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US Patent 11466697 Fan module comprising variable-pitch blades

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Contents

Is a
Patent
Patent

Patent attributes

Patent Applicant
Safran
Safran
Current Assignee
Safran
Safran
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
11466697
Date of Patent
October 11, 2022
Patent Application Number
17283496
Date Filed
October 10, 2019
Patent Citations
‌
US Patent 11052994 System for changing the pitch of a turboprop engine comprising an upstream pair of contrarotating propellers
‌
US Patent 10393137 Method and system for integrated pitch control mechanism actuator hydraulic fluid transfer
‌
US Patent 10479514 Assembly for turbine machine with open rotor contra-rotating propellers, comprising a small duct for the passage of ancillaries
‌
US Patent 10584641 Turbine engine with a pair of contrarotating propellers placed upstream of the gas generator
‌
US Patent 11221017 Method and system for integrated pitch control mechanism actuator hydraulic fluid transfer
Patent Primary Examiner
‌
Richard A. Edgar
CPC Code
‌
F01D 7/00
‌
F01D 25/16
‌
F02C 7/36
‌
F04D 29/323
‌
F04D 29/056
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F01D 25/162
‌
B64C 11/38

A fan module including variable-pitch blades, a fan rotor bearing the blades of the fan, each mounted to pivot about a pitch axis; a fan shaft extending along a longitudinal axis X inside the fan rotor and driving the fan rotor in rotation. A power shaft drives the fan shaft with a planetary gear speed reducer At least a first and a second bearing guide the rotation of the fan rotor, housed inside a lubrication chamber. A system varies the pitch of the fan blades, including a connecting mechanism connected to the blades of the fan and a controller acting on the connecting mechanism. The first bearing is disposed upstream of the speed reducer and the second bearing is disposed downstream of the speed reducer. The fan rotor is connected to the fan shaft by an annular trunnion extending at least along an upstream portion of the lubrication chamber.

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