the aircraft by extending the first configuration from the location of the plug insertion; compare the engineering bill of materials with the manufacturing bill of materials, and based on the comparison; determine that the aircraft of the first configuration will be completed on the first production line after the aircraft of the second configuration on the second production line based on the different manufacturing speeds in the first and second production lines; identify respective differences between each of the first plurality of parts and the second plurality of parts; generate a three dimensional view of an area of the first configuration of the aircraft and the second plurality of parts; trigger the change, in the three dimensional view based on the plug insertion; determine a first grid overlay, for the first configuration, from a nose of the aircraft to a tail of the aircraft; determine a second grid overlay for the second configuration; display the second configuration including the second grid overlay; shift a part of the first configuration and further shift the changed three dimensional view together with the shifted part, wherein the shifted three dimensional view is associated with a part of the second plurality of parts included in the three dimensional view; and further shift the three dimensional view when displaying the second configuration of the aircraft to correspond to the associated part, wherein the displayed second configuration includes a zoom-in of a location of installation of the associated part from an overhead view of the aircraft by referencing to the station line, the water line, or the buttock line of the aircraft in order to differentiate the associated part from other multiple parts of a same part number. - View Dependent Claims (16, 17, 18, 19, 20, 21)
-
Specification