Split airfoil cluster and method therefor
US-2015369072-A1 · Dec 24, 2015 · US
US9855626B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9855626-B2 |
| Application number | US-201514609162-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 29, 2015 |
| Priority date | Jan 29, 2015 |
| Publication date | Jan 2, 2018 |
| Grant date | Jan 2, 2018 |
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A manufacturing method is provided which utilizes a laser system. During an embodiment of this method, an object is arranged relative to a head of the laser system. A pattern of holes are formed in the object by ablating the object with a plurality of laser beams which are directed from the head.
Opening claim text (preview).
We claim: 1. A manufacturing method utilizing a laser system, comprising: arranging an object relative to a head of the laser system, wherein the head includes a laser beam multiplexer; and concurrently forming a pattern of holes in the object by ablating the object with a plurality of laser beams which are directed from the head, wherein at least some of the laser beams are incident with the laser beam multiplexer; and translating the laser beam multiplexer to adjust inter hole spacing of the pattern of holes; wherein the object is configured as at least a portion of an acoustic panel. 2. The manufacturing method of claim 1 , wherein the pattern of holes is a rectangular array of holes. 3. The manufacturing method of claim 1 , wherein the object comprises a fiber-reinforced composite. 4. The manufacturing method of claim 1 , wherein the laser beam multiplexer redirects at least some of the laser beams such that the laser beams are directed on substantially parallel trajectories. 5. The manufacturing method of claim 1 , further comprising: moving the head from a first position to a second position, wherein the pattern of holes is formed while the head is in the first position; and forming another pattern of holes in the object by ablating the object with a plurality of laser beams which are directed from the head while the head is in the second position. 6. A manufacturing method utilizing a laser system, comprising: arranging an object relative to a head of the laser system; forming a pattern of apertures in the object by ablating the object with a plurality of laser beams which are directed from the head; wherein the head includes a laser beam multiplexer which redirects at least some of the laser beams such that the laser beams are directed on substantially parallel trajectories; and translating the laser beam multiplexer to adjust inter hole spacing of the pattern of holes. 7. The manufacturing method of claim 6 , wherein the laser beam multiplexer comprises a prismatic mirror with which at least some of the laser beams are incident. 8. The manufacturing method of claim 6 , wherein the pattern of apertures comprises a pattern of four holes. 9. The manufacturing method of claim 6 , wherein the pattern of apertures comprises a pattern of nine holes. 10. The manufacturing method of claim 6 , wherein the object comprises a fiber-reinforced composite. 11. The manufacturing method of claim 6 , wherein the object is configured as at least a portion of an acoustic panel for a turbine engine. 12. The manufacturing method of claim 6 , wherein the laser system includes a plurality of lasers, each laser generates a respective one of the laser beams, and each laser beam ablates the object to foul′ a respective one of the apertures in the pattern. 13. The manufacturing method of claim 6 , wherein the pattern of apertures is a rectangular array of holes. 14. The manufacturing method of claim 1 , wherein a first of the laser beams is incident with a first surface of the laser beam multiplexer; and a second of the laser beams is incident with a second surface of the laser beam multiplexer that is positioned opposite the first surface. 15. The manufacturing method of claim 1 , wherein the laser system includes a plurality of lasers, and each of the lasers generates a respective one of the laser beams; a first of the lasers is configured to direct a respective one of the laser beams onto a first side of the laser beam multiplexer; and a second of the lasers is configured to direct a respective one of the laser beams onto a second side of the laser beam multiplexer that is opposite the first side. 16. The manufacturing method of claim 1 , wherein the laser system includes a plurality of lasers, each of the lasers generates a respective one of the laser beams; an end portion of an optical fiber of a first of the lasers is positioned on a first side of the laser beam multiplexer; and an end portion of an optical fiber of a second of the lasers is positioned on a second side of the laser beam multiplexer.
by boring · CPC title
Scanning systems, i.e. devices involving movement of the laser beam relative to the laser head · CPC title
involving non-metallic material, e.g. isolators · CPC title
Inorganic materials other than metals or composite materials · CPC title
Composite materials · CPC title
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