Composite tubular woven seal for an inner compressor discharge case
AssigneeGeneral Electric Company
InventorsSrikanth Vedantam, Mahmut Faruk Aksit, Ahmad Safi, Abdul-Azeez Mohammed-Fakir, Ning Fang
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AssigneeGeneral Electric Company
InventorsSrikanth Vedantam, Mahmut Faruk Aksit, Ahmad Safi, Abdul-Azeez Mohammed-Fakir, Ning Fang
Estimating the term…
Upper and lower halves of the inner barrel of a compressor for a turbine are bolted to one another along a horizontal midline joint with metal-to-metal surface contact. Elongated grooves are provided in the margin of one of the barrel halves. Elongated composite tubular woven seals are provided in the grooves, the seals having a diameter in excess of the depth of the grooves. The seals comprise an inner woven metal core surrounded by an annular silica fiber layer, in turn surrounded by a metal foil with an outer protective covering of a braided stainless steel. Upon joining the upper and lower halves, the compliant seal is crushed within the groove, maintaining a seal between the barrel halves in the event of warpage of the compressor casing during turbine operation.
An inner compressor discharge case for a gas turbine, comprising:
An inner compressor discharge case for a gas turbine, comprising:
An inner compressor discharge case for a gas turbine, comprising:
An inner compressor discharge case for a gas turbine, comprising:
Dependencies are inferred from the claim text.