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US Patent 8083482 Method and system for limiting blade pitch

Patent 8083482 was granted and assigned to GE Aviation Systems on December, 2011 by the United States Patent and Trademark Office.

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Patent Citations Received
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US Patent 12103702 Removeable fuselage shield for an aircraft
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US Patent 11834196 System and method for control for unducted engine
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Patent abstract

A method for limiting blade pitch is provided. The method includes providing a brake assembly that is actuatable to limit blade pitch, providing a limit stop assembly including a stop wheel and a traveler movable relative to the stop wheel, and coupling the limit stop assembly to the brake assembly such that the limit stop assembly actuates the brake assembly when the traveler engages the stop wheel.

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Patent Inventor Names
Mark Serven0
Ronald W. Rapp0
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US Patent 11702188 Bistable pitch propeller system with bidirectional propeller rotation
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US Patent 08083482 Method and system for limiting blade pitch US Patent 8083482 Method and system for limiting blade pitch

Infobox
Patent Number
080834820
Patent Number
80834820
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edited on 23 Sep, 2022
Infobox
Is a
Patent
Patent
0
Current Assignee
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GE Aviation Systems
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
080834820
Date of Patent
December 27, 2011
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Patent Application Number
122419090
Date Filed
September 30, 2008
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Patent Primary Examiner
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Thomas L. Dickey
0
Edits on 14 Dec, 2021
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created this topic on 14 Dec, 2021
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 US Patent 08083482 Method and system for limiting blade pitch

Infobox
Is a
Patent
Patent
Current assignee
‌
GE Aviation Systems
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
08083482
Date of patent
December 27, 2011
Patent application number
12241909
Date Filed
September 30, 2008
Patent primary examiner
‌
Thomas L. Dickey

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