Gas turbine engine wall assembly interface
US-2016377296-A1 · Dec 29, 2016 · US
US10533747B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10533747-B2 |
| Application number | US-201715474004-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 30, 2017 |
| Priority date | Mar 30, 2017 |
| Publication date | Jan 14, 2020 |
| Grant date | Jan 14, 2020 |
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An additively manufactured fastener and a method of manufacturing the same are provided. The fastener includes a shank defining an internal passageway and a head defining a distribution plenum in fluid communication with the internal passageway. The head further defines a cooling face defining a plurality of cooling holes for receiving a flow of cooling air from the internal passageway and the distribution plenum. In addition, an impingement baffle is positioned in the distribution plenum and defines impingement holes for directing the flow of cooling air onto the cooling face.
Opening claim text (preview).
What is claimed is: 1. An additively manufacturing fastener defining a centerline, the fastener comprising: a shank extending along the centerline and defining an internal fluid passageway; and a head attached to the shank and defining a distribution plenum in fluid communication with the internal fluid passageway, the head comprising a cooling face defining a plurality of cooling holes in fluid communication with the distribution plenum; and an impingement baffle positioned within the distribution plenum and spaced apart from the cooling face along the centerline, the impingement baffle defining a plurality of impingement holes. 2. The fastener of claim 1 , wherein the shank defines a fluid inlet in fluid communication with the internal fluid passageway. 3. The fastener of claim 1 , wherein the head of the fastener defines a mating face positioned opposite the cooling face along the centerline, the mating face defining one or more fluid inlets in fluid communication with the distribution plenum. 4. The fastener of claim 1 , wherein the cooling holes extend through the cooling face substantially parallel to the centerline. 5. The fastener of claim 1 , wherein the cooling holes extend through the cooling face at an angle relative to the centerline. 6. The fastener of claim 1 , wherein the impingement holes extend through the impingement baffle substantially parallel to the centerline. 7. The fastener of claim 1 , wherein the head defines a perimeter extending along an outermost portion of the head along a radial direction perpendicular to the centerline, and wherein the head defines at least one perimeter cooling passageway that extends through the impingement baffle at an angle relative to the centerline to direct a flow of cooling fluid onto the perimeter. 8. The fastener of claim 1 , further comprising a bypass air passageway that extends through the impingement baffle and the cooling face, the bypass air passageway being in fluid communication with the internal passageway. 9. The fastener of claim 1 , further comprising one or more support structures positioned within the distribution plenum. 10. The fastener of claim 1 , wherein the shank is threaded or defines a groove for receiving a snap ring. 11. The fastener of claim 1 , wherein the shank or the head define a means for fastening the fastener including at least one of a hole for receiving a cotter pin, an upset end for rivet, a swage fastener, or a keyed insert. 12. The fastener of claim 1 , wherein the fastener is positioned within a combustion section of a gas turbine engine, the fastener passing through a combustor liner and defining a central bypass passageway in fluid communication with a combustion chamber for providing dilution air. 13. The fastener of claim 1 , wherein a first portion of the fastener is formed from a first material and a second portion of the fastener is formed from a second material, the second material being different from the first material. 14. The fastener of claim 1 , wherein the fastener comprises a plurality of layers defined along the centerline of the fastener, each of the plurality of layers being formed by: depositing a layer of additive material on a bed of an additive manufacturing machine; and selectively directing energy from an energy source onto the layer of additive material to fuse a portion of the additive material. 15. A method of manufacturing a fastener, the method comprising: depositing a layer of additive material on a bed of an additive manufacturing machine; and directing energy from an energy source onto the layer of additive material to fuse a portion of the additive material and form the fastener, the fastener comprising: a shank extending along the centerline and defining an internal fluid passageway; and a head attached to the shank and defining a distribution plenum in fluid communication with the internal fluid passageway, the head comprising a cooling face defining a plurality of cooling holes in fluid communication with the distribution plenum; and an impingement baffle positioned within the distribution plenum and spaced apart from the cooling face along the centerline, the impingement baffle defining a plurality of impingement holes. 16. The method of claim 15 , further comprising: forming on the shank or the head a means for fastening the fastener including at least one of a hole for receiving a cotter pin, an upset end for rivet, a swage fastener, or a keyed insert. 17. The method of claim 15 , further comprising: forming an impingement baffle spaced apart from the cooling face along the centerline, the impingement baffle defining a plurality of impingement holes. 18. The method of claim 15 , further comprising: forming one or more support structures positioned within the head of the fastener. 19. The method of claim 15 , wherein the shank and the head are integrally formed as a single monolithic component.
Manufacturing combustion chamber liners or subparts · CPC title
Laser welding · CPC title
Combustors or associated equipment · CPC title
with deposition of material · CPC title
Support structures; Attaching or mounting means · CPC title
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