Repair methods utilizing additively manufacturing for rotor blades and components
US-2017106482-A1 · Apr 20, 2017 · US
US9914172B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9914172-B2 |
| Application number | US-201514887459-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 20, 2015 |
| Priority date | Oct 20, 2015 |
| Publication date | Mar 13, 2018 |
| Grant date | Mar 13, 2018 |
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 joining two components using additive manufacturing is provided. The method includes forming a first component made of a first material; forming an interlocking transition zone from the first material and a second material; and forming a second component made of the second material. The interlocking transition zone includes a plurality of projections alternately extending from the first component and the second component, respectively, to undetachably couple the first component and the second component.
Opening claim text (preview).
What is claimed: 1. An additively manufactured component, comprising: a first component comprising a plurality of fused layers of a first material; a second component comprising a plurality of fused layers of a second material; and an interlocking transition zone comprising a plurality of projections alternately extending from the first component and the second component, respectively, to undetachably couple the first component and the second component, wherein the first component and the second component are made from a powdered metal, and the plurality of fused layers are formed by a melting process. 2. The additive manufactured component as in claim 1 , wherein at least a portion of adjacent projections between the first component and the second component prevent relative motion between the first component and second component. 3. The additively manufactured component of claim 1 , wherein each of the plurality of projections allow relative motion between the first component and the second component. 4. The additively manufactured component of claim 1 , wherein each projection comprises a shaft extending from the first component or the second component, a distal end of the shaft further comprising a knob having a diameter larger than the diameter of the shaft. 5. The additively manufactured component of claim 1 , wherein the first material is different from the second material. 6. The additively manufactured component of claim 1 , wherein the first component and the second component are made of a polymer material, and the plurality of fused layers are formed by a thermosetting process. 7. The additively manufactured component of claim 1 , wherein the first component and the second component are made of epoxy, and the plurality of fused layers are formed by a crosslinking process. 8. The additively manufactured component of claim 1 , wherein the first component and the second component are made of a ceramic material, and the plurality of fused layers are formed by a sintering process. 9. The additively manufactured component of claim 1 , wherein each of the plurality of projections has a trapezoidal shape that extends from the first component or the second component such that a widest portion of each trapezoid is disposed at a distal end of the projection from the first component or the second component, respectively. 10. The additively manufactured component of claim 1 , wherein the second component is a protective coating. 11. The additively manufactured component of claim 10 , wherein the protective coating is a thermal barrier coating. 12. The additively manufactured component of claim 10 , wherein the protective coating is a bond coat of a thermal barrier coating. 13. The additively manufactured component of claim 1 , wherein the first material has a first coefficient of thermal expansion and the second material has a second coefficient of thermal expansion, wherein the first coefficient of thermal expansion is different than the second coefficient of thermal expansion. 14. The additively manufactured component of claim 1 , wherein the interlocking transition zone has a fluid channel formed therein, wherein the fluid channel is configured to allow a fluid to flow through the interlocking transition zone. 15. The additively manufactured component of claim 1 , wherein a brazed joint is located between the first component and the second component to act as adhesive.
using filamentary material being melted, e.g. fused deposition modelling [FDM] · CPC title
Products made by additive manufacturing · CPC title
Processes of additive manufacturing · CPC title
Use of {EP, i.e.} epoxy resins {or derivatives thereof}, as moulding material · CPC title
Dovetailed interlocking undercuts · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.