Engine fault diagnostic system

• US 5,408,412 A
• Filed: 04/09/1992
• Issued: 04/18/1995
• Est. Priority Date: 04/09/1992
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Hogg, George W., Wright, Brian D., Carron, Karen A., Stambaugh, Craig T. Sr.
• Primary Examiner(s): Chin, Gary
• Application Number:
  US07/865,428
• Time in Patent Office: 1,104 Days
• Field of Search: 364/424.03, 364/424.04, 364/431.01, 364/431.11, 364/550, 364/551.01, 73/117.2, 73/117.3, 340/438, 340/439
• US Class Current: 701/33
• CPC Class Codes: G01M 15/05 by combined monitoring of two or more different engine parameters

Abstract

A diagnostic system for use in troubleshooting malfunctions in an aircraft engine control system receives sensor data obtained during a flight. The sensor data is supplemented by signals indicative of the operation of the engine control system'"'"'s computer. The combined data is downloaded to the diagnostic system. Included in the diagnostic system is an inference engine and knowledge database. The diagnostic system includes a computer for executing a plurality of algorithms by means of the inference engine using the downloaded data and knowledge database as input to aid the technician in correctly determining the source of malfunctions in a minimum of time. The diagnostic system is capable of processing "unknown" responses to diagnostic system inquiries and can retrocede a step or steps during the execution of diagnostic system algorithms.

Claims

1. A system for use in diagnosing a malfunction in an aircraft engine from engine sensor signals including signals corresponding to engine faults, said system comprising:

a diagnostic supervisory signal generator means for generating system command signals;

an input/output device for receiving signals from and sending signals to a technician;

a knowledge memory means having stored therein signals corresponding to a database of engine sensor signal values and facts and rules relating each of said engine sensor signal values and facts with selected ones thereof, each of said rules including a logical premise and conclusion;

an inference engine means for receiving said knowledge memory means signals and, in response to said system command signals, for performing an inference engine test to establish the cause of the engine faults and generating signals indicative thereof, said inference engine test including the steps of;

determining from said engine sensor signals a first series of rules to be tested;

searching said knowledge memory means for signals corresponding to one of said engine sensor signal values and facts that establishes the validity of a first rule conclusion;

generating signals for said input/output means for querying said technician for input signals that establishes the validity of said first rule conclusion;

receiving signals from said input/output means indicative of technician input signals;

inferring the value of a first rule premise signal corresponding to a first rule premise associated with said first rule conclusion in dependence on the establishment of the validity of said first rule conclusion,

determining a second series of rules to be tested in dependence on said first rule premise signal value; and

a retroceding means for receiving a signal indicative of an erroneous input signal and, in response thereto, determining all of said first rule conclusion and premise signal values established as a result of said erroneous input signal;

said retroceding means further for removing all the erroneously established signal values from said knowledge database.

2. The diagnostic system of claim 1 wherein said inference engine test further comprises the steps of:

selecting a subsequent rule conclusion; and

generating signals corresponding to the value of said subsequent rule conclusion and inferring therefrom the values of signals corresponding to an associated subsequent rule premise.

3. The diagnostic system of claim 1 further comprising a metafact memory means having stored therein signals corresponding to aircraft engine sensor signal value related metafacts and wherein said inference engine test further comprises the steps of searching said metafact memory means for signals corresponding to one of said metafacts and generating signals for said input/output means for prompting the technician for a value therefor.

4. The diagnostic system of claim 1 further comprising a data preparatory means for receiving said engine sensor signals and generating therefrom signals in a preselected data format.

5. The diagnostic system of claim 1 wherein said knowledge database is divided into a plurality of knowledge database portions, and said diagnostic system further comprises a means for moving a selected one of said knowledge database portions into a computer memory means for communicating with said diagnostic system.

6. The diagnostic system of claim 1 further comprising a means for suspending operation of said diagnostic supervisory signal generator means at a selected one of said steps and returning thereto directly after a suspension of test.

7. The diagnostic system of claim 1 further comprising a log memory means for storing signals indicative of engine faults in previous sets of said aircraft engine sensor signals and comprising a means for generating signals for said input/output means indicative of said engine fault signals stored in said log memory means.

8. The diagnostic system of claim 1 further comprising a memory means for storing signals indicative of events processed during said inference engine test.

9. The diagnostic system of claim 1 further comprising a memory means for storing signals corresponding to aircraft engine components generating said fault signals, said input/output means further comprising display means configured to present said aircraft engine component signals to said technician in response to said system command signals presented therefrom.

10. The diagnostic system of claim 9 wherein said aircraft engine component signals further comprise signals corresponding to electrical representations of schematic diagrams of aircraft electrical circuits.

11. The diagnostic system of claim 1 further comprising a memory means for determining the temporal order of said engine fault signals and a means for establishing an order of the testing thereof in dependence on said temporal order.

12. The diagnostic system of claim 1 wherein said knowledge database means further comprises a means for determining which of said engine fault signals are indicative of independent and dependent type of engine faults and comprising a means for establishing an order of the testing thereof in dependence on said determination.

13. The diagnostic system of claim 12 further comprising a means for testing only said engine fault signals determined to be indicative of said independent type engine faults.

14. The diagnostic system of claim 12 further comprising a means for determining the temporal order of signals indicative of first and second independent engine faults and for establishing an order of the testing thereof in dependence thereon.

15. The diagnostic system of claim 1 wherein said retroceding means generates a third series of rules to be tested, the rules of said third series being selected in dependence on said removed values.

16. The diagnostic system of claim 1 wherein said retroceding means is disabled should said inference engine test be suspended.

17. The diagnostic system of claim 1 wherein said retroceding means is disabled should said inference engine test be terminated.

18. The diagnostic system of claim 1 further comprising an expert system shell (ESS) for receiving said system command signals, generating therefrom signals to control the operation of said inference engine, and providing a cache memory means for storing test result signals.

19. The diagnostic system of claim 1 wherein said inference engine means test further comprises the steps of inferring the values of signals corresponding to a second rule premise in dependence on the establishment of said first rule conclusion.