The present invention relates to a method of manufacturing a forging for forming a split casing. It particularly relates to forgings which are used to form the casing for a gas turbine engine.
The current process for forming a gas turbine engine casing is illustrated in
The forging 10 is used to form an axial split casing 20 for a gas turbine engine. It may be formed from corrosive resistant steel, titanium or nickel alloy.
a. A lathe is used to remove material from the interior of the forging 10. The lathe cuts a cylindrical tube of radius R1 centred at (−X1, 0).
b. A lathe is used to remove material from the interior of the forging 10. The lathe cuts a cylindrical tube of radius R1 centred at (X1, 0).
c. A lathe is used to remove material from the exterior of the forging 10. The lathe cuts a cylindrical tube of radius R2 centred at (0, Y2).
d. A lathe is used to remove material from the exterior of the forging 10. The lathe cuts a cylindrical tube of radius R2 centred at (0,−Y2).
In
The forging is then axially split by removing the material between −X1 and +X1 as shown in
The two portions 20a, 20b are then joined as shown in
The rough machining of the interior and exterior of the forging illustrated in
There are several problems associated with the above mentioned process. A considerable amount of material may need to be removed from the interior and the exterior of the forging during the rough machining process. This is a waste of material and also results in excessive wear to the lathes used to perform the rough machining.
It would therefore be desirable to provide an improved process for forming an axial split casing.
According to a first aspect of the present invention there is provided a method of manufacturing a forging for forming a split casing comprising the steps of: creating a forging; and deforming the forging to compress it along a first axis and/or extend it along a second axis perpendicular to the first axis.
For a better understanding of the present invention reference will now be made by way of example only to the following Figs. in which:
The forging 110 illustrated in
The forging 110 of
The deformed forging 110 is then split along the first axis A. The splitting of the deformed cylindrical forging produces first 120a and second 120b portions of an axial split casing 120. When joined the portions 120a, 120b create a substantially cylindrical tubular casing 120 as shown in
Thus, the deformation of the cylindrical forging reduces or obviates the need to perform off-centre rough machining to ensure that portions of the forging, when split and rejoined, form a substantially cylindrical tubular casing. Consequently, the original forging provided in
Although embodiments of the present invention have been described in the preceding paragraphs with reference to various examples, it should be appreciated that modifications to the examples given can be made without the parting from the scope of the invention as claimed. For example, although the deformation of a forging has been described with relation to a cylindrical forging only, it is possible to apply the principle of the invention to other shapes of forging.
Whilst endeavouring in the foregoing specification to draw attention to those features of the invention believed to be of particular importance it should be understood that the Applicant claims protection in respect of any patentable feature or combination of features hereinbefore referred to and/or shown in the drawings whether or not particular emphasis has been placed thereon.
Number | Date | Country | Kind |
---|---|---|---|
0317765.6 | Jul 2003 | GB | national |
This is a continuation of International Application Number PCT/GB2004/002989 filed Jul. 9, 2004, designating the United States.
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Number | Date | Country | |
---|---|---|---|
20060107718 A1 | May 2006 | US |
Number | Date | Country | |
---|---|---|---|
Parent | PCT/GB2004/002989 | Jul 2004 | US |
Child | 11327410 | US |