ON AUTOMATION OF DESIGN OF OIL SYSTEM OF AN AIRCRAFT GTE


Дәйексөз келтіру

Толық мәтін

Аннотация

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.

Авторлар туралы

Oleg Grishanov

JSC «Kuznetsov»

Хат алмасуға жауапты Автор.
Email: oa.grishanov@uec-kuznetsov.ru

design bureau expert

Zavodskoe shosse,29, Samara, 443009, Russian Federation

Әдебиет тізімі

  1. Mitin, B.M., Rahal'skiy, V.A.; Aksenov, N.K. and Frankshteyn, L.I. (1982), "Theoretical and experimental aimed at devising methods of reduction development terms and improving operational reliability of the aircraft gas turbine engine oil system", Transactions of Central Institute of Aviation Motors, №12007. (in Russian)
  2. Tryanov A.E., Grishanov, О.А. and Butylkin, S.V. (2006), Proektirovanie sistem suflirovaniya maslyanyh polostey aviatsionnyh GTD, uchebnoe posobie [Designing of breather systems oil sumps of aviation turbine engines, manual], SGAU, Samara. (in Russian).
  3. Marchukov, Е.Yu. and Kuprik, V.V. (2004),"Life cycle cost of converted aviation turbine engine", Gas turbo technology magazine, №10. (in Russian).
  4. Schurovskiy, V.А. (2002),"Application of a cost index of life cycle of the gas-turbine plant", Gas turbo technology magazine, №5. (in Russian).
  5. 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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© Grishanov O.A., 2023

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