Method of manufacturing a component of a turbomachine, component of turbomachine and turbomachine
US-2017241429-A1 · Aug 24, 2017 · US
US2018200799A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2018200799-A1 |
| Application number | US-201815864183-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jan 8, 2018 |
| Priority date | Jan 13, 2017 |
| Publication date | Jul 19, 2018 |
| Grant date | — |
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A method of manufacturing a component ( 100 ) having a main part ( 101 ) and a projecting feature ( 104,114 ), the method comprising providing a shaped void ( 210 ) corresponding to the component, locating a pre-formed element ( 214 ) in a feature region of the shaped void which corresponds to the projecting feature, locating powder ( 212 ) within the shaped void; and forming the element and the powder into the component such that the element creates at least a part of the projecting feature.
Opening claim text (preview).
1 . A method of manufacturing a component having a main part and a projecting feature, the method comprising: providing a shaped void corresponding to the component within a canister, the shaped void further comprising a recess to provide a feature region for receiving a pre-formed element to provide the projecting feature; locating the pre-formed element in the feature region of the shaped void which corresponds to the projecting feature such that the pre-formed element only partially fills the feature region such that it can be surrounded by powder within the feature region; locating powder within the shaped void and around the pre-formed element within the feature region; and forming the element and the powder into the component such that the element creates at least a part of the projecting feature. 2 . A method as claimed in claim 1 , wherein the shaped void comprises an annular gap between a first and second canisters or parts. 3 . A method as claimed in either of claim 1 , wherein the recess has a first thickness corresponding to the projecting feature, and a second region having a second thickness less than the first thickness corresponding to the main part. 4 . A method as claimed in claim 1 , wherein the pre-formed element and the powder are formed into the component using a hot isostatic pressing process. 5 . A method as claimed in claim 1 , wherein the pre-formed element is formed of substantially the same material as the powder. 6 . A method as claimed in claim 1 , wherein the pre-formed element is shaped such that a depth of the powder between the pre-formed element and a wall of the shaped void is substantially constant. 7 . A method as claimed in claim 1 , wherein the projecting feature is a boss or duct of the component. 8 . A method as claimed in claim 7 , wherein the boss or duct comprises a bore from an interior to an exterior of the component, and wherein the element comprises a bore cavity which forms at least a part of the bore. 9 . A method as claimed in claim 1 , wherein the component is an aerospace component. 10 . A method as claimed in claim 9 , wherein the component is an engine casing, and wherein the projecting feature is a boss or duct of the engine casing. 11 . A method as claimed in claim 1 , further comprising forming the pre-formed element using hot isostatic pressing. 12 . A method as claimed in claim 1 , wherein the pre-formed element is supported in the feature region by one or more support members of the element. 13 . A method as claimed in claim 12 , wherein the one or more support elements contact the canister. 14 . A method as claimed in claim 1 , wherein the component has a plurality of projecting features, and wherein the pre-formed element is located in each of a plurality of feature regions of the shaped void corresponding to the plurality of projecting features. 15 . A method as claimed in claim 1 , wherein the pre-formed element contacts the canister within the shaped void. 16 . A method as claimed in claim 1 , wherein the pre-formed element is encapsulated by the powder on all sides such that it does not contact the canister.
Machines or parts thereof not otherwise provided for (conveyor belts B29L2031/7092; driving belts B29L2031/7094; bearings B29L2031/04) · CPC title
the parts being joined · CPC title
Pressing by means acting upon the material via flexible mould wall parts, e.g. by means of inflatable cores, isostatic presses (isostatic presses in general B30B5/02) · CPC title
of engine cylinder parts or of piston parts other than piston rings (of piston rings B22F5/02) · CPC title
incorporating preformed parts or layers, e.g. compression moulding around inserts or for coating articles {(B29C43/206 takes precedence)} · CPC title
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