Editing Combustor (section)

{{short description|Part of a jet engine where fuel is burned}}

A '''combustor''' is a component or area of a [[gas turbine]], [[ramjet]], or [[scramjet]] [[engine]] where [[combustion]] takes place. It is also known as a '''burner''', '''burner can''', '''combustion chamber''' or '''flame holder'''. In a gas turbine engine, the ''combustor'' or [[combustion chamber]] is fed high-pressure air by the compression system. The combustor then heats this air at constant pressure as the fuel/air mix burns.  As it burns the fuel/air mix heats and rapidly expands. The burned mix is exhausted from the combustor through the nozzle guide vanes to the turbine. In the case of ramjet or scramjet engines, the exhaust is directly fed out through the nozzle.

A combustor must contain and maintain stable combustion despite very high air flow rates. To do so combustors are carefully designed to first mix and ignite the air and fuel, and then mix in more air to complete the combustion process. Early gas turbine engines used a single chamber known as a can-type combustor. Today three main configurations exist: can, annular, and cannular (also referred to as can-annular tubo-annular). Afterburners are often considered another type of combustor.

Combustors play a crucial role in determining many of an engine's operating characteristics, such as [[fuel efficiency]], levels of emissions, and transient response (the response to changing conditions such as fuel flow and air speed).