Gas turbine blade impulse body module
AssigneeMTU Aero Engines AG
InventorsKarl-Hermann Richter, Herbert Hanrieder, Steffen Gerloff
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AssigneeMTU Aero Engines AG
InventorsKarl-Hermann Richter, Herbert Hanrieder, Steffen Gerloff
Estimating the term…
The present invention relates to an impulse body module group with at least two impulse body modules, which, in particular, are identical in construction, for a gas turbine blade, wherein each of the impulse body modules comprises a housing, which, in particular, is of one piece and which has a first cavity, which is closed, in particular in an airtight manner, by a first cover, which is joined to the housing, in particular in a material-bonded manner, and in which a single, in particular spherical or cylindrical, first impulse body is accommodated with play of movement in at least one first direction of impact, wherein the housing has no additional cavity or a single additional cavity, in which a single, in particular spherical or cylindrical, additional impulse body is accommodated with play of movement in at least one direction of impact.
An impulse body module group with at least two impulse body modules, which are identical in construction, for a gas turbine blade, wherein each of the impulse body modules comprises
Dependencies are inferred from the claim text.