US Patent 7090165 Aeroengine nacelle
Patent 7090165 was granted and assigned to Rolls-Royce on August, 2006 by the United States Patent and Trademark Office.
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Patent abstract
A nacelle (55) for a gas turbine engine (10), the engine (10) comprising accessories (34) mounted to a fan casing (28) and a core engine (9), the nacelle (55) substantially surrounds the engine (10) and comprises an intake (12) and a thrust reverser unit (31). The thrust reverser unit (31) is formed by two generally C-shaped portions (31a, 31b). The thrust reverser unit (31) is openable to provide access to the accessories (34) and the core engine (9). The nacelle (55) further comprises a fan containment casing (33) that is integral with the intake (12).
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US Patent 07090165 Aeroengine nacelle US Patent 7090165 Aeroengine nacelle
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Patent Number
0709016500
Patent Number
709016500
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Is a
Current Assignee
Patent Jurisdiction
Patent Number
070901650
Date of Patent
August 15, 2006
0Patent Application Number
106979450
Date Filed
October 31, 2003
0Official Website
Patent Primary Examiner
Edits on 25 Sep, 2022
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
070901650
Date of Patent
August 15, 2006
0Patent Application Number
106979450
Date Filed
October 31, 2003
0Official Website
Patent Primary Examiner
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US Patent 07090165 Aeroengine nacelle
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
07090165
Date of patent
August 15, 2006
Patent application number
10697945
Date Filed
October 31, 2003
Patent primary examiner
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