| 摘要 |
<p>A process and apparatus is provided for cleaning deposits (9) from gas turbine engine components, particularly turbine blades (1), by locating or drilling a hole into the cavity of the component, inserting a cleaning tube (7) into the cavity and cleaning the deposits (9) from the cavity with a cleaning material inserted into the cavity through the tube (7), followed by sealing any hole drilled in the component.</p> |
