Analysis of Composite Blades of Gas Turbine Engines.

被引：0

作者：

Dem'yanushko, E.L.

机构：

来源：

Izvestia vyssih ucebnyh zavedenij. Masinostroenie | 1986年 / 09期

关键词：

AIRCRAFT ENGINES; JET AND TURBINE - Blades - COMPOSITE MATERIALS - COMPUTER AIDED ANALYSIS - COMPUTER AIDED DESIGN - TURBOMACHINERY - Blades;

D O I：

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学科分类号：

摘要：

Computation of the turbocompressor rotor blade is proposed. The blade is made of a composite material. Using a variational method, equations are obtained determining stresses and deformations of a twisted blade under the effect of centrifugal and gas loads. The equations correspond to the theory of naturally twisted rods with consideration of deplanation. An example of computer-aided analysis of a blade is presented.

引用

页码：7 / 10

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