Analysis of Composite Blades of Gas Turbine Engines.

被引：0
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作者：
Dem'yanushko, E.L.
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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;
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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.
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页码：7 / 10
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