Gas turbine engine having outlet guide vanes
US-2024418094-A1 · Dec 19, 2024 · US
US9598979B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9598979-B2 |
| Application number | US-201213544140-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 9, 2012 |
| Priority date | Feb 15, 2012 |
| Publication date | Mar 21, 2017 |
| Grant date | Mar 21, 2017 |
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A method for producing a diffusion cooling hole extending between a wall having a first wall surface and a second wall surface includes forming a cooling hole inlet at the first wall surface, forming a cooling hole outlet at the second wall surface, forming a metering section downstream from the inlet and forming a multi-lobed diffusing section between the metering section and the outlet. The inlet, outlet, metering section and multi-lobed diffusing section are formed by laser drilling, particle beam machining, fluid jet guided laser machining, mechanical machining, masking and combinations thereof.
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The invention claimed is: 1. A method for producing a diffusion cooling hole extending between a wall having a first wall surface and a second wall surface, the method comprising: forming a cooling hole inlet at the first wall surface; forming a cooling hole outlet at the second wall surface; forming a metering section downstream from the inlet; and forming a multi-lobed diffusing section between the metering section and the outlet, wherein forming the diffusing section comprises: forming a first lobe that diverges longitudinally and laterally from a center axis of the metering section and has a trailing edge; forming a second lobe that diverges longitudinally and laterally from a center axis of the metering section and has a trailing edge; and forming a third lobe that diverges longitudinally and laterally from a center axis of the metering section and has a trailing edge; wherein the inlet, outlet, metering section and ,multi-lobed diffusing section are formed by a technique selected from the group consisting of laser drilling, particle beam machining, fluid jet guided laser machining, mechanical machining, masking and combinations thereof. 2. The method of claim 1 , wherein the wall comprises a metal or superalloy substrate. 3. The method of claim 1 , wherein the second wall surface comprises a coating, and wherein at least a portion of the cooling hole extends through the coating. 4. The method of claim 3 , wherein the coating comprises: a bond coating; and a thermal barrier coating. 5. The method of claim 4 , wherein a portion of the diffusing section is located within the coating. 6. The method of claim 5 , wherein the entire diffusing section is located within the coating. 7. The method of claim 6 , wherein a portion of the metering section is located within the coating. 8. The method of claim 1 , wherein the inlet and metering section are formed using a first laser having a frequency between about 5 Hz and about 200 kHz and a millisecond (10 −3 ) to nanosecond (10 −9 ) pulse duration range, and wherein the multi-lobed diffusing section and outlet are formed using a second laser having a frequency between about 1 kHz and about 200 kHz and a pulse duration range from nanoseconds (10 −9 ) to femtoseconds (10 −15 ) seconds. 9. The method of claim 8 , wherein the wall comprises a coating on the second wall surface, and wherein at least a portion of the cooling hole extends through the coating. 10. The method of claim 1 , wherein the inlet, metering section, multi-lobed diffusing section and outlet are formed using a fluid jet guided laser. 11. The method of claim 10 , wherein the wall comprises a coating on the second wall surface, and wherein at least a portion of the cooling hole extends through the coating. 12. The method of claim 1 , wherein the inlet, metering section, multi-lobed diffusing section and outlet are formed using a particle beam. 13. The method of claim 12 , wherein the particle beam is an electron beam. 14. The method of claim 12 , wherein the particle beam is an ion beam or molecular beam. 15. The method of claim 13 , wherein the wall comprises a coating on the second wall surface, and wherein at least a portion of the cooling hole extends through the coating. 16. The method of claim 1 , wherein the inlet, metering section, multi-lobed diffusing section and outlet are formed by a technique selected from the group consisting of drilling, milling, grinding, superabrasive machining and combinations thereof. 17. The method of claim 1 , wherein the inlet and metering section are formed by drilling, and wherein the multi-lobed diffusing section and outlet are formed using a laser having a frequency between about 1 kHz and about 200 kHz and a pulse duration range from nanoseconds (10 −9 ) to femtoseconds (10 −15 ). 18. The method of claim 1 , wherein the inlet and metering section are formed using a laser having a frequency between about 5 Hz and about 200 kHz, and a millisecond (10 −3 ) to nanosecond (10 −9 ) pulse duration range, and wherein the multi-lobed diffusing section and outlet are formed by a technique selected from the group consisting of drilling, milling, grinding, superabrasive machining and combinations thereof. 19. The method of claim 3 , wherein the outlet and the portion of the diffusing section extending through the coating are formed by masking. 20. The method of claim 1 , wherein the metering section and the diffusing section are formed using different techniques. 21. The method of claim 1 , wherein the inlet and the metering section are formed before the diffusing section and the outlet. 22. The method of claim 1 , wherein the inlet and the metering section are formed after the diffusing section and the outlet. 23. A method for producing a diffusion cooling hole extending between a wall having a first wall surface and a second wall surface, the method comprising: forming a cooling hole inlet at the first wall surface; forming a cooling hole outlet at the second wall surface; forming a metering section downstream from the inlet; and forming a multi-lobed diffusing section between the metering section and the outlet, wherein forming the diffusing section comprises: forming a first lobe that diverges longitudinally and laterally from a center axis of the metering section and has a trailing edge; forming a second lobe that diverges longitudinally and laterally from a center axis of the metering section and has a trailing edge; and forming a third lobe that diverges longitudinally and laterally from a center axis of the metering section and has a trailing edge; wherein the inlet and metering section are formed by a first technique selected from the group consisting of laser drilling, particle beam machining, fluid jet guided laser machining, mechanical machining and masking, and wherein the outlet and multi-lobed diffusing section are formed by a second technique different from the first technique and selected from the group consisting of laser drilling, particle beam drilling, fluid jet guided laser machining, mechanical machining and masking.
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