System and method for managing machine servicing including workscope generation

• US 20060010152A1
• Filed: 07/12/2004
• Published: 01/12/2006
• Est. Priority Date: 07/12/2004
• Status: Abandoned Application

• Current Assignee: Safran Aircraft Engine Company
• Original Assignee: Snecma Moteurs
• Inventors: Rodrigue, Didier, Catalano, Matthieu, Llorens-Cortes, Dominique, Marie-Agnes, Henri, Crochemore, Yves
• Application Number:
  US10/887,928
• Publication Number:
  US 20060010152A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G06Q 10/06 Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling

Abstract

The present invention relates to management of machine servicing, particularly, but not only, aircraft engine servicing. When a machine is received in a service facility for one of a plurality of predefined reasons, repair and/or maintenance procedures known to correspond to that reason are identified and a workscope defining work to be performed is generated. It is desirable (but not required according to the present invention) to identify what parts and/or tools will be needed to carry out the repair and/or maintenance procedures. It is additionally desirable to permit the parts and/or tools to be ordered or otherwise requested in anticipation of carrying out the defined work. The workscope can be enhanced by taking into account work (required or not) that is customarily performed for a given client. A cost estimate corresponding to the workscope may also be generated, and may also be modified according to client-specific parameters such as the nature of the client'"'"'s service contract

Claims

1. A system for managing service of a machine, comprising:

at least one database for storing;

structural information about the machine;

servicing information relevant to the machine, including at least repair procedures and maintenance procedures relevant to the machine; and

at least one predefined reason for servicing the machine, the stored at least one reason for servicing the machine being linked to at least one of the stored repair procedures and stored maintenance procedures;

an interface for selecting at least one of the stored reasons for servicing the machine; and

a processor constructed and arranged to automatically generate a workscope of work to be performed on the machine, the workscope including one or more of the repair and maintenance procedures selected on the basis of the selected at least one reason for servicing the machine.

2. The system according to claim 1, wherein the at least one database further stores secondary work information corresponding to at least some of the stored repair and maintenance procedures, the secondary work information comprising work that must or should be performed in conjunction with a given stored repair or maintenance procedure, wherein the processor is further constructed and arranged to automatically include in the workscope the secondary work information corresponding to each of the one or more of the selected repair and maintenance procedures.

3. The system according to claim 1, wherein the stored structural information includes machine parts information, the processor being further constructed and arranged to automatically identify any machine part needed in order perform the selected one or more repair and maintenance procedures included in the workscope.

4. The system according to claim 1, wherein the at least one database stores tool information corresponding to the repair and maintenance procedures, the processor being further constructed and arranged to automatically identify any tool necessary for performing the selected one or more repair and maintenance procedures included in the workscope.

5. The system according to claim 2, wherein the at least one database stores cost information corresponding to the repair and maintenance procedures, the processor being further constructed and arranged to automatically determine an estimated cost for performing the selected one or more repair and maintenance procedures included in the workscope.

6. The system according to claim 5, wherein the cost information comprises labor cost information.

7. The system according to claim 6, wherein the labor cost information is empirically based.

8. The system according to claim 5, wherein the at least one database stores client-specific requirements, the processor being constructed and arranged to automatically modify the cost estimate in accordance with the client-specific requirements.

9. The system according to claim 8, wherein the client-specific requirements comprises client contract-defined requirements.

10. The system according to claim 9, wherein the machine is an aircraft engine and the client contract is one of an hours-in-air contract and a time-and-materials contract.

11. The system according to claim 3, further comprising means for requesting the needed machine parts from a machine parts supply source.

12. The system according to claim 4, further comprising means for requesting the needed tools from a tool supply source.

13. The system according to claim 5, further comprising means for transmitting the estimated cost to a client.

14. The system according to claim 3, wherein the at least one database stores tool information corresponding to the repair and maintenance procedures, the processor being further constructed and arranged to automatically identify any tool necessary for performing the selected one or more repair and maintenance procedures included in the workscope,

wherein the at least one database stores cost information corresponding to the repair and maintenance procedures, the machine parts information, and the tool information,

the processor being further constructed and arranged to automatically determine an estimated cost for performing the selected one or more repair and maintenance procedures included in the workscope, including the corresponding tools and parts therefor.

15. The system according to claim 1, comprising means for identifying non-critical machine service related to the selected one or more repair and maintenance procedures included in the workscope, the processor being further constructed and arranged to include the identified non-critical service in the workscope.

16. The system according to claim 1, wherein the at least one database stores an operational history of the machine, the operational history including a service history of the machine.

17. The system according to claim 16, wherein the interface is additionally for inputting a machine identification so that the operational history of the machine can be obtained.

18. The system according to claim 17, comprising means for identifying non-critical machine service related to the service history of the machine.

19. The system according to claim 3, wherein the stored machine parts information is organized in an Illustrated Part Catalog.

20. The system according to claim 1, wherein the interface comprises one or more of a keyboard, a keypad, a touchscreen, and a personal data assistant.

21. The system according to claim 10, wherein the processor is constructed and arranged to generate a workscope using minimal material and labor for a time-and-materials contract.

22. The system according to claim 10, wherein the machine is an aircraft engine, and the processor is constructed and arranged to generate a workscope estimated to maximize a time period between servicing in a hours-in-air contract.

23. The system according to claim 1, wherein the at least one database, the interface, and the processor are embodied in a PC computer.

24. The system according to claim 1 wherein the at least one database and the processor are embodied in at least one computer network server and the interface is embodied in a workstation computer located on the computer network.

25. A method of managing machine servicing, comprising:

identifying one or more reasons for servicing the machine;

based on the identified one or more reasons for servicing, identifying required primary work needed to address the identified one or more reasons for servicing;

generating a workscope defining the work to be performed on the machine, including at least the identified primary work.

26. The method according to claim 25, wherein identifying primary work needed to address the identified one or more reasons for servicing comprises identifying stored repair and/or maintenance procedures corresponding to the identified one or more reasons for servicing.

27. The method according to claim 26, further comprising identifying required secondary work corresponding to the identified primary work, wherein the generated workscope further includes the identified secondary work.

28. The method according to claim 27, further comprising identifying machine parts corresponding to the identified primary and secondary work, wherein the generated workscope includes the identified machine parts.

29. The method according to claim 27, further comprising identifying tools corresponding to the identified primary and secondary work, wherein the generated workscope includes the identified tools.

30. The method according to claim 27, further comprising generating a cost estimate for the identified primary and secondary work.

31. The method according to claim 30, wherein generating a cost estimate comprises modifying an initial cost estimate in view of client contract requirements.

32. The method according to claim 31, wherein the machine is an aircraft engine and the client contract is one of an hours-in-air contract and a time-and-materials contract.

33. The method according to claim 32, wherein modifying the initial cost estimate in view of an hours-in-air contract includes generating a workscope estimated to maximize a time interval between servicing performed on the aircraft engine.

34. The method according to claim 32, wherein modifying the initial cost estimate in view of a time-and-materials contract includes selecting a workscope estimated to minimize time and materials expended during servicing.

35. The method according to claim 25, wherein identifying the primary work needed to address the identified one or more reasons for servicing is additionally based on an operational history of the machine.

36. The method according to claim 35, further including identifying recommended work based upon the operational history of the machine, wherein the workscope further includes the recommended work.

37. The method according to claim 36, wherein identifying recommended work comprises identifying recommended work based on an operational age of the machine.

38. The method according to claim 36, wherein identifying recommended work comprises identifying recommended work based on an operating environment of the machine.

39. The method according to claim 36, wherein identifying recommended work comprises identifying recommended work based on a frequency of operation of the machine.

40. The method according to claim 39, wherein the machine is an aircraft engine and the frequency of operation of the aircraft engine is measured in terms of flight cycles.

41. The method according to claim 37, wherein the machine is an aircraft engine and the operational age of the aircraft engine is measured in terms of hours of operation.

42. The method according to claim 28, further comprising generating a request for the identified machine parts.

43. The method according to claim 29, further comprising generating a request for the identified tools.

44. The method according to claim 30, wherein the cost estimate includes one or more of a cost for parts, a cost labor, and a cost for materials.

45. The method according to claim 30, wherein generating a cost estimate comprises using empirical cost data to generate the cost estimate.

46. The method according to claim 25, further comprising identifying required general work unrelated to the primary and secondary work, wherein the generated workscope includes the required general work.

47. The method according to claim 46, wherein identifying the general work comprises identifying servicing required by governmental regulations.

48. The method according to claim 47, wherein the general work is defined with respect to an operational age of the machine.

49. The method according to claim 46, wherein identifying the general work comprises identifying manufacturer-defined maintenance and/or repair procedures.

50. The method according to claim 27, further comprising filtering out repetitive and/or redundant work actions constituting the primary and secondary work, the workscope comprising the filtered primary and secondary work.

51. An article of manufacture comprising:

a computer-readable medium having computer readable program code thereon for enabling the automatic management of machine servicing, the computer-readable program code comprising;

identifying one or more reasons for servicing the machine;

based on the one or more reasons for servicing the machine, identifying all work procedures for addressing the one or more reasons for servicing the machine;

generating a workscope including the identified work procedures.

52. A method of managing service performed on a client'"'"'s aircraft engine, the method comprising:

identifying one or more reasons for servicing the engine;

identifying work procedures corresponding to the one or more identified reasons for servicing the engine;

narrowing the identified work procedures in accordance with client-specific requirements to obtain a client-specific set of work procedures corresponding to the one or more reasons for servicing the engine;

identifying pending general work procedures applicable to the engine;

narrowing the pending general work procedures down to identify required general work procedures and discretionary general work procedures desired by the client to obtain a client-specific set of general work procedures;

combining the client-specific set of work procedures corresponding to the one or more reasons for servicing the engine and the client-specific set of general work procedures to obtain a combined client-specific set of work procedures;

eliminating redundant and/or repeated work procedures from the combined client-specific set of work procedures;

identifying complimentary work procedures corresponding to the combined client-specific set of work procedures;

identifying the engine parts affected by the combined client-specific set of work procedures and the identified complimentary work procedures; and

generating a workscope comprising the combined client-specific set of work procedures, the identified complimentary work procedures, and the affected engine parts.

53. The method according to claim 52, wherein the general work procedures are defined by regulatory notices.

54. The method according to claim 53, wherein the regulatory notices comprise airworthiness directives.

55. The method according to claim 52, wherein the general work procedures are defined by manufacturer service bulletins.

56. The method according to claim 52, further comprising identifying tools needed to carry out the combined client-specific set of work procedures and the identified complimentary work procedures, wherein generating a workscope further comprises the identified tools.

57. The method according to claim 52, further identifying an estimated cost for the combined client-specific set of work procedures, the identified complimentary work procedures, and the affected engine parts, wherein the workscope comprises the combined client-specific set of work procedures, the identified complimentary work procedures, and the estimated cost therefor.

58. The method according to claim 52, wherein identifying pending general work procedures is at least partly based on an operational history of an individual engine.

59. The method according to claim 58, wherein the operational history of an individual engine comprises a predominant operating environment.

60. The method according to claim 58, wherein the operational history of an individual engine comprises engine age.

61. The method according to claim 60, wherein engine age is measured in terms of operating hours.

62. The method according to claim 60, wherein engine age is measured in terms of flight cycles.