Aircraft fault real-time monitoring method and system based on ACMS
A technology of real-time monitoring and fault monitoring, applied in the field of aircraft maintenance, can solve the problems of increasing the manpower input for ground maintenance, increasing the maintenance cost of the fleet, and impossible to achieve in one step. big effect
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Embodiment 1
[0072] refer to figure 1 , shows a flow chart of the steps of an ACMS-based aircraft fault real-time monitoring method, including the following steps:
[0073] Step 101, obtaining aircraft technical manual and ACMS technical specification;
[0074] The aircraft technical manual is a technical manual provided by the manufacturer, which records the technical specifications of the parameters of each subsystem or component of the aircraft, and the ACMS technical specifications also belong to the public category.
[0075] Step 102, extracting aircraft failure characteristic parameters according to the aircraft technical manual;
[0076] The working principle and mathematical model of the subsystem or component of the aircraft to be monitored can be determined from the aircraft technical manual, and its characteristic parameters can be determined. The change of this parameter can reflect the working performance or state of the subsystem or component.
[0077] Step 103, write the a...
Embodiment 2
[0086] A method for real-time monitoring of aircraft faults based on ACMS, comprising the steps of:
[0087] Step 201, obtaining aircraft technical manuals and ACMS technical specifications;
[0088] Step 202, searching for aircraft subsystems or components that affect the safe operation of the aircraft according to the aircraft technical manual;
[0089] These aircraft subsystems or components include: flight control system, navigation system, air conditioning system, bleed air system and so on.
[0090] Step 203, extracting parameters reflecting the performance of the aircraft subsystem or component to obtain aircraft failure characteristic parameters;
[0091] Step 204, comparing the characteristic parameters of the aircraft with the parameters in the original ACMS parameter library, and identifying the list of parameters included and the list of parameters not included;
[0092] Specifically, it is to distinguish which of all aircraft failure characteristic parameters ob...
Embodiment 3
[0144] refer to Figure 7 , shows a structural block diagram of an ACMS-based aircraft fault real-time monitoring system, including:
[0145] A manual acquisition module 301, configured to acquire aircraft technical manuals and ACMS technical specifications;
[0146] Parameter extraction module 302, is used for extracting aircraft failure characteristic parameter according to described aircraft technical manual;
[0147] In this embodiment, the parameter extraction module 302 includes:
[0148] The parameter search sub-module is used to find aircraft subsystems or components that affect the safe operation of the aircraft;
[0149] The parameter extraction sub-module is used to extract parameters reflecting the performance of the aircraft subsystem or component, and obtain aircraft failure characteristic parameters.
[0150] Parameter storehouse building module 303, for writing described aircraft fault characteristic parameter into ACMS parameter storehouse according to desc...
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