Gas turbine and guide blade for a housing of a gas turbine
AssigneeMTU Aero Engines AG
InventorsMarkus Schlemmer, Marcin Rozak
Life of this patent
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AssigneeMTU Aero Engines AG
InventorsMarkus Schlemmer, Marcin Rozak
Estimating the term…
A gas turbine, in particular an aircraft engine, having a housing in which at least one guide blade (12) is situated, the guide blade (12) including at least one shroud configuration (21) having a radially outer shroud (16) and having a shroud holding device (23) with the aid of which the shroud (16) is secured on the housing, as well as including a turbine blade (18) extending radially inward from the shroud configuration (21). The shroud holding device (23) or parts thereof include(s) at least one air passage channel (28), which permits a flow passage through the shroud holding device (23). The invention also relates to a guide blade (12) for placement on a housing of a gas turbine as well as a method for manufacturing such a guide blade (12).
A gas turbine comprising:
A guide blade for placement on a housing of a gas turbine, comprising:
A method for manufacturing a guide blade for a housing of a gas turbine, the guide blade including a shroud configuration having a radially outer shroud in the installed state and having a shroud holding device with the aid of which the shroud is securable on the housing;
Dependencies are inferred from the claim text.