Technology of manufacturing some elements of a combustion chamber with a lateral system of reverse current area formation
UDK 621.45.022 BBK 39.55
With each passing year, the operational requirements for the aircraft power plants are getting stricter and stricter. The combustion chamber as one of the main parts of an aircraft engine determines the indicators of its efficiency, reliability and environmental compatibility. The indicators can be improved due to taking into account the operational requirements at the stage of designing a combustion chamber.
As the concept of a combustion chamber with a lateral system of reverse current area formation implies presence of a number of thin-walled elements as well as double-curved surfaces, designing a chamber of such construction is a complex engineering problem.
The article describes a technology of manufacturing a combustion chamber of the desired design on an example of experimental model for a chamber stand.
Key words: combustion chamber, aircraft gas-turbine engine, operational features, technology of manufacturing, combustion process.
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