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RESEARCH PAPERS

Preliminary Study on Reheat Combustors for Advanced Gas Turbines

[+] Author and Article Information
Kenji Mori, Junichi Kitajima, Takeshi Kimura

Research Section, Technical Institute, Kawasaki Heavy Industries, Ltd., Akashi 673, Japan

Sansei Miki

Technology Development Group, Kawaski Heavy Industries, Ltd., Tokyo 105, Japan

J. Eng. Power 104(1), 1-8 (Jan 01, 1982) (8 pages) doi:10.1115/1.3227250 History: Received December 05, 1980; Online September 28, 2009

Abstract

Feasibility studies carried out by the Engineering Research Association for Advanced Gas Turbines under the sponsorship of the Agency of Industrial Science and Technology of Japan have indicated that the thermal efficiency of the combined cycle plant incorporating a high temperature reheat gas turbine and a steam turbine can exceed 50 percent. One of the engine components being investigated is the high temperature reheat combustor which will operate under high temperature (973 K) and heavily vitiated (12.4 percent O2 ) inlet-air conditions. This paper describes the design considerations on the reheat combustor and the results of the near-atomospheric pressure tests (0.1 ∼ 0.3 MPa) under vitiated conditions, using a conventional can-type combustor and a full scale model of the reheat combustor. Effects of air vitiation on inflammability limits, combustion efficiency, NOx and wall temperatures of gas turbine combustors are discussed.

Copyright © 1982 by ASME
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