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Patent Searching and Data


Title:
Pitch control assembly
Document Type and Number:
Japanese Patent JP6118460
Kind Code:
B2
Abstract:
A method of controlling a propeller assembly, having a blade, piston end cap, and piston, with a pitch control unit, having a transfer bearing and a blade angle unit, the method comprising: axially moving a transfer tube relative to and circumscribing the transfer bearing, and sensing an axial movement of the transfer tube with the blade angle unit.

Inventors:
Carrington, Christopher Roy
Application Number:
JP2016519859A
Publication Date:
April 19, 2017
Filing Date:
October 07, 2013
Export Citation:
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Assignee:
GE AVIATION SYSTEMS LIMITED
International Classes:
B64C11/38
Domestic Patent References:
JP2002513705A
Foreign References:
US5186608
WO1998022340A1
EP2261115A2
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka