Method of manufacturing a component

US2018200799A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2018200799-A1
Application numberUS-201815864183-A
CountryUS
Kind codeA1
Filing dateJan 8, 2018
Priority dateJan 13, 2017
Publication dateJul 19, 2018
Grant date

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

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.

First claim

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.

Assignees

Inventors

Classifications

  • 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

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US2018200799A1 cover?
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 th…
Who is the assignee on this patent?
Rolls Royce Plc
What technology area does this patent fall under?
Primary CPC classification B22F7/064. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Jul 19 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).