Long and short range storage and transmission system on aircraft parts
According to one embodiment, an aircraft part storage system includes a first storage device and a second storage device. The first storage device is configured to be coupled to an aircraft part and operable to store and transmit a first set of information about the aircraft part. The second storage device is configured to be coupled to the same aircraft part and operable to store and transmit a second set of information about the aircraft part. The second storage device has a larger storage capacity than the first storage device but a shorter transmission range than the first storage device.
1. A rotorcraft, comprising:
a body;
a power train coupled to the body and comprising a power source and a drive shaft coupled to the power source;
a hub;
a rotor blade coupled to the hub;
an aircraft part;
an aircraft part storage system comprising:
a first storage device comprising a radio frequency identification tag coupled to the aircraft part and operable to store and transmit a first set of information identifying the aircraft part; and
a second storage device comprising a contact memory button coupled to the same aircraft part and operable to store and transmit a second set of information about the aircraft part, the second storage device having a larger storage capacity than the first storage device but a shorter transmission range than the first storage device;
a vibration sensor coupled to the rotorcraft proximate to the aircraft part and configured to measure and transmit vibration load data to the second storage device, wherein the second set of information about the aircraft part comprises the vibration load data; and
an aircraft part information system comprising:
a first data repository operable to receive the first set of information about the aircraft part from the first storage device;
a second data repository operable to receive the second set of information about the aircraft part from the second storage device; and
a correlation engine operable to correlate information between the first data repository and the second data repository.
2. The rotorcraft of claim 1 , wherein the first set of information identifying the aircraft part comprises a part number unique to a category of parts.
3. The rotorcraft of claim 1 , wherein the first set of information identifying the aircraft part comprises a serial number unique to the individual aircraft part.
4. The rotorcraft of claim 1 , wherein the second set of information about the aircraft part further comprises a maintenance history of the aircraft part.
5. The rotorcraft of claim 1 , further comprising an environmental condition sensor coupled to the rotorcraft proximate to the aircraft part and configured to transmit information about at least one aspect of a natural environment to which the aircraft is subject, to the second storage device,
wherein the second set of information about the aircraft part further comprises the information about at least one aspect of a natural environment to which the aircraft is subject.
6. An aircraft part storage system comprising:
a first storage device comprising a radio frequency identification tag, configured to be coupled to an aircraft part, and operable to store and transmit a first set of information about the aircraft part;
a second storage device comprising a contact memory button, configured to be coupled to the same aircraft part, and operable to store and transmit a second set of information about the aircraft part, the second storage device having a larger storage capacity than the first storage device but a shorter transmission range than the first storage device;
a vibration sensor coupled to the rotorcraft proximate to the aircraft part and configured to measure and transmit vibration load data to the second storage device, wherein the second set of information about the aircraft part comprises the vibration load data; and
an aircraft part information system comprising:
a first data repository operable to receive the first set of information about the aircraft part from the first storage device;
a second data repository operable to receive the second set of information about the aircraft part from the second storage device; and
a correlation engine operable to correlate information between the first data repository and the second data repository.
7. The aircraft part storage system of claim 6 , wherein the first set of information about the aircraft part comprises information identifying the aircraft part.
8. The aircraft part storage system of claim 7 , wherein the information identifying the aircraft part comprises a part number unique to a category of parts.
9. The aircraft part storage system of claim 7 , wherein the information identifying the aircraft part comprises a serial number unique to the individual aircraft part.
10. The aircraft part storage system of claim 6 , wherein the second set of information about the aircraft part further comprises a maintenance history of the aircraft part.
11. The aircraft part storage system of claim 6 , wherein the second set of information about the aircraft part further comprises an environmental history of the aircraft part.
12. The aircraft part storage system of claim 6 , further comprising an environmental condition sensor coupled to the rotorcraft proximate to the aircraft part and configured to transmit information about at least one aspect of a natural environment to which the aircraft is subject, to the second storage device,
wherein the second set of information about the aircraft part further comprises the information about at least one aspect of a natural environment to which the aircraft is subject.
13. The aircraft part storage system of claim 6 , wherein the first data repository is operable to store the first set of information about the aircraft part as a set of aircraft configuration data.
14. The aircraft part storage system of claim 13 , wherein the set of aircraft configuration data comprises one or more serial numbers corresponding to aircraft parts installed on an aircraft over a period of time.
15. The aircraft part storage system of claim 13 , wherein the set of aircraft configuration data comprises serial numbers corresponding to aircraft parts installed on multiple aircraft over a period of time.
16. The aircraft part storage system of claim 6 , wherein the second set of information about the aircraft part further comprises a set of part history data.
17. The aircraft part storage system of claim 16 , wherein the set of part history data comprises a maintenance history for at least one aircraft part.
18. The aircraft part storage system of claim 16 , wherein the set of part history data comprises an environmental history for at least one aircraft part.
19. The aircraft part storage system of claim 6 , wherein:
the first data repository is operable to store the first set of information about the aircraft part as a set of aircraft configuration data;
the second set of information about the aircraft part further comprises a set of part history data; and
the correlation engine is operable to identify an aircraft corresponding to at least one aircraft part at a time reflected in the part history data.
20. The aircraft part storage system of claim 6 , wherein:
the first data repository is operable to store serial numbers corresponding to aircraft parts installed on multiple aircraft over a period of time;
the second data repository is operable to store a maintenance history for at least one aircraft part; and
the correlation engine is operable to identify an aircraft corresponding to the at least one aircraft part at the time of a maintenance event reflected in the maintenance history of the at least one aircraft part.
21. The aircraft part storage system of claim 6 , wherein:
the first data repository is operable to store serial numbers corresponding to aircraft parts installed on multiple aircraft over a period of time;
the second data repository is operable to store an environmental history for at least one aircraft part; and
the correlation engine is operable to identify an aircraft corresponding to the at least one aircraft part at the time of an environmental event reflected in the environmental history of the at least one aircraft part.
22. The aircraft part storage system of claim 12 , wherein the environmental condition sensor comprises a sacrificial sensor.
23. The aircraft part storage system of claim 12 , wherein the environmental condition sensor comprises a salinity sensor.
24. The aircraft part storage system of claim 12 , wherein the environmental condition sensor comprises a corrosivity sensor.
25. The aircraft part storage system of claim 12 , wherein the environmental condition sensor comprises a particulate sensor.
26. The aircraft part storage system of claim 12 , wherein the environmental condition sensor comprises a pressure sensor.