Research of the thermal state of aviation engine supports

Alexandr Vinogradov; Renat Badykov; Clovis Pilla

doi:10.3923/rjasci.2014.789.794

Research of the thermal state of aviation engine supports

Alexandr Vinogradov^*
, Renat Badykov
, Clovis Pilla

^*Corresponding author for this work

Samara National Research University

Research output: Contribution to journal › Article › peer-review

3 Scopus citations

Abstract

This study discusses the main sources of heat transferred to the support of an aircraft engine; explores ways to identify and give them a quantitative comparison. A technique for determining the thermal state of supports of aircraft engines was developed this makes it possible to select a desired cooling system as well as to evaluate and adjust the basic parameters of the engine oil system.

Original language	English
Pages (from-to)	789-794
Number of pages	6
Journal	Research Journal of Applied Sciences
Volume	9
Issue number	11
DOIs	https://doi.org/10.3923/rjasci.2014.789.794
State	Published - 2014
Externally published	Yes

Keywords

Bearing
Cooling
Friction
Heat flow
Heat transfer coefficient
Seal
Temperature

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10.3923/rjasci.2014.789.794

Cite this

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title = "Research of the thermal state of aviation engine supports",

abstract = "This study discusses the main sources of heat transferred to the support of an aircraft engine; explores ways to identify and give them a quantitative comparison. A technique for determining the thermal state of supports of aircraft engines was developed this makes it possible to select a desired cooling system as well as to evaluate and adjust the basic parameters of the engine oil system.",

keywords = "Bearing, Cooling, Friction, Heat flow, Heat transfer coefficient, Seal, Temperature",

author = "Alexandr Vinogradov and Renat Badykov and Clovis Pilla",

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AU - Badykov, Renat

AU - Pilla, Clovis

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PY - 2014

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N2 - This study discusses the main sources of heat transferred to the support of an aircraft engine; explores ways to identify and give them a quantitative comparison. A technique for determining the thermal state of supports of aircraft engines was developed this makes it possible to select a desired cooling system as well as to evaluate and adjust the basic parameters of the engine oil system.

AB - This study discusses the main sources of heat transferred to the support of an aircraft engine; explores ways to identify and give them a quantitative comparison. A technique for determining the thermal state of supports of aircraft engines was developed this makes it possible to select a desired cooling system as well as to evaluate and adjust the basic parameters of the engine oil system.

KW - Bearing

KW - Cooling

KW - Friction

KW - Heat flow

KW - Heat transfer coefficient

KW - Seal

KW - Temperature

UR - https://www.scopus.com/pages/publications/84918541792

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DO - 10.3923/rjasci.2014.789.794

M3 - 文章

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JO - Research Journal of Applied Sciences

JF - Research Journal of Applied Sciences

IS - 11

ER -

Research of the thermal state of aviation engine supports

Abstract

Keywords

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