Invention Grant
US08377232B2 On-line cleaning of turbine hot gas path deposits via pressure pulsations 有权
通过压力脉动在线清洁涡轮机热气体通道沉积物

On-line cleaning of turbine hot gas path deposits via pressure pulsations
Abstract:
A method for removing hot gas deposits from a system via pressure pulses is provided. The method includes regulating a flow of a mixture of detonation fluid and oxidizer into an expansion chamber; and generating a detonation within the expansion chamber by igniting the mixture of detonation fluid and oxidizer in the expansion chamber producing a high-pressure wave, the high-pressure wave propagating along a fluid path of the system in a supersonic rate removing hot gas deposits in the fluid path while the system is in fired operation, the expansion chamber directing the high-pressure wave towards the fluid path of the system.
Information query
Patent Agency Ranking
0/0