Anti-deflection feature for additively manufactured thin metal parts and method of additively manufacturing thin metal parts

US10094240B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10094240-B2
Application numberUS-201514620256-A
CountryUS
Kind codeB2
Filing dateFeb 12, 2015
Priority dateFeb 12, 2015
Publication dateOct 9, 2018
Grant dateOct 9, 2018

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 conduction riser additively manufactured onto thin metal parts, the conduction riser extending in a build direction of the thin metal part and traversing the thin metal part as the conduction riser extends in the build direction. The conduction riser transferring heat from the upper layers of additively manufactured part during manufacturing, preventing thermal deflection of the part.

First claim

Opening claim text (preview).

The invention claimed is: 1. A gas turbine component comprising: a thin metal part, the thin metal part manufactured with an additive manufacturing process, wherein the thin metal part is an impingement baffle, the impingement baffle comprising: a supply side disposed opposite an exit side; a conduction riser joined to the supply side of the impingement baffle, the conduction riser and the impingement baffle concurrently manufactured with the additive manufacturing process; and a plurality of impingement holes extending through the impingement baffle from the supply side to the exit side, wherein at least one impingement holes of the plurality of impingement holes extends through the conduction riser, and wherein the at least one impingement hole is configured to direct a flow of cooling air onto a second gas turbine component. 2. The gas turbine component of claim 1 , wherein the conduction riser comprises a continuous bulge projecting from the supply side of the impingement baffle. 3. The gas turbine component of claim 2 , wherein the continuous bulge has a triangularly-shaped cross-section with fillets. 4. The gas turbine component of claim 1 , wherein the conduction riser extends in a build direction of the thin metal part. 5. The gas turbine component of claim 1 , wherein the conduction riser traverses the supply side of the impingement baffle. 6. The gas turbine component of claim 5 , wherein at least a portion of the conduction riser forms an undulating conduction path. 7. The gas turbine component of claim 1 , wherein the thin metal part and the conduction riser are made from one of nickel and a nickel alloy. 8. The gas turbine component of claim 1 , wherein a ratio of a thickness of the conduction riser to a thickness of the thin metal part is 1:1 to 1.3:1, inclusive. 9. A conduction riser for an additively manufactured impingement baffle, the conduction riser comprising: a projection additively manufactured onto a supply side surface of the additively manufactured impingement baffle, the projection normal to the supply side surface; the projection traversing the supply side surface of the impingement baffle; and the projection having a continuous cross-section; wherein at least one impingement hole extends through the projection to an exit side of the additively manufactured impingement baffle, the at least one impingement hole configured to direct a flow of cooling air onto a gas turbine component. 10. The conduction riser of claim 9 , wherein the continuous cross-section is a triangularly-shaped cross-section with fillets. 11. The conduction riser of claim 9 further comprising: a ratio of a thickness of the conduction riser to a thickness of the additively manufactured impingement baffle is 1:1 to 1.3:1, inclusive. 12. The conduction riser of claim 9 , wherein the conduction riser extends in a build direction of the impingement baffle. 13. The conduction riser of claim 9 , wherein at least a portion of the conduction riser forms an undulating conduction path.

Assignees

Inventors

Classifications

  • Data acquisition or data processing · CPC title

  • Cooling means · CPC title

  • by mechanical means · CPC title

  • by thermal means (control of energy beam parameters for post heating B22F10/364) · CPC title

  • characterised by structural features · 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 US10094240B2 cover?
A conduction riser additively manufactured onto thin metal parts, the conduction riser extending in a build direction of the thin metal part and traversing the thin metal part as the conduction riser extends in the build direction. The conduction riser transferring heat from the upper layers of additively manufactured part during manufacturing, preventing thermal deflection of the part.
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F01D25/12. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Oct 09 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).