The combustion chamber supplies heat to the working medium.

Main requirements:

• high extent of combustion
• uniformity of temperature
• multimode operation capacity
• low emission level
• minimum overall dimensions

Our experience: The circular reverse-flow combustion chamber of the TV7-117S turboprop engine reduces the length of the engine. It is a small unit that features a high extent of combustion and restores full pressure fast. Thanks to the chamber’s superb emission parameters it may be installed without modifications in a more powerful version of the engine, the ТV7-117SМ (SТ).

Further improvements:  To use new materials, particularly ceramic metal composites for operation at higher temperatures.