DocumentCode
1887901
Title
Analysis of spectrometric data of aeroengines to establish hazard threshold limits for Iron content
Author
Hassan, Ahmad ; Manarvi, Irfan Anjum
Author_Institution
Centre for Adv. Studies in Eng., Islamabad, Pakistan
fYear
2012
fDate
3-10 March 2012
Firstpage
1
Lastpage
7
Abstract
As aero-engines operate, metal and other material particles are removed from the contact surfaces and are carried away in the flow of lubricating oil. Spectrometric Oil Analysis Program (SOAP) is a powerful tool for elemental analysis of structural metals in the lubricating oils circulating inside the machine, and is suitable for determining wear metal quantity, elemental composition, rate of wear and its source. The oil samples from the aero-engines are analyzed through spectrometry and the readings are assessed against pre-defined values to ascertain the physical health of the engines. This method is employed to continuously monitor the condition of the engine internal parts without any stripping, thus reducing maintenance time and costs. The predefined values or limits for SOAP are defined by the Original Equipment Manufacturer and are normally formalized during design process of the equipment. For the Chinese range engines powering the fighter jet aircraft, the limits for SOAP are not defined and thus this valuable technique cannot be fully applied to these engines. As a consequence the benefits of continuous condition monitoring together with reduced maintenance cost and time are not fully accrued. Iron (Fe) is the major element of the engine internal parts and its inclusion in oil sample gives a clear picture of the wear and tear of the engine internal parts. In order to accrue benefits of SOAP on Chinese range aero-engines there is a need to define the alert and hazard thresholds limits for SOAP on these engines. Once defined, the SOAP data can be used to decide about the continued operation of the engine or its induction for maintenance. In this paper the SOAP data for Chinese range engines operating in the fighter aircraft is collected and then it is statistically analysed to establish the limits for alerts and hazard for Iron (Fe).
Keywords
aerospace engines; condition monitoring; cost reduction; inclusions; iron; lubricating oils; machinery production industries; maintenance engineering; military aircraft; spectrochemical analysis; spectroscopy; wear testing; aeroengines; condition monitoring; contact surfaces; elemental composition; engine internal parts; engine physical health; fighter jet aircrafts; hazard threshold limits; iron content; lubricating oils; machines; maintenance cost reduction; original equipment manufacturer; spectrometric data analysis; spectrometric oil analysis program; tear; wear metal quantity; wear rate; Engines; Hazards; Histograms; Iron; Simple object access protocol; Weibull distribution;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2012 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4577-0556-4
Type
conf
DOI
10.1109/AERO.2012.6187361
Filename
6187361
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