Integrated aircraft test system

• US 5,111,402 A
• Filed: 01/19/1990
• Issued: 05/05/1992
• Est. Priority Date: 01/19/1990
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Brooks, David K., Gross, Larry E., Waun, Cindy M.
• Primary Examiner(s): Chin, Gary
• Application Number:
  US07/467,772
• Time in Patent Office: 837 Days
• Field of Search: 364/424.01, 364/424.03, 364/424.04, 364/431.01, 364/578, 364/579, 364/580, 364/550, 364/551.01, 324/73.1, 371/15.1, 371/25.1, 371/26, 371/27, 371/71, 73/117.2
• US Class Current: 701/35
• CPC Class Codes: G01R 31/008 on air- or spacecraft, railway rolling stock or sea-going vessels

Abstract

An integrated aircraft system for funtionally testing the components and subsystems of an aircraft during its manufacture and subsequent maintenance. A central control unit serves as a repository for test applications and instruction sets that comprise the individual steps of the functional tests performed on the aircraft. In response to receiving indications of work performed on the aircraft, the central control unit displays an indication of the functional tests that should be performed on the aircraft. The system includes a plurality of automated test equipment carts (ATEs). Each of the ATEs contains a number of processor-controllable instruments for performing functional tests on specific components and subsystems that comprise a specific aircraft system. A system controller on each of the ATEs controls the operation of the test instruments associated therewith. The system controllers are also capable of directing the broadcast of simulation data to aircraft components so that the response of the components to the stimulation data can be tested. Test application from the central control unit are run on the system controller of each ATE contain instructions that direct the system controller to perform specific functional tests on the aircraft using test instruments and to store the test results in a system controller memory associated therewith. The ATEs are selectiively connected to the central control unit having a main memory so that the test results results stored in the system controller memory may be unloaded and permanently archieved. A remote access terminal also connectable to the central control unit is also provided so that personnel can receive instructions for manual tests and be provided with a means for entering the test results into the system. The central control unit reviews the results of the functional tests performed on the aircraft and broadcasts appropriate messages if functional tests were missed or failed, or the aircraft passed functional testing.

Claims

1. An integrated aircraft test system for functionally testing a plurality of aircraft components and subsystems, wherein at least one of the aircraft components and subsystems operates in response to data broadcast from another one of the aircraft components, and wherein during functional testing of said one of the aircraft components and subsystems, simulation data are broadcast thereto, said test system comprising:

(a) at least two automated test equipment carts for performing functional tests on different aircraft components and subsystems, at least one said cart having instruments for functionally testing the at least one aircraft component and subsystem that operates in response to data broadcast by another of the one of the aircraft components, each of said carts including;

a plurality of processor controllable instruments for performing functional tests on specific aircraft components and subsystems;

connection means for interconnecting said instruments to the components and subsystems that said instruments functionally test; and

a system controller connected to said instruments for controlling said instruments and having an input/output unit, said system controller controlling the functional test of said at least one aircraft component and subsystem by said instruments and including means for receiving and storing the results of the functional test from said instruments, said system controller input/output unit of said automated test equipment cart having said instruments for performing functional testing on the at least one aircraft component and subsystem that operates in response to the simulation data broadcast from the another aircraft component further being connected to said connection means so that said system controller can control the broadcast of the simulation data to the at least one aircraft component and subsystem through data transmissions over said connection means; and

(b) a central control unit including a memory, said central control unit adapted for connection to said system controller input/output units for reading said stored test results therefrom and for storing said test results in said central control unit memory.

2. The integrated aircraft test system claim 1, wherein each said system controller includes at least two test applications, each said test application comprising a set of system controller-executable instructions directing said system controller to perform a functional test with said instruments associated therewith, said test applications containing instructions directing said system controller to perform different functional tests.

3. The integrated aircraft test system of claim 1, wherein each said automated test equipment cart further includes:

at least one signal interface cable associated with said cart, having a plurality of connector elements for establishing separate conductive links to the aircraft components and subsystems;

a processor controllable switch matrix connected to said test instruments and said signal interface conductive elements for selectively establishing conductive interconnections between said instruments and said signal interface cable conductive elements; and

wherein said system controller is connected to said switch matrix and is operative to control said conductive interconnections established thereby during the functional tests.

4. The integrated aircraft test system of claim 2, wherein each automated test equipment cart further includes:

at least one signal interface cable associated with said cart, having a plurality of conductive elements for establishing separate conductive links to the aircraft components and subsystems;

a processor controllable switch matrix connected to said test instruments and said signal interface conductive elements, for selectively establishing conductive interconnections between said instruments and said signal interface cable conductive elements;

said system controller being connected to said switch matrix for controlling said conductive interconnections established thereby; and

said test applications further containing instructions directing said system controller to control said switch matrix so that selected electrical interconnections are established during each functional test.

5. The integrated aircraft test system of claim 1, wherein a plurality of aircraft components and subsystems operate in response to data broadcasts by separate aircraft line-replaceable units, and during functional testing of at least two of the aircraft components and subsystems, the simulation data are broadcast thereto by at least one of the line-replaceable units, and wherein:

said connection means associated with said automated test equipment cart having instruments for functionally testing the aircraft components and subsystems to which the simulation data is broadcast configured to interconnect said automated test equipment cart and the aircraft line-replaceable unit; and

the input-output unit of said automated test equipment cart is connected to said connection means so that said system controller can control the broadcast of the simulation data to the aircraft line-replaceable unit through data transmission over said connection means.

6. The integrated aircraft test system of claim 5, wherein the line-replaceable unit that broadcasts the simulation data is connected to an on-aircraft central maintenance processor that controls the broadcast of the simulation data;

said system further including;

a plurality of said automated test equipment carts for functionally testing the aircraft components and subsystems, which during the functional testing thereof receive the simulation data, each said cart having a central maintenance processor cable for providing a communications link between the central maintenance processor and the associated system controller; and

wherein

each said system controller is operative to control the broadcast of the simulation data by the line-replaceable unit through data transmission to the central maintenance processor over said central maintenance processor cable.

7. The integrated aircraft test system of claim 6, wherein each said system controller includes at least one test application comprising a set of system controller-executable instructions directing said system controller to perform a functional test with said instruments associated therewith.

8. The integrated aircraft test system of claim 7, wherein each said system controller further includes at least two test applications containing instructions directing said system controller to perform different functional tests, and at least one of said applications on at least one said automated test equipment cart having said instruments for functionally testing the aircraft components and subsystems that operate in response to data broadcast by another aircraft component is a set of instructions for performing a functional test on the aircraft component or subsystem that during the testing thereof receives the simulation data, said test application further containing instructions that direct said automated test equipment cart system controller to operatively control the broadcast of the simulation data during the functional test.

9. The integrated aircraft test system of claim 7, wherein each said automated test equipment cart further includes:

at least one signal interface cable associated with said cart, having a plurality of connector elements for establishing separate conductive links to the aircraft components and subsystems;

a processor-controllable switch matrix for selectively establishing conductive interconnections between said cart instruments and said signal interface cable conductive elements;

said system controller being connected to said switch matrix for controlling said electrical connections established thereby; and

wherein

said at least one test application further includes instructions that said system controller executes to control said switch matrix so that said electrical connections are established during each said functional test.

10. The integrated aircraft test system of claim 9 further including:

a central control unit including a memory, said central control unit being adapted for connection to said system controllers for reading and storing test results in said central control unit memory.

11. The integrated aircraft test system of claim 4, wherein one said automated test equipment cart includes instruments for testing the components and subsystems associated with a flight controller system on the aircraft, and said test applications associated with said cart direct said system controller associated with said cart to perform flight controller component and subsystem functional tests with said instruments.

12. The integrated aircraft test system of claim 4, wherein one of said automated test equipment carts includes instruments for testing components and subsystems associated with an avionics system on the aircraft, and said test applications associated with said cart direct said system controller associated with said cart to perform functional tests on the components and subsystems of the aircraft avionics system.

13. The integrated aircraft test system of claim 4, wherein one of said automated test equipment carts includes test instruments for performing functional tests on the components and subsystems associated with an engine system on the aircraft, and said test applications associated with said one cart direct said system controller associated with said one cart to perform functional tests on the components and subsystems of the aircraft engine system.

14. The integrated aircraft test system of claim 4, wherein one of said carts includes instruments for functionally testing the components and subsystems associated with a power system on the aircraft, and said test applications associated with said one cart direct said system controller associated with said one cart to perform functional tests on the components and subsystems of the aircraft power system.

15. The integrated aircraft test system of claim 6, wherein one of said automated test equipment carts includes test instruments for functionally testing the components and subsystems associated with a flight controller system on the aircraft, and said test applications associated with said one cart direct said system controller to perform functional tests on the components and subsystems associated with the flight controller system.

16. The integrated aircraft test system of claim 6, wherein one of said automated test equipment carts includes instruments for testing the components and subsystems associated with an avionics system on the aircraft, and said test applications associated with said one cart direct said system controller associated with said one cart to perform functional tests on the components and subsystems associated with the avionics system.

17. The integrated aircraft test system of claim 6, wherein one of said automated test equipment carts includes instruments for performing functional tests on the components and subsystems associated with an engine system on the aircraft, and said test applications associated with said one cart direct said system controller associated with said one cart to perform functional tests on the components and subsystems of the engine system.

18. The integrated aircraft test system of claim 6, wherein one of said automated test equipment carts includes instruments for testing the components and subsystems associated with a power system on the aircraft, and said test applications associated with said one cart direct said system controller associated with said one cart to perform functional tests on the components and subsystems associated with the aircraft power system.

19. An automated test equipment cart for functionally testing a plurality of aircraft components and subsystems, at least one of the aircraft components and subsystems functionally tested while operating in response to simulation data broadcast by another aircraft component, the functional testing of one of the components and subsystems including determination of its response to the simulation data, said cart comprising:

(a) a portable housing;

(b) a plurality of processor-controllable instruments disposed on said housing for performing functional tests on the aircraft components and subsystems;

(c) connection means for interconnecting said instruments to the aircraft components and subsystems; and

(d) a system controller connected to said cart instruments, and further connected to the aircraft component broadcasting the simulation data, said system controller operative to control the functional test performance of the aircraft components and subsystems by said test instruments and operative to control the broadcast of the simulation data from the aircraft component broadcasting the simulation data, and including means for receiving and storing the results of the functional tests performed by said cart instruments.

20. The automated test equipment cart of claim 19, wherein said system controller further includes at least one test application comprising a set of system controller-executable instructions directing said system controller to perform a functional test with said instruments.

21. The integrated aircraft test system of claim 20, wherein said system controller contains at least two test applications directing said system controller to perform different functional tests.

22. The automated test equipment cart of claim 19 further including:

at least one display-data entry device connected to said system controller enabling an exchange of data between an operator and said system controller;

said system controller being adapted to exchange said data with the operator over said display-data entry device and further able to control said instruments in response to commands entered by the operator through said display-data entry device and to display said test results on said display-data entry device.

23. The automated test equipment cart of claim 21 further including:

at least one display-data entry device connected to said system controller enabling an exchange of data between an operator and said system controller; and

said system controller being adapted to exchange said data with an operator over said display-data entry device, and further able to control said instruments in response to commands entered by the operator through said display-data entry device and to display said test results on said display-data entry device.

24. The automated test equipment cart of claim 23, wherein at least one of said test applications contains instructions directing said system controller to generate messages on said display-data entry device informing the operator of the operator-performed steps that need to be performed during the functional test.

25. The automated test equipment cart of claim 19, wherein said system controller includes an input/output unit so that a central control unit can be connected thereto for reading said stored test results.

26. The automated test equipment cart of claim 19 further including:

at least one signal interface cable associated with said cart, having a plurality of connector elements for establishing separate conductive links to the aircraft components and subsystems;

a processor-controllable switch matrix for selectively establishing conductive interconnections between said instruments and said signal interface cable conductive elements; and

said system controller being connected to said switch matrix for controlling said electrical connections established thereby during the functional test.

27. The automated test equipment cart of claim 21 further including:

at least one signal interface cable associated with said cart, having a plurality of connector elements for establishing conductive links to the aircraft components and subsystems;

a processor-controllable switch matrix for selectively establishing conductive interconnections between said instruments and said signal interface cable conductive elements;

said system controller being connected to said switch matrix for controlling said electrical connections established thereby; and

said test application instructions directing said system controller to control said switch matrix so that selected electrical interconnections are established during each said functional test.

28. The automated test equipment cart of claim 19, wherein a plurality of aircraft components and subsystems operate in response to data broadcast by separate aircraft line-replaceable units, and during the functional testing of at least one of the aircraft components and subsystems, the simulation data is broadcast thereto by at least one line-replaceable unit;

said cart further including;

connection means for establishing interconnections between said system controller and the aircraft line-replaceable units; and

said system controller having an input/output unit so that said connection means can be connected thereto and being operative to control the broadcast of the simulation data by the aircraft line-replaceable units through signals transmitted over said connection means during the functional testing.

29. The automated test equipment carts of claim 28, wherein the line-replaceable units that broadcast the simulation data are connected to an on-aircraft central maintenance processor that controls the broadcast of the simulation data, said cart further including:

a central maintenance processor cable for providing a signal communications link between the central maintenance processor and said system controller;

said system controller being operative to control the broadcast of the simulation data from the line-replaceable units by the transmission of control signals to the central maintenance processor.

30. The automated test equipment cart of claim 29, wherein said system controller contains a plurality of test applications, each said test application comprising a set of system controller-executable instructions directing said system controller to perform a different functional test with said instruments, at least one said test application containing instructions to perform functional tests on an aircraft component or subsystem that, during the testing thereof, causes the simulation data to be broadcast to the aircraft component or subsystem, said at least one test application containing instructions directing said system controller to transmit control signals to the central maintenance processor to invoke the broadcast of the simulation data.

31. An integrated aircraft test system for functionally testing a plurality of aircraft components and subsystems, said test system comprising:

(a) a central control unit with memory means for storing a plurality of test applications used for performing functional tests on specific aircraft components and subsystems, at least two of said test applications comprising instructions for performing functional tests on different aircraft components and subsystems, for storing test results of functional tests performed on the aircraft, and for storing an indication of which said functional tests should be performed on the aircraft after particular work processes are performed;

(b) a test access station connected to said central control unit having input/output means for entering into said central control unit an indication of work processes performed on the aircraft wherein said central control unit responds to said indication of work processes performed on the aircraft by generating a message on said test access station input/output means indicating the functional tests that need to be performed on the aircraft in response to the work processes performed thereon; and

(c) a plurality of portable automated test equipment carts, each cart having instruments for performing functional tests on the aircraft in response to said test applications, at least two of said carts having instruments for performing functional tests on different aircraft components and subsystems, said carts each further having means for storing said test applications and test results of functional tests performed on the aircraft, and connection means for electronically connecting each said cart to said central control unit so that said test applications can be loaded from said central control unit to each said cart and so that said test results can be loaded from each said cart to said central control unit.

32. The integrated aircraft test system of claim 31, wherein:

said central control unit memory means are further operative to store a plurality of instruction sets of functional tests manually performed on the aircraft, further comprising;

a portable remote access terminal for storing said instruction sets and said test results;

display means for displaying instructional information regarding functional tests performed on the aircraft in response to said stored instruction sets;

data entry means for manually entering said test results of functional tests performed on the aircraft; and

connection means for electronically connecting said remote access terminal to said central control unit so that said instruction sets can be loaded from said central control unit to said remote access terminal and so that said test results can be loaded from said remote access terminal to said central control unit.

33. The integrated aircraft test system of claim 31, wherein said central control unit further responds to said indication of work performed by loading selected test applications for said functional tests to be performed on the aircraft into said automated test equipment carts used to perform said functional tests.

34. The integrated test access system of claim 31, wherein said central control unit includes a test auditor means for reviewing said test results and said work processes performed on the aircraft stored in said central control unit memory means and, wherein in response to said review, said test auditor means generates messages indicating missed and failed functional tests.

35. The integrated aircraft test system of claim 31, further including:

a test development site connected to said central control unit, having input/output means for entering said test applications, and for reviewing and certifying said test applications; and

wherein said central control unit stores each newly entered test application and loads said test applications into said automated test equipment carts and remote access terminal only after each said newly entered test application is certified.

36. An integrated aircraft test system for functionally testing a plurality of aircraft components and subsystems, said test system comprising:

(a) a central control unit with memory means for storing;

a plurality of test applications used for performing functional tests on specific aircraft components and subsystems, at least two of said test applications comprising instructions for performing functional tests on different aircraft components and subsystems;

instruction sets of functional tests manually performed on the aircraft;

test results of said functional tests performed on the aircraft; and

, an indication of which said functional tests should be performed on the aircraft after particular work processes are performed;

(b) a test access station connected to said central control unit having input/output means for entering into said central control unit an indication of work processes performed on the aircraft wherein said central control unit responds to said indication of work processes performed on the aircraft by generating a message on said test access station input/output means indicating the functional tests that need to be performed on the aircraft in response to the work processes performed thereon;

(c) a plurality of portable automated test equipment carts, each cart having instruments for performing functional tests on the aircraft in response to said test applications, at least two of said carts having instruments for performing functional tests on different aircraft components and subsystems, said carts each further having means for storing said test applications and test results of functional tests performed on the aircraft, and connection means for electronically connecting each said cart to said central control unit so that said test applications can be loaded from said central control unit to each said cart and so that said test results can be loaded from each said cart to said central control unit; and

(d) a portable remote access terminal comprising;

memory means for storing said instruction sets and said test results;

display means for displaying instructional information regarding functional tests performed on the aircraft in response to said stored instruction sets;

data entry means for manually entering said test results of functional tests performed on the aircraft; and

, connection means for electronically connecting said remote access terminal to said central control unit so that said instruction sets can be loaded from said central control unit to said remote access terminal and so that said test results can be loaded from said remote access terminal to said central control unit.

37. The integrated aircraft system of claim 36, wherein said central control unit further responds to said indication of work performed by loading selected test applications and instruction sets comprising instructions for said functional tests to be performed on the aircraft into said automated test equipment carts and into said remote access terminal.

38. The integrated aircraft test system of claim 36, wherein said central control unit includes test auditor means for reviewing said test results stored in said central control unit memory means and said work processes performed on on the aircraft, and, wherein in response to said review, said test auditor means are operative to generate messages indicating missed and failed functional tests.

39. The integrated aircraft test system of claim 36, further including:

a test development site connected to said central control unit, having input/output means for entering said test applications and said instructions sets and for reviewing and certifying said test applications and said instruction sets; and

wherein said central control unit stores each newly entered test application and instruction set and loads said test applications and said instruction sets into said automated test equipment carts and said remote access terminal only after each said newly entered test application or instruction set is certified.