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US Patent 7360769 Sealing arrangement

Patent 7360769 was granted and assigned to Rolls-Royce on April, 2008 by the United States Patent and Trademark Office.

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Patent Citations Received
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US Patent 12104533 Methods and apparatus for gas turbine frame flow path hardware cooling
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edited on 10 Apr, 2024
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US Patent 11953095 Flexible seal assembly
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edited on 21 Mar, 2024
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US Patent 11933403 Metallic sealing assembly for sealing between a rotating shaft and a fixed frame
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Edits on 22 Feb, 2024
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edited on 22 Feb, 2024
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US Patent 11905842 Partition damper seal configurations for segmented internal cooling hardware
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Patent Inventor Names
Stephen P. Bennett0
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Patent abstract

A sealing arrangement, for example between adjacent nozzle guide vane platform segments (2A, 2B) in a gas turbine engine, comprises a seal (12) which extends across a gap (13) between the platform segments (2A, 2B) and engages, at opposite ends, in grooves (8A, 8B). The seal (12) comprises a web element (14) having recesses (20A, 20B) at its opposite edges, which receive sealing elements (16A, 16B). The sealing elements (16A, 16B) may comprise a braided amorphous silica yarn or other filamentary temperature-resistant material.

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US Patent 07360769 Sealing arrangement US Patent 7360769 Sealing arrangement

Infobox
Patent Number
07360769
Patent Number
7360769
Edits on 19 May, 2023
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=07360769
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Website URL
https://pdfpiw.uspto.gov/.piw?Docid=07360769
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 US Patent 07360769 Sealing arrangement

Infobox
Is a
Patent
Patent
Current assignee
Rolls-Royce
Rolls-Royce
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
07360769
Date of patent
April 22, 2008
Patent application number
11636582
Date Filed
December 11, 2006
Patent primary examiner
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Alison K. Pickard

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