Method for manufacturing a propeller reduction gear

Patent metadata

Field	Value
Publication number	US-10047849-B2
Application number	US-201615543106-A
Country	US
Kind code	B2
Filing date	Jan 12, 2016
Priority date	Jan 13, 2015
Publication date	Aug 14, 2018
Grant date	Aug 14, 2018

Abstract

A method for manufacturing a propeller reduction gear, which includes measuring manufacturing defects of the casing; calculating a first angular play induced at each intermediate gear by the measured manufacturing defects; estimating a second angular play induced at each intermediate gear by deformations of the casing when the reduction gear transmits a threshold torque; calculating a total angular play from the first angular play and the second angular play; and selecting two intermediate gears with a phase difference that compensates for the total angular play.

First claim

The invention claimed is:

1. A method for manufacturing a propeller reduction gear including:
a casing including at least two front bearing seatings and two rear bearing seatings;
an input gear;
at least two intermediate gears, each intermediate gear including a first stage meshing with the input gear and a second stage, each intermediate gear being attached to the casing via at least one front bearing and one rear bearing, each front bearing being supported by one of the at least two front bearing seatings, each rear bearing being supported by one of the at least two rear bearing seatings;
an output gear wheel meshing with the second stage of each of the at least two intermediate gears;
the method comprising:

(a) measuring manufacturing defects of the casing;
(b) calculating a first angular play induced at each intermediate gear from the measured manufacturing defects;
(c) estimating a second angular play induced at each intermediate gear by deformations of the casing upon transmitting a threshold torque by the reduction gear;
(d) calculating a total angular play from the first angular play and the second angular play;
(e) selecting two intermediate gears having a phasing difference compensating for the total angular play; and
(f) manufacturing the propeller reduction gear using the selected two intermediate gears.

2. The method according to claim 1 , wherein step (a) of measuring defects includes a step of measuring a real position of each bearing seating.

3. The method according to claim 2 , wherein step (b) of calculating the first angular play includes:
for each bearing seating, calculating a difference between the real position of the bearing seating and a reference position so as to obtain a bearing seating offset;
for each intermediate gear:
calculating an offset of the intermediate gear from the bearing seating offsets supporting the bearings of the intermediate gear;
calculating the first angular play from the offset of the intermediate gear.

4. The method according to claim 1 , wherein step (c) of estimating the second angular play includes:
estimating a displacement of each bearing seating upon transmitting a threshold torque by the reduction gear;
for each intermediate gear:
calculating a displacement of the first stage from the displacements of the bearing seatings supporting the bearings of this intermediate gear; and
calculating a second angular play from the calculated displacements.

Assignees

• Safran Trans Systems

Inventors

• Mathieu Antoine
• Feraud Benjamin

Classifications

• F02C7/36 Primary

  Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title

• F16H57/023 Primary

  Mounting or installation of gears or shafts in the gearboxes, e.g. methods or means for assembly · CPC title

• F05D2230/60

  Assembly methods · CPC title

• Y10T29/49771

  Quantitative measuring or gauging · CPC title

• Y10T29/49696

  Mounting · CPC title