Lifetime support process for rapidly changing, technology-intensive systems

• US 20060217929A1
• Filed: 08/08/2005
• Published: 09/28/2006
• Est. Priority Date: 08/06/2004
• Status: Abandoned Application

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Feeley, Michael E., VanBuskirk, David J., Gellen, Jack, Gruenloh, Eric V., Herald, Thomas E. Jr.
• Application Number:
  US11/199,573
• Publication Number:
  US 20060217929A1
• Time in Patent Office: Days
• US Class Current: 702/184
• CPC Class Codes: B63B 71/00 Designing vessels; Predicting their performance
• CPC Class Codes: G21D 3/00 Control of nuclear power plant control of nuclear reaction in general G21C7/00
• CPC Class Codes: Y02E 30/00 Energy generation of nuclear origin
• CPC Class Codes: Y02E 30/30 Nuclear fission reactors

Abstract

A system is operable without repair for a predetermined maintenance-free operating period (MFOP). The system includes a first portion that is operable to perform a function, a second portion, and a control portion coupled to the first and second portions. The control portion is operable to cause the second portion to perform the function for a remainder of the MFOP if the first portion fails during the MFOP. For example, a system on board a submarine that comes in to port every ninety days can have a ninety-day MFOP. Therefore, crewmembers do not need to repair the system while the submarine is at sea on a mission. This servicing strategy may reduce costs by allowing one to eliminate training crew to repair the sonar system, preparing and printing repair documentation for the crew, and carrying this documentation, spare parts, and repair equipment on board the submarine.

Claims

1. A system operable for a predetermined period of time without maintenance, the system comprising:

a first portion operable to perform a function;

a second portion; and

a control portion coupled to the first and second portions and operable to cause the second portion to perform the function for a remainder of the predetermined period if the first portion fails during the predetermined period.

2. The system of claim 1 wherein the predetermined period comprises an integer multiple of a mission duration of a vessel on which the system is disposed.

3. The system of claim 1 wherein the control portion is operable to detect a failure that renders the first portion unable to perform the function and to cause the second portion to perform the function in response to detecting the failure.

4. The system of claim 1, further comprising:

a third portion coupled to the control portion; and

wherein the control portion is operable to cause the third portion to perform the function for a remainder of the predetermined period if the first and second portions fail during the predetermined period.

5. A method, comprising:

operating a system for a predetermined period of time without performing maintenance to the system; and

if a first portion of the system performing a function fails during the predetermined period, then causing a second portion of the system to perform the function for a remainder of the predetermined period.

6. The method of claim 5 wherein:

the system is disposed on a vessel; and

the predetermined period comprises an integer multiple of a mission duration of the vessel.

7. The method of claim 5, further comprising:

wherein the system is disposed on a vessel; and

carrying on the vessel no spares for any part of the system.

8. The method of claim 5, further comprising repairing the first portion of the system after the predetermined period ends if the first portion fails during the predetermined period.

9. The method of claim 8 wherein:

the first portion of the system includes a part of a part generation; and

repairing the first portion comprises replacing the part with a part of the same generation.

10. The method of claim 8 wherein:

the first portion of the system includes a part of a part generation; and

repairing the first portion comprises refreshing the first portion by replacing the part with a part of a later part generation.

11. The method of claim 8 wherein:

the first portion of the system includes a number of parts of respective part generations and has a capacity for performing the function; and

repairing the first portion of the system comprises refreshing the first portion of the system by replacing the parts with fewer later-generation parts such that after the repairing, the first portion of the system has substantially the same capacity for performing the function as before the repairing.

12. The method of claim 8 wherein:

the first portion of the system includes a first number of parts of respective part generations and has a capacity for performing the function; and

repairing the first portion of the system comprises inserting new technology into the first portion of the system by replacing the parts with a second number of later-generation parts such that after the repairing, the first portion of the system has a greater capacity for performing the function than before the repairing.

13. The method of claim 12 wherein the second number is less than or equal to the first number.

14. The method of claim 5, further comprising causing a third portion of the system to perform the function for the remainder of the predetermined period if the first and second portions of the system fail during the predetermined period.

15. The method of claim 5, further comprising refreshing the system at an interval that is an integer multiple of the predetermined period.

16. The method of claim 5, further comprising inserting technology into the system at an interval that is an integer multiple of the predetermined period.

17. An apparatus, comprising:

a first system that is operable to perform a first function and that is repairable only during predetermined maintenance periods;

a second system; and

a control system coupled to the first and second systems and operable to cause the second system to perform the first function until the next predetermined maintenance period if the first system fails between maintenance periods.

18. The apparatus of claim 17 wherein:

the second system is operable to perform a second function; and

the control-system is operable to cause the second system to perform the first and second functions until the next predetermined maintenance period if the first system fails between maintenance periods.

19. The apparatus of claim 17 wherein a duration between consecutive maintenance periods comprises an integer multiple of a mission duration of the apparatus.

20. The apparatus of claim 17 wherein the first system comprises an electronic part.

21. The apparatus of claim 17 wherein the first system, the second system, and the control system are parts of a same system.

22. A method, comprising:

detecting a failure of a system between predetermined maintenance periods;

if the system was performing a task before the failure, then performing the task without the system until a next predetermined maintenance period; and

repairing the system during the next predetermined maintenance period.

23. The method of claim 22 wherein the failure comprises a failure of a part of the system.

24. The method of claim 22 wherein:

the system is disposed on a vessel; and

the predetermined maintenance periods coincide with times during which the vessel is in respective predetermined locations.

25. The method of claim 22 wherein:

the system includes a part of a part generation; and

repairing the system comprises replacing the part with a part of the same generation.

26. The method of claim 22 wherein:

the system includes a part of a part generation; and

repairing the system comprises replacing the part with a part of a later generation.

27. The method of claim 22 wherein:

the system includes a number of parts of respective part generations and has a functional capacity; and

repairing the system comprises replacing the parts with fewer subsequent-generation parts such that after the repairing, the system has substantially the same functional capacity.

28. The method of claim 22 wherein:

the system includes a first number of parts of respective part generations and has a functional capacity; and

repairing the system comprises replacing the parts with a second number of subsequent-generation parts such that after the repairing, the system has an increased functional capacity.

29. The method of claim 22 wherein the second number is less than or equal to the first number.

30. A method, comprising:

operating a system for a predetermined period of time without performing maintenance to the system;

if a first portion of the system performing a function fails during the predetermined period, then causing a second portion of the system to perform the function for a remainder of the predetermined period; and

refreshing the first portion of the system after the predetermined period of time, the refreshing causing the first portion to be repaired if the first portion failed during the predetermined period of time.

31. A method, comprising:

designing a system to have predetermined maintenance-free operability periods; and

scheduling technology refreshes of the system at intervals that are no longer than the respective maintenance-free operability periods.

32. The method of claim 31, further comprising scheduling technology insertions to the system to occur simultaneously with at least some of the technology refreshes.

33. The method of claim 31 wherein scheduling the technology refreshes further comprises synchronizing the technology refreshes with the maintenance-free operating periods.

34. A method, comprising:

designing a system to have predetermined maintenance-free operability periods; and

scheduling technology insertions to the system at intervals that are no longer than the respective maintenance-free operability periods.

35. The method of claim 34 wherein scheduling the technology insertions further comprises synchronizing the technology insertions with the maintenance-free operating periods.