Blade cascade for a turbomachine
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United States of America Patent
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Apr 24, 2018
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N/A
app pub date -
Jul 16, 2015
filing date -
Jul 22, 2014
priority date (Note) -
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Abstract
A blade cascade for a gas turbine, which has a first group with at least two, in particular at least three, first blade arrangements of the same type to one another, on which first element arrangements that are identical to one another and have at least one first element are movably mounted; and a second group with at least two, in particular at least three, second blade arrangements, which are of the same type to one another and are of different type from the first blade arrangements, on which second element arrangements, which are identical to one another and have at least one second element are movably mounted, wherein first and second element arrangements are different from each other.
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