Insert element, annular segment, gas turbine and mounting method
A technology for gas turbines and installation methods, applied in the direction of safety devices, engine components, blade support components, etc., can solve the problems of heavy lifting, etc., and achieve the effect of fast setting and execution
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0029] figure 1 A gas turbine 10 according to the invention is shown in an exemplary embodiment. The gas turbine 10 comprises a turbine 11 in which at least one rotor blade row 12 is arranged. A ring composed of a plurality of ring segments is arranged around the rotor blade row 12 . The rotor blade row 12 is arranged in such a manner that it can rotate about an axis of rotation 20 .
[0030] A rotor blade row 12 is in particular a rotor blade row located downstream of other rotor blade rows. exist figure 1 , the corresponding rotor blade row 12 is the fourth rotor blade row of the turbine 11 of the gas turbine 10 .
[0031] The gas turbine 10 according to the invention has at least one ring segment 13 according to the invention. figure 2 Ring segment 13 is shown in an exemplary embodiment.
[0032] The ring segment 13 comprises a ring segment body 25 and an insert element 14 according to the invention.
[0033] The ring segment body 25 includes a hot gas side 27 . In...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 