Device and system for maintaining a complex system, particularly an aircraft

• US 20040153800A1
• Filed: 06/18/2003
• Published: 08/05/2004
• Est. Priority Date: 06/19/2002
• Status: Abandoned Application

• Current Assignee: Eurocopter
• Original Assignee: Eurocopter
• Inventors: Germanetti, Serge
• Application Number:
  US10/463,856
• Publication Number:
  US 20040153800A1
• Time in Patent Office: Days
• US Class Current: 714/30
• CPC Class Codes: B64F 5/60 Testing or inspecting aircraft components or systems
• CPC Class Codes: G01D 3/08 with provision for safeguarding the apparatus, e.g. against abnormal operation, against breakdown

Abstract

The maintenance device (2) comprises electronic equipments (4A, 4B, 4C) each comprising a test means (5A, 5B, 5C) and a memory (6A, 6B, 6C) for recording information relating to a fault, a central unit (8) comprising a test means (10), a memory (11), a computer (12) which receives information from, the electronic equipments (4A, 4B, 4C) indicating the test means that detected a fault, which determines, from this information, a faulty element and which indicates, on a screen (16, 17) while the complex system is in operation, the occurrence of a fault and the faulty element and, at the end of operation, a list of the faults that have occurred, with the faulty elements, a memory (13) for recording the information processed by the computer (12), and interfaces for accessing said memories.

Claims

1. Device for maintaining a complex system, particularly an aircraft,

which comprises at least:

a plurality of electronic equipments (4A, 4B, 4C) which are mounted on said complex system, each of said electronic equipments (4A, 4B, 4C) comprising;

at least one built-in test means (5A, 5B, 5C) for detecting a fault while the complex system is in operation;

at least one first test memory (6A, 6B, 6C) for recording, when a fault is detected by said test means (5A, 5B, 5C), information relating to this fault; and

an interface (7A, 7B, 7C) providing access to said first test memory (6A, 6B, 6C); and

a central unit (8) mounted on said complex system, connected to said electronic equipments (4A, 4B, 4C) and which comprises;

at least one built-in test means (10) for detecting a fault while the complex system is in operation;

at least one second test memory (11) for recording, when a fault is detected by said test means (10), information relating to this fault;

a computer (12) which receives, when a fault is detected, information from said electronic equipments (4A, 4B, 4C) indicating the test means that detected the fault, which attempts to determine, from this information, at least one faulty element in said complex system and which is able to indicate on a display screen (16, 17);

while the complex system is operating, automatically, the occurrence of a fault and, if it has been determined, the corresponding faulty element; and

at the end of operation of the complex system, on request, a list of the faults that occurred during operation, with the corresponding faulty elements;

at least one maintenance memory (13) for recording all the information processed by said computer (12); and

at least one interface (14, 15) providing access to said second test memory (11) and to said maintenance memory (13).

2. Device according to claim 1, which additionally comprises a plurality of sensors (23A, 23B, 23C) able to measure the values of parameters of the complex system, while it is operating, and to transmit the measured values to said central unit (8) so that they can be recorded in said maintenance memory (13).

3. Device according to claim 1, wherein said central unit (8) additionally comprises filtering means (19).

4. Device according to claim 1, wherein said display screen (16, 17) forms part of a display system (4B, 4C) which represents an electronic equipment additionally equipped with a built-in test means (5B, 5C), with a first test memory (6B, 6C) and with an interface (7B, 7C).

5. Device according to claim 4, which comprises two display systems (4B, 4C).

6. Device according to claim 1, wherein said display screen forms part of said central unit.

7. Device according to claim 1, wherein said computer (12) displays, on request, at the end of operation of the complex system, on said display screen (16, 17), at least a diagnostic table which represents a compilation comprising, for each fault, at least the following information:

the test or tests performed;

the element or elements likely to be responsible for the fault;

the probability of these elements being faulty, or any other indicator associated with this probability.

8. Device according to claim 7, which additionally comprises a means allowing the diagnostic table to be amended.

9. Device according to claim 1, wherein said central unit (8) is produced with dual architecture.

10. System for maintaining a complex system, particularly an aircraft, which comprises:

said maintenance device (2) specified in claim 1;

and

a portable maintenance unit (3) able to be connected, via at least one digital link (20A, 20B, 20C, 20D, 20E) to said interfaces of said first test memories (4A, 4B, 4C), of said second test memory (11) and of said maintenance memory (13) and which comprises;

a processing means (21) able to receive and to process the information recorded in said first and second test memories (4A, 4B, 4C, 11) and said maintenance memory (13) and to form, from this information, a maintenance report; and

information-presenting means (22) able to present said maintenance report to an operator.

11. System according to claim 10, wherein said maintenance unit (3) forms and presents the maintenance report, at least in part, on at least a diagnostic table which represents a compilation comprising, for each fault, at least the following information:

the test or tests performed;

the element or elements likely to be responsible for the fault;

the probability of these elements being faulty, or any other indicator associated with this probability.

12. System according to claim 11, which additionally comprises a means allowing the diagnostic table to be amended.

13. System according to claim 10, wherein said maintenance unit (3) is a portable personal computer.