Bachman & LaPointe, P.C.
Segmented rim seal spacer for a gas turbine engine
A seal segment for a gas turbine engine includes a first axial span that extends between the first radial span and the second radial span. A second axial span extends between the first radial span and the second radial span, the first radial span, the second radial span, the first axial span and the second axial span forming a torque box.
United Technologies Corporation
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David R Julian Gabriel L James D. Gregory M Brian D
Pack Partyka Suciu Hill Dolansky Merry