Aluminum airfoil
A method of making an aluminum airfoil includes brazing a first airfoil piece and a second airfoil piece together using a braze material that includes an element selected from magnesium and zinc, to form a braze joint between the first airfoil piece and the second airfoil piece. At least one of the first airfoil piece or the second airfoil piece has an aluminum alloy composition that includes greater than 0.8% by weight of zinc.
1. A method of making an aluminum airfoil, the method comprising:
brazing a first airfoil piece and a second airfoil piece together using a braze material that includes an element selected from a group consisting of magnesium and zinc, to form a braze joint between the first airfoil piece and the second airfoil piece, and at least one of the first airfoil piece and the second airfoil piece has an aluminum alloy composition comprising greater than 0.8% by weight of zinc, wherein the one of the first airfoil piece and the second airfoil piece that is not the aluminum alloy composition is formed of a non-aluminum alloy.
2. The method as recited in claim 1 , wherein at least one of the first airfoil piece and the second airfoil piece includes an airfoil suction side surface or an airfoil pressure side surface.
3. The method as recited in claim 1 , wherein the aluminum alloy composition includes greater than 4% by weight of the zinc.
4. The method as recited in claim 1 , wherein the aluminum alloy composition includes greater than 5% by weight of the zinc.
5. The method as recited in claim 1 , wherein the aluminum alloy composition includes greater than 7% by weight of the zinc.
6. The method as recited in claim 1 , wherein the brazing of the first airfoil piece and the second airfoil piece enclose a hollow cavity between the first airfoil piece and the second airfoil piece.
7. The method as recited in claim 1 , wherein the brazing includes heating the first airfoil piece, the second airfoil piece and the braze material at a temperature that is 450° C.-550° C.
8. The method as recited in claim 1 , including brazing in a vacuum environment.
9. The method as recited in claim 1 , wherein the brazing of the first airfoil piece and the second airfoil piece includes compressing and heating the first airfoil piece and the second airfoil piece in a die.
10. The method as recited in claim 1 , wherein the braze material includes 40 to 65 weight percent zinc and a balance of magnesium.
11. The method as recited in claim 1 , wherein the braze material includes 93 to 100% by weight of zinc and a balance of magnesium.
12. The method as recited in claim 1 , wherein the braze material includes greater than 54% by weight zinc and a balance of aluminum.
13. A aluminum airfoil comprising:
a first airfoil piece; and
a second airfoil piece bonded to the first airfoil piece at a braze joint that includes an element selected from a group consisting of magnesium and zinc,
at least one of the first airfoil piece and the second airfoil piece has an aluminum alloy composition comprising greater than 0.8% by weight of zinc, wherein the one of the first airfoil piece and the second airfoil piece that is not the aluminum alloy composition is formed of a non-aluminum alloy, and
the first airfoil piece and the second airfoil piece defining a cavity there between, the cavity having a series of distinct pockets.
14. The aluminum airfoil as recited in claim 13 , wherein the aluminum alloy composition includes greater than 4% by weight of the zinc.
15. The aluminum airfoil as recited in claim 13 , wherein at least one of the first airfoil piece and the second airfoil piece includes an airfoil pressure side surface or an airfoil suction side surface.
16. A gas turbine engine comprising:
a fan;
a compressor section downstream from the fan;
a combustor in fluid communication with the compressor section; and
a turbine section in fluid communication with the combustor, and
at least one of the fan or the compressor section including an aluminum airfoil that has a first airfoil piece and a second airfoil piece bonded to the first airfoil piece at a braze joint that includes an element selected from a group consisting of magnesium and zinc, at least one of the first airfoil piece and the second airfoil piece has an aluminum alloy composition comprising greater than 0.8% by weight of zinc, wherein the one of the first airfoil piece and the second airfoil piece that is not the aluminum alloy composition is formed of a non-aluminum alloy, and the first airfoil piece and the second airfoil piece defining a cavity there between, the cavity having a series of distinct pockets.
17. The gas turbine engine as recited in claim 16 , where the aluminum alloy composition includes greater than 4% by weight of the zinc.
18. The aluminum airfoil as recited in claim 13 , including at least one insert in at least one of the pockets.
19. The aluminum airfoil as recited in claim 18 , wherein the at least one insert includes a spar.
20. The aluminum airfoil as recited in claim 18 , wherein the at least one insert includes a foam material.
21. The aluminum airfoil as recited in claim 18 , wherein the at least one insert includes structurally supports at least one of the first airfoil piece or the second airfoil piece.
22. The aluminum airfoil as recited in claim 18 , wherein the at least one insert is formed of a non-aluminum alloy.
23. The method as recited in claim 1 , including, prior to heating to the brazing temperature, applying a layer of the braze material exclusively onto bonding surfaces on at least one of the first airfoil piece or the second airfoil piece.