Design solutions to provide thermal protection of three-shaft turbofan engine turbine support oil cavities

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Abstract

The paper presents design approach to providing thermal protection of three-shaft turbofan engine turbine support oil cavities. The advantages and disadvantages of three-shaft engines are described. Basing upon the performed analysis, there are offered the potential decisions for providing thermal protection of turbine support oil cavities.

About the authors

A. G. Petrukhin

JSC «KUZNETSOV», Samara

Author for correspondence.
Email: petruhin_t@mail.ru

Design Engineer

Russian Federation

A. A. Boev

JSC «KUZNETSOV», Samara

Email: petruhin_t@mail.ru

Design Engineer

Russian Federation

S. V. Butylkin

JSC «KUZNETSOV», Samara

Email: petruhin_t@mail.ru

Design Engineer

Russian Federation

References

  1. Трянов, А.Е. О тепловой защите масляных полостей опор создаваемых ГТД [Текст] / А.Е. Трянов, О.А. Гришанов, А.С. Виноградов // Вестн. СГАУ. - 2009. – №3. Ч.1. - С. 318-328.
  2. Киселев, Ю.В. Конструкция и техническая эксплуатация двигателя Д-36 [Текст]: учеб. пособие / Ю.В. Киселев, С.Н. Тиц – Самара: Самар. гос. аэрокосм. ун-т. - 2006. - 90 с.
  3. Пат. 109223 Российская Федерация. Турбина трёхвального газотурбинного двигателя [Текст] / А.Е. Трянов, О.А. Гришанов, А.А. Боев, опубл. 10.10.2011. – 3 с.

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