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US Patent 8979491 Turbofan mounting arrangement

Patent 8979491 was granted and assigned to Pratt & Whitney Canada on March, 2015 by the United States Patent and Trademark Office.

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Patent Citations Received
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US Patent 11933190 Front section stiffness ratio
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US Patent 11927106 Frame connection between fan case and core housing in a gas turbine engine
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Patent abstract

A gas turbine engine has a rear mounting structure incorporating a mounting apparatus attached to a bypass duct wall with a link device of six rods for transferring core portion related inertia-induced loads, from an inner case of the core portion in a short circuit across an annular bypass air passage to the bypass duct wall.

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Patent Inventor Names
Bryan Olver0
Jeffrey Bernard Heyerman0
Stephen Caulfeild0
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US Patent 11708772 Triangular-frame connection between fan case and core housing in a gas turbine engine
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US Patent 11686220 H-frame connection between fan case and core housing in a gas turbine engine
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US Patent 11674415 Front section stiffness ratio
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US Patent 08979491 Turbofan mounting arrangement US Patent 8979491 Turbofan mounting arrangement

Infobox
Patent Number
08979491
Patent Number
8979491
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=08979491
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Website URL
https://pdfpiw.uspto.gov/.piw?Docid=08979491
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 US Patent 08979491 Turbofan mounting arrangement

Infobox
Is a
Patent
Patent
Current assignee
Pratt & Whitney Canada
Pratt & Whitney Canada
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
08979491
Date of patent
March 17, 2015
Patent application number
13289067
Date Filed
November 4, 2011
Patent primary examiner
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Edward Look

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