System and method of cooling turbines
View Patent ↗A method of cooling a turbine having internal moving components to a predetermined temperature is disclosed. The method comprises taking the turbine offline. While the turbine is offline, nitrogen is flowed through the turbine until the turbine reaches the predetermined temperature while controlling the flow of nitrogen from at least one injection point to prevent damage to the moving components of the turbine by achieving uniform cooling of the internal moving components. Then the flow of nitrogen is stopped. A method and assembly for cleaning a turbine having a deposit formed on an internal surface of the turbine is also disclosed.
1. A method of cleaning a turbine with a deposit thereon, the method comprising:
flowing nitrogen gas through the turbine, wherein the turbine has internal moving components;
introducing a cleaning aerosol into the nitrogen gas to clean the turbine, the aerosol comprising at least one organic compound suitable for cleaning organic vapors or deposits from the turbine; and
contacting the internal moving components with the aerosol so as to remove deposits from the components.
2. The method of claim 1 , wherein the at least one organic compound is chosen from naptha, ethanol, terpenes, propanol, anionic surfactants and a product of hexylene glycol and diethanolamine.
3. The method of claim 1 , wherein the aerosol comprises a majority of droplets that are 100 microns or less in diameter.
4. The method of claim 1 , wherein the nitrogen gas is heated to a temperature of about 100.degree. F. or greater before introducing the aerosol.
5. The method of claim 1 , wherein the nitrogen gas is at temperature ranging from about 200.degree. F. to about 350.degree. F. before introducing the aerosol.
6. The method of claim 1 , wherein the nitrogen gas comprises essentially no water prior to introduction of the aerosol.