“System And Method For Propeller Pitch Control”

Abstract: Systems and methods are disclosed for controlling the pitch angle of a propeller and rotor assembly (24, 26) that minimizes circumferential loads and stresses to a pitch angle control system (38). The system (38) may generally include an annular actuator (44), load transfer bearing (LTB) (50), and a guide shaft (64) is pivotally attached to the LTB (50) to direct the LTB (50) along an arcuate path (86) relative to a rotor frame (42). FIGS. 1, 2

Patent Information

Application #

Filing Date

26 August 2016

Publication Number

10/2017

Publication Type

INA

Invention Field

MECHANICAL ENGINEERING

Status

Email

bpo.mail@ge.com

Parent Application

Applicants

GENERAL ELECTRIC COMPANY

1 River Road Schenectady, New York 12345

Inventors

1. TOMASZEWICZ, Piotr Wincenty

Aleja Krakowska 110/114 Warsaw, Masovia 02-256

Specification

SOFT COPY ATTACHED IN PDF

Documents

Application Documents

#	Name	Date
1	PROOF OF RIGHT [26-08-2016(online)].pdf	2016-08-26
2	Power of Attorney [26-08-2016(online)].pdf	2016-08-26
3	Form 5 [26-08-2016(online)].pdf	2016-08-26
4	Form 3 [26-08-2016(online)].pdf	2016-08-26
5	Drawing [26-08-2016(online)].pdf	2016-08-26
6	Description(Complete) [26-08-2016(online)].pdf	2016-08-26
7	abstract-201644029029-jpeg.jpg	2016-09-29
8	Other Patent Document [25-01-2017(online)].pdf	2017-01-25
9	Correspondence by Agent_Assignment Power of Attorney_25-01-2017.pdf	2017-01-25
10	Assignment_As Filed_25-01-2017.pdf	2017-01-25