Arrangement for axially securing blades in a rotor of a gas turbine
The invention relates to an arrangement (10) for axially securing blades (14) of a rotor (23) of a gas turbine. The arrangement has a sealing element (16) arranged on the end side surface of the rotor (23), which can be particularly reliably attached to the rotor (23) by means of a sheet metal strip...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention relates to an arrangement (10) for axially securing blades (14) of a rotor (23) of a gas turbine. The arrangement has a sealing element (16) arranged on the end side surface of the rotor (23), which can be particularly reliably attached to the rotor (23) by means of a sheet metal strip made of a shape-memory alloy. |
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