Central maintenance computer system and fault data handling method

• US 4,943,919 A
• Filed: 10/17/1988
• Issued: 07/24/1990
• Est. Priority Date: 10/17/1988
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Aslin, Matthew J., Patton, Gary J.
• Primary Examiner(s): Black, Thomas G.
• Application Number:
  US07/260,985
• Time in Patent Office: 645 Days
• Field of Search: 364/424.01, 364/424.06, 364/507, 364/550, 364/551.01, 364/424.03, 340/945, 371/11
• US Class Current: 701/3
• CPC Class Codes: G07C 5/006 Indicating maintenance
• CPC Class Codes: G07C 5/085 using electronic data carriers

Abstract

The present invention is directed towards an onboard central maintenance computer system integrated into an aircraft system and a system for collecting and analyzing complete maintenance information. The central maintenance computer system (CMCS) collects, consolidates, and reports LRU faults data in order to aid flight crew and maintenance personnel in maintenance procedures. An aircraft system in which the CMCS is used includes a plurality of line replaceable units (LRU), a communication system through which the LRUs can transmit LRU fault data and receiver test initiation commands, and an operator interface device for receiving input commands, displaying data, and communicating with other systems. The central maintenance computer system includes a data transfer system, an input/output processor, a memory device, and a control processing system. During flight, the control processing system controls the collection of complete LRU fault data; generates an isolated fault from the LRU fault data; associates the isolated fault with one of the maintenance messages stored in the memory device; and causes the associated maintenance message to be stored as an active maintenance message in fault history.

Claims

1. An onboard central maintenance computer system for an aircraft system, the aircraft system including:

(a) a plurality of LRUs;

(b) communication means through which the LRUs can transmit LRU fault data and receive test initiation commands; and

(c) an operator interface device including (i) presentation means for presenting maintenance information generated by the central maintenance computer system, (ii) input means for receiving input commands, and (iii) interface communication means for transmitting the input commands and receiving the maintenance information, the central maintenance computer system comprising;

(a) data transfer means for transferring data within said central maintenance computer system;

(b) input/output means coupled to the data transfer means, and coupled to the communication means and to the interface communication means for receiving and transmitting data therebetween;

(c) memory means coupled to said data transfer means for storing data including a plurality of preestablished maintenance messages; and

,

(d) control processing means coupled to said data transfer means for controlling the transfer and processing of data within said central maintenance computer system and for controlling the operations of said input/output means and said memory means, said control processing means including;

a collection module for causing said input/output means to collect the LRU fault data via the communication means; and

a consolidation module for generating an active maintenance message from the LRU fault data by screening out cascaded faults and consolidating multiple faults to produce an isolated fault, associating said isolated fault with one of said maintenance messages, termed active maintenance message, in said memory means, and causing said active maintenance message to be identified in said memory means.

2. A central maintenance computer system in accordance with claim 1, wherein the communication means further includes an LRU control system for monitoring and testing controlled LRUs, and for generating controlled LRU fault data, and a fault collection device coupled to the LRU control system for receiving the controlled LRU fault data, and wherein said collection module includes an indirect module for controlling the communication means such that controlled LRU fault data is transmitted from the fault collection device to said input/output means and a direct module for controlling the communication means such that LRU fault data is transmitted directly from noncontrolled LRUs, which are not monitored or tested by said LRU control system, to said input/output means.

3. A central maintenance computer system, in according with claim 2, wherein said central maintenance computer system further includes a data selection module in the fault collection device for selecting which controlled LRU fault data is received by the fault collection device.

4. A central maintenance computer system in accordance with claim 1, further comprising an output module for causing, in response to an input command indicative display request received by said input/output means, said active maintenance message to be transmitted as maintenance information from the memory means to the interface communication means, whereby said maintenance message is presented by the operator interface device for analysis.

5. A central maintenance computer system in accordance with claim 4, wherein:

the fault collection device further includes flight deck effect means for generating a flight deck effect indicative of an LRU fault in response to the LRU fault data;

said indirect module further causes the flight deck effect to be transmitted from the fault collection device to said input/output means;

said control processor means further includes a correlation module for correlating the flight deck effect with one of said active maintenance messages, and for causing said correlated flight deck effect to be stored in said memory means in association with said active maintenance message; and

said output module further causes the correlated flight deck effect and maintenance message to be transmitted to the interface communication means as the maintenance information.

6. A central maintenance computer system in accordance with claim 5, wherein each of said preestablished maintenance messages is stored in said memory means in association with possible flight deck effect data, and wherein said correlation module, in order to correlate the flight deck effect received from the fault collection device with an active maintenance message, attempts to correlate the flight deck effect so received to said possible flight deck effect data associated with each of said active maintenance messages.

7. A central maintenance computer system in accordance with claim 4, wherein said output module, in response to an input command indicative of an input monitoring request received via said input/output means, causes the collected LRU fault data for the specified LRU to be formatted in a predetermined display format, and to be transmitted via said input/output means to the interface communication means as the maintenance information, whereby the LRU status can be interactively monitored via the operator interface device.

8. A central maintenance computer system in accordance with claim 4, wherein said memory means includes an airline data base including airline messages, and said output module includes means for associating an airline message with an active maintenance message in said memory means, and for causing the associate airline message to be transmitted via said input/output means to the interface communication means in conjunction with said active maintenance message.

9. A central maintenance computer system in accordance with claim 4, wherein the operator interface device includes an ACARS interface for transmitting and receiving digital data between the aircraft system and the ground, and wherein said output module, in response to an input command indicative of an ACARS output request received via the input/output means, causes said active maintenance message to be formatted in ACARS format and causes said formatted maintenance message to be transmitted to the interface communication means via said input/output means, whereby the maintenance message is transmitted via the operator interface device to the ground for operator analysis.

10. A central maintenance computer system in accordance with claim 1, wherein said control processing means further includes a test module for (i) causing, in response to an input command indicative of an LRU test initiation request received via said input/output means, a test initiation request to be transmitted to the LRU specified in the command, (ii) in response to a test complete signal generated by the LRU, determining the test results, and (iii) causing the test results to be transmitted to the interface communication means as the maintenance information, whereby the central maintenance computer system acts as a test interface device between the operator and the LRU.

11. A central maintenance computer system in accordance with claim 10, wherein said memory means includes a test result data base of LRU fail conditions, a fail condition being true if the LRU condition occurs during the testing period, and wherein said test module, in order to determine said test results, determines whether any of the fail conditions match an active maintenance message generated by the consolidation module during the testing period, and, if there is a match, causes a fail message to be transmitted to the interface communication means, and, upon receipt of an input command indicative of a test result display command, causes the matched active maintenance message to be transmitted to the interface communicaton means, whereby said maintenance message provides the operator with an explanation of the test results.

12. A central maintenance computer system in accordance with claim 1, wherein each of said preestablished maintenance messages is stored in said memory in association with a combinatory logic phrase including operating parameters such as LRU states, flight legs and time delays, and logical connectors, wherein the aircraft system generates data indicative of the operating parameters, wherein said collection module causes said input/output means to collect data indicative of the operating parameters, and wherein said consolidation module matches the LRU fault data and operating parameters with the combinatory logic phrases in said memory means and, if a combinatory logic phrase is matched, the associated maintenance message, termed active maintenance message, is identifying in said memory means.

13. A central maintenance computer system in accordance with claim 1, wherein said input/output means includes an automated test equipment (ATE) connector for coupling ATE to said central maintenance computer system, and transmitting the correlated flight deck effect along with said active maintenance message to the interface communication means as the maintenance information.

14. A method for centralized fault handling in an aircraft system, the aircraft system including:

(a) a plurality of LRUs;

(b) communication means through which the LRUs can transmit LRU fault data and receive test initiation commands;

(c) an operator interface device including (i) presentation means for presenting maintenance information generated by the central maintenance computer system, (ii) input means for receiving input commands, and (iii) interface communication means for transmitting the input commands and receiving the maintenancee information; and

(d) a central maintenance computer system including;

(i) input/output means for receiving and transmitting data between the central maintenance computer system and other aircraft system components;

(ii) memory means for storing data including a plurality of preestablished maintenance messages;

(iii) control processing means for controlling the transfer and processing of data within said central maintenance computer system and for controlling the operations of said input/output means and said memory means, said method comprising;

(a) collecting a complete set of LRU fault data at the input/output means via the communication means; and

(b) generating, in response to the LRU fault data and the preestablished maintenance messages, an active maintenance message by screening out cascaded faults and consolidating multiple faults to produce an isolated fault, associating said isolated fault with one of the preestablished maintenance messages, termed active maintenance message, and causing said active maintenance message to be identified in said memory means.

15. The method for centralized fault handling in accordance with claim 14, further comprising the step of transmitting the active maintenance message as maintenance information from the memory means to the interface communication means, whereby said maintenance message is presented by the operator interface device for analysis.

16. The method of centralized fault handling in accordance with claim 15, wherein a component in the aircraft system generates a flight deck effect indicative of an LRU fault, and wherein the step of collecting a complete set of LRU fault data includes the step of collecting the flight deck effect, and the fault handling method further includes the steps of:

correlating the flight deck effect with one of said active maintenance messages;

storing said correlated flight deck effect in said memory means in association with said active maintenance message; and

wherein said control processing means further includes a test module for causing, in response to an input command indicative of an ATE LRU test initiation request received via said input/output means, a test initiation request to be transmitted to the LRU, and, in response to a test complete signal generated by the LRU, determining the test results and causing the test results to be transmitted to the ATE via said input/output means, whereby the central maintenance computer system acts as an ATE interface between the operator and the LRU.

17. The method for centralized fault handling in accordance with claim 16, wherein:

each of said preestablished maintenance messages is stored in association with a flight mode;

a preestablished flight deck effect data base is stored in said memory means, said data base including flight deck effects in association with flight modes;

the aircraft system generates data indicative of operating parameters such as flight mode; and

wherein

said step of collecting said LRU fault data includes the step of collecting said fight modes;

said step of generating an active maintenance message includes the step of determining whether said flight mode corresponds to the maintenance message in the maintenance message data base, and causing said maintenance message to be stored in said memory means as an active maintenance messagee if said flight mode corresponds thereto;

said step of collecting the flight deck effect includes the step of determining whether said flight mode corresponds to the flight deck effect in the flight mode data base; and

said step of correlating the flight deck effect is carried out if the flight mode corresponds to the flight deck effect.

18. The method for centralized fault handling in accordance with claim 14, wherein each of said preestablished maintenance messages is stored in said memory means in association with a combinatory logic phrase, wherein the aircraft system generates data indicative of the operating parameters, wherein:

said step of collecting complete LRU fault data includes collecting the data indicative of the operating parameters;

said step of generating an active maintenance message includes the step of matching the collected LRU fault data andd operating parameters with the combinatory logic phrases in said memory means and, if a combinatory logic phrase is matched, identifying the associated maintenance message, termed active maintenance message, in the memory means.