Method and arrangement for providing a fault diagnosis for at least one system
First Claim
1. A fault diagnosis apparatus for at least one system of an aircraft, the fault diagnosis system comprising:
- a number N1, n1 ε
[1, . . . , N1], of systems, wherein the n1-th system, in each case, is configured to provide a number N2, n2 ε
[1, . . . , N2], of instances of a main function of a number N3, n3 ε
[1, . . . , N3] of main functions of the aircraft;
a number N4, n4 ε
[1, . . . , N4], of IMA modules, wherein the n4-th IMA module, in each case, is configured to provide resources at least to the respective n2-th instances of the main functions;
a generic diagnostic unit comprisinga predetermined number N5, n5 ε
[1, . . . , N5], of instances of the generic diagnostic unit; and
wherein, the n5-th instance, in each case, of the generic diagnostic unit is configured for adaption of the corresponding n5-th diagnostic unit to at least one system.
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Accused Products
Abstract
The present invention provides a method for providing a fault diagnosis for at least one system, in particular of an aircraft. The method comprises: (a) providing a number N1, n1ε[1, . . . , N1], of systems, wherein the n1-th system, in each case, provides a number N2, n2ε[1, . . . , N2], of instances of a main function of a number N3, n3ε[1, . . . , N3], of main functions of the aircraft; (b) providing a number N4, n4ε[1, . . . , N4], of IMA modules, wherein in each case the n4-th IMA module provides resources at least for the respective n2-th instances of the main functions; (c) providing a generic diagnostic unit; (d) instantiating the generic diagnostic unit to provide a predetermined number N5, n5ε[1, . . . , N5], of instances of the generic diagnostic unit; and (e) configuring the n5-th instance, in each case, of the generic diagnostic unit for adaption of the corresponding n5-th diagnostic unit to at least one system.
11 Citations
22 Claims
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1. A fault diagnosis apparatus for at least one system of an aircraft, the fault diagnosis system comprising:
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a number N1, n1 ε
[1, . . . , N1], of systems, wherein the n1-th system, in each case, is configured to provide a number N2, n2 ε
[1, . . . , N2], of instances of a main function of a number N3, n3 ε
[1, . . . , N3] of main functions of the aircraft;a number N4, n4 ε
[1, . . . , N4], of IMA modules, wherein the n4-th IMA module, in each case, is configured to provide resources at least to the respective n2-th instances of the main functions;a generic diagnostic unit comprising a predetermined number N5, n5 ε
[1, . . . , N5], of instances of the generic diagnostic unit; andwherein, the n5-th instance, in each case, of the generic diagnostic unit is configured for adaption of the corresponding n5-th diagnostic unit to at least one system. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21)
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22. An arrangement for providing a fault diagnosis for at least one system, in particular of an aircraft, comprising:
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a number N1, n1 ε
[1, . . . , N1], of systems, wherein the n1-th system, in each case, provides a number N2, n2 ε
[1, . . . , N2] of instances of a main function of a number N3, n3 ε
[1, . . . , N3] of main functions of the aircraft;a number N4, n4 E [1, . . . , N4], of IMA modules, wherein the n4-th IMA module, in each case, provides resources at least for the respective n2-th instances of the main functions; and a predetermined number N5, n5 ε
[1, . . . , N5], of instances of a generic diagnostic unit, wherein the n5-th instance, in each case, of the generic diagnostic unit is configured for adaption of the corresponding n5-th diagnostic unit to at least one system.
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Specification