Email this article ON AUTOMATION OF DESIGN OF OIL SYSTEM OF AN AIRCRAFT GTE
- Authors: Grishanov O.A.1
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Affiliations:
- JSC «Kuznetsov»
- Issue: Vol 9, No 3 (2023)
- Pages: 43-48
- Section: Articles
- URL: https://journals.rcsi.science/2409-4579/article/view/249376
- DOI: https://doi.org/10.18287/2409-4579-2023-9-3-43-48
- ID: 249376
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Abstract
The design of subsystems and main elements of the oil system of an aircraft gas turbine engine comes down to working on the proposed algorithms. Traditionally, the oil system is divided into hydraulic, thermal and mechanical modules. The methods for designing the elements of each module are known and verified by development experience. But coupled with an assessment of the engine life cycle cost, on the basis of which the algorithms presented in the article were created, a convenient engineering design tool is formed.
About the authors
Oleg A. Grishanov
JSC «Kuznetsov»
Author for correspondence.
Email: oa.grishanov@uec-kuznetsov.ru
design bureau expert
Zavodskoe shosse,29, Samara, 443009, Russian FederationReferences
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- Marchukov, Е.Yu. and Kuprik, V.V. (2004),"Life cycle cost of converted aviation turbine engine", Gas turbo technology magazine, №10. (in Russian).
- Schurovskiy, V.А. (2002),"Application of a cost index of life cycle of the gas-turbine plant", Gas turbo technology magazine, №5. (in Russian).
- OST № 1 00969-80 [Industrial standard]. Sistemy maslyanye gazoturbinnyh dvigateley samoletov. Obshchie tekhnicheskie trebovaniya [Systems oil gas-turbine engines of airplanes. The general technical requirements] (in Russian).
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