Manufacturing of a turbomachine impeller by assembling a plurality of tubular components
US-10697465-B2 · Jun 30, 2020 · US
US12083600B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12083600-B2 |
| Application number | US-202117179526-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 19, 2021 |
| Priority date | Feb 24, 2020 |
| Publication date | Sep 10, 2024 |
| Grant date | Sep 10, 2024 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A method of fabricating a component is described and involves retaining a canister as an integral part of the component after performing an isostatic pressing process. The method comprises: providing a canister having a canister wall that encloses an internal cavity, the canister wall comprising at least a first wall section and a second wall section, where the first wall section and the second wall section are of different materials; filling the internal cavity with a powdered material; performing an isostatic pressing process on the filled canister to consolidate the powder; and retaining the canister as an integral part of the component such that an internal structure of the component comprises the consolidated powder and the canister wall forms at least part of a surface of the component that covers the internal structure.
Opening claim text (preview).
We claim: 1. A method of manufacturing a component, the method comprising the steps of: providing a canister that encloses an internal cavity, the canister comprising at least a first wall and a second wall, wherein: the first wall and the second wall are of different materials; the first wall has only one first thickness throughout an entire length of the first wall that is different than only one second thickness throughout an entire length of the second wall; and at least a section of the canister that is provided is pre-coated; filling the internal cavity with a powdered material; performing an isostatic pressing process on the canister that is filled to consolidate the powdered material; and retaining the canister as an integral part of the component such that an internal structure of the component comprises the consolidated powder material and the canister forms at least part of a surface of the component that covers the internal structure, wherein: the at least the section of the canister is provided pre-coated such that, after performing the isostatic pressing process, at least part of the component is coated. 2. The method of claim 1 , wherein at least a section of the canister is provided for use as cladding of the component such that, after performing the isostatic pressing process, at least part of the component is clad. 3. The method of claim 1 , wherein the component is a blade for a gas turbine engine. 4. The method of claim 1 , wherein the component is or forms part of a vessel. 5. The method of claim 1 , wherein providing the canister comprises fabricating the canister. 6. The method of claim 1 , wherein one or more further components is or are placed in the internal cavity of the canister before the internal cavity is filled with a powdered material. 7. The method of claim 1 , wherein performing the isostatic pressing process comprises sealing the canister that is filled and subjecting the canister that is filled to high pressure conditions from 100-150 MPa. 8. The method of claim 1 , wherein the first wall is made of steel, the second wall is a nickel alloy and the coating is a hydrophobic coating, an aluminide coating, a coating comprising aluminium or chromium, or a ceramic coating. 9. The method of claim 1 , wherein the second wall includes a first sub-section and a second sub-section that have a same thickness and have different material properties and that are joined together by a weld. 10. The method of claim 1 , wherein the canister comprises a third wall that connects the first wall to the second wall and has a third thickness that is different than the first thickness and the second thickness. 11. The method of claim 2 , wherein the section provided for use as cladding comprises stainless steel, a nickel based alloy, an aluminide, a ceramic, aluminium or chromium. 12. The method of claim 4 , wherein the second wall is opposite the first wall, at least a part of the internal cavity being defined between the first wall and the second wall, and wherein the first wall of the canister that is retained forms part of an external surface of the vessel and the second wall of the canister that is retained forms part of an internal surface of the vessel. 13. The method of claim 12 , wherein the second wall is formed of or coated in a corrosion resistant material. 14. The method of claim 6 , wherein the one or more further components comprises a metal plate.
of articles with cavities or holes, not otherwise provided for in the preceding subgroups · CPC title
of turbine blades · CPC title
by applying fluid pressure {, e.g. by cold isostatic pressing [CIP]} · CPC title
Container manufacturing · CPC title
of composite workpieces or articles from parts, e.g. to form tipped tools {(B22F7/002 takes precedence)} · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.