Basic Research of the Intercooled Turbofan Aero-Engine

Jin Chuan Zhang; Yun Wang; Can Zhang

doi:10.4028/www.scientific.net/AMR.516-517.544

Paper Titles

Numerical Simulation of Thermal Environment in High Heat Tunnel
p.519

Study of Forming & Exfoliation Mechanism of Oxide Skin in High-Temperature Tube of Supercritical Boiler
p.524

The Application of the Smirnov Test in the Homogeneity Test for Non-Normal Distribution Temperature Series
p.530

Analysis on Abnormal Rejects Discharge of a Medium Speed Pulverizer
p.539

Basic Research of the Intercooled Turbofan Aero-Engine
p.544

A Heuristic Search Algorithm for a Dynamic Production Model with Random Factors
p.548

Analysis of Two-Dimensional and Three-Dimensional Simulation of the Disc Eddy Current Braking Device
p.553

Application of Matrix Analysis in Multiple Index Orthogonal Test Design
p.558

Application of Similarity Modeling in Failure Prognostic System
p.563

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 516-517Basic Research of the Intercooled Turbofan...

Basic Research of the Intercooled Turbofan Aero-Engine

Abstract:

In conventional turbofan aero-engine designs, the effective way of improvement of engine efficiency is through the increasing of overall pressure ratio and improving of combustor inlet gas temperature, but the further incresement of compressor overall pressor ratio is constricted by high pressure compressor outlet allowed temperature. The improvement of combustor outlet temperature is limited by turbine allowed inlet temperature during take-off and climbing. An intercooled core can be designed with a significantly higher overall pressure ratio also with reduced cooling air requirements, providing a higher thermal efficiency compared with a conventional core. Through the basic analysis of performance of intercooler aeroengines. It indicated that the intercooled aero-engines can decrese the feul consume clearly and have a further potential in future civil aircraft application.

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Periodical:

Advanced Materials Research (Volumes 516-517)

Pages:

544-547

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.516-517.544

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Online since:

May 2012

Authors:

Jin Chuan Zhang, Yun Wang, Can Zhang

Keywords:

Aeroengine, Compressor, Intercooler

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