Invention Grant
- Patent Title: Variable pitch change control method
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Application No.: US15962550Application Date: 2018-04-25
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Publication No.: US10934866B2Publication Date: 2021-03-02
- Inventor: Patrick Bailey
- Applicant: Rolls-Royce North American Technologies Inc.
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies Inc.
- Current Assignee: Rolls-Royce North American Technologies Inc.
- Current Assignee Address: US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D7/00
- IPC: F01D7/00 ; F04D29/36 ; F02K3/06 ; F04D29/32 ; B64C11/32

Abstract:
A gas turbine engine includes a fan having a plurality of fan blades configured to rotate about a central axis of the gas turbine engine. Each fan blade is configured to pivot about a pivot axis that extends radially away from the central axis to vary a pitch of the fan blade. The fan further includes a counterforce system configured to resist forces that urge the fan blades away from their pitch positions during operation of the gas turbine engine.
Public/Granted literature
- US20180363481A1 VARIABLE PITCH CHANGE CONTROL METHOD Public/Granted day:2018-12-20
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