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Method of precisely calculating continuouly using time of airplane auxiliary power device through establishing dynamic model

An aircraft auxiliary power and dynamic model technology, applied in the aviation field, can solve problems such as large APU time calculation errors, potential safety hazards, and deviations, and achieve the effects of improving work quality, ensuring correct judgment, and reducing errors

Inactive Publication Date: 2008-06-18
XIAMEN AIRLINES CO LTD
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  • Abstract
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Problems solved by technology

For this reason, in the process of monitoring the use of APU and related accessories, the common practice in the civil aviation industry is to multiply the aircraft use time by a conversion factor to obtain the use time of the APU; due to the lack of complete and accurate data basis, the conversion factor is often Lack of certain science and dynamics, so that there is a large deviation between the APU conversion coefficient and the objective reality, resulting in a large error in the calculation of the APU time, affecting the quality of the monitoring of the APU and its accessories, resulting in the APU and its accessories. The misjudgment of the performance trend of the accessories and the miscalculation of the APU usage cost not only bring hidden dangers to safety, but also bring economic losses.

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  • Method of precisely calculating continuouly using time of airplane auxiliary power device through establishing dynamic model
  • Method of precisely calculating continuouly using time of airplane auxiliary power device through establishing dynamic model
  • Method of precisely calculating continuouly using time of airplane auxiliary power device through establishing dynamic model

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Embodiment Construction

[0058] see figure 1 , figure 2 , image 3 Shown, a kind of method of the present invention accurately calculates the continuous service time of aircraft auxiliary power unit APU by setting up dynamic model, it comprises the steps:

[0059] Box 1 is to set the initial conversion coefficient; this is the initial step of the whole plan. For each model in the fleet, first determine an initial APU usage time conversion coefficient for each model based on past experience. This coefficient is generally The value range is 0.5-1.5. One of the determination methods is to take an aircraft that has not undergone APU and APU timer replacement in each model, and divide its total APU usage time within a period of time (the period is at least one month) by the The total flight time of the aircraft, and the result is the initial APU usage time conversion factor.

[0060] Box 2 is to establish the attribute value of APU accumulative use time; since it is necessary to provide continuous APU...

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Abstract

Through procedures of setting initial deduction coefficient, establishing attribute value of accumulating service time of auxiliary power unit (APU) and determining annual deduction coefficient etc. by using comparison and discrimination made by computer for the readings of APU timer obtained each time, the method can provide continuous APU accumulated service time, modify APU deduction coefficient, making value calculated accurate gradually. The method reduces calculating error and error of APU deduction coefficient to increase quality of monitoring APU Ensuring corrective judgment for service performance of APU and accessories.

Description

technical field [0001] The invention belongs to the field of aviation technology, in particular to a method for accurately calculating the continuous service time of an aircraft auxiliary power unit APU by establishing a dynamic model. Background technique [0002] In the maintenance process of civil aviation aircraft, it is usually necessary to know the service time of the aircraft itself and the service time of the aircraft auxiliary power unit (APU) (hereinafter referred to as APU). There is a difference between the use time of the aircraft; the use time of the aircraft itself can be calculated by calculating the flight time recorded by the pilot in the aircraft flight record book, or directly using the aircraft recorded by the aircraft data acquisition system (DFDAU) Time, the data acquisition system (DFDAU) can obtain accurate automatic record values; but it is more difficult to obtain the APU usage time. The APU usage time of the aircraft is obtained by means of the r...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/40G06N7/00
Inventor 林朝阳吴兴旺薛明宏李童祝建军
Owner XIAMEN AIRLINES CO LTD