Journal of Chemical Engineering and Energy Materials

Torch Set for Gas and Liquid Fuel, Burner Assembly for Fuel Gas & Liquid Fuels

Articles in Press

Document Type : Original Article

Author

Andi Johnson

Department of Research and Development, UOP, Santiago, Chile

10.22034/jceem.2026.588571.1032
Abstract
The two combustion chambers are located vertically around the turbine and are connected to the turbine housing by side flanges. This type of design makes it possible to keep the inlet air from the compressor to the combustion chamber and from the combustion chamber to the turbine in one direction and causes the least relative pressure drop and relative velocity. Compressed air from the compressor entering the combustion chamber cools the outer shell of the hot gas. In addition, the symmetrical inlet and dual variable airflow results in a symmetrical temperature distribution with minimal pressure change in front of the first row of rotating vanes. Each combustion chamber consists of 8 burners (BURNER) designed for both gas and diesel fuel. Fuel burners operate in accordance with the law of reverse flow. This arrangement of the combustion chamber creates a great flexibility in the dimensions as well as the shape of the combustion system and provides a good possibility for inspection as well as the possibility of easy assembly and disassembly. Combined burners 1 cause diffusion as well as premixing of the flame and produce nitrous oxide and low carbon monoxide without spraying water and steam injection. However, a gas turbine engine can use a water or steam injection system to reduce pollution.

Keywords

Torch Set
Gas and Liquid Fuel
Burner Assembly
Fuel Gas &‌ Liquid Fuels
Industry
Subjects
Journal of Chemical Engineering and Energy Materials

Articles in Press, Accepted Manuscript
Available Online from 20 July 2026

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