Method of fabricating a turbine engine shaft

Patent metadata

Field	Value
Publication number	US-9429034-B2
Application number	US-201214367076-A
Country	US
Kind code	B2
Filing date	Dec 7, 2012
Priority date	Dec 23, 2011
Publication date	Aug 30, 2016
Grant date	Aug 30, 2016

Abstract

A method of fabricating a turbine engine shaft from a metal billet of generally cylindrical shape, the method including drilling the billet to form a through axial cylindrical bore therein, engaging a cylindrical insert in the bore, the insert being made of a material having yield stress close to that of the material of the billet so that the materials of the insert and of the billet have substantially the same behavior during forging, hot forging the billet to form a forged blank of length greater than that of the billet, withdrawing the insert, and machining the blank.

First claim

The invention claimed is:

1. A method of fabricating a turbine engine shaft from a metal billet of a generally cylindrical shape, the method comprising:
hot forging the billet to form a blank of a greater length than a length of the billet;
machining the blank; and
prior to the forging, one of a boring and drilling comprising respectively boring and drilling the billet to form an at least partially through axial cylindrical bore in the billet, and removably engaging an insert in the bore, the insert being of a substantially cylindrical shape complementary to a shape of the bore and being made of a material having yield stress during forging that is close to yield stress of a material of the billet such that the materials of the insert and of the billet have substantially a same behavior during forging; and
after the forging, withdrawing the insert, the material of the insert having a coefficient of thermal expansion that is lower than that of the blank, such that the insert is withdrawn from the blank by one of a heating and a cooling comprising respectively heating and cooling the blank and the insert, and then by moving the insert in an axial translation relate to the blank.

2. A method according to claim 1 , wherein an outer cylindrical surface of the insert is coated in a thin layer of at least one of a barrier substance and an anti-adhesive substance, which substance withstands temperatures at which the billet is forged.

3. A method according to claim 1 , wherein the insert is engaged in the bore of the billet at ambient temperature.

4. A method according to claim 1 , wherein the insert is axially retained in the bore of the billet at at least one of axial ends.

5. A method according to claim 1 , wherein the insert is made of NC19FeNb and the billet is made of one of X25NiCoCr1313-6-4 steel and X1NiCoMo18-8-5 steel.

6. A method according to claim 1 , wherein the step of removably engaging the insert in the bore comprises engaging the insert having a first diameter in the bore having a second diameter which is the same as the first diameter.

Assignees

• Snecma

Inventors

• Leblanc Jonathan

Classifications

• B21K3/00

  Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like · CPC title

• B21K1/063 Primary

  hollow (hollow racks B21K1/768) · CPC title

• F01D25/00 Primary

  Component parts, details, or accessories, not provided for in, or of interest apart from, other groups · CPC title

• Y10T29/49229

  Prime mover or fluid pump making · CPC title

• F05D2230/25

  by forging · CPC title