Twin-airfoil blade with spacer strips
View Patent ↗The invention relates to a blade possessing a leading edge and a trailing edge, the blade comprising a first airfoil possessing an inner face and an outer face extending between said leading edge and said trailing edge, a second airfoil possessing an inner face and an outer face extending between said leading edge and said trailing edge, and at least one spacer strip interconnecting said inner face of the first airfoil and said inner face of the second airfoil, said at least one strip extending to said trailing edge, the distance between the inner face of the first airfoil and the inner face of the second airfoil being of the same order of magnitude as the maximum thickness of the first or the second airfoil.
1. A turbomachine blade possessing a leading edge and a trailing edge, wherein the blade comprises a first airfoil possessing an inner face and an outer face extending between said leading edge and said trailing edge, a second airfoil possessing an inner face and an outer face extending between said leading edge and said trailing edge, said first airfoil and said second airfoil being in side-by-side alignment such that, over substantially its entire area, said inner face of the first airfoil faces said inner face of the second airfoil, and at least one spacer strip interconnecting said inner face of the first airfoil and said inner face of the second airfoil, said at least one strip extending to said trailing edge.
2. A blade according to claim 1 , including at least three strips.
3. A blade according to claim 2 , including a first strip situated in the range 0% to 30% up the height of the blade, a last strip situated in the range 70% and 100% up the height of the blade, and a strip situated substantially halfway up the height of the blade, a height of 0% corresponding to the radially-inner end of the blade and a height of 100% corresponding to the radially-outer end of the blade.
4. A blade according to claim 1 , wherein the thickness of said at least one strip increases from its middle towards the leading edge of said at least one strip such that said leading edge forms a sharp edge.
5. A blade according to claim 1 , wherein the thickness of said at least one strip decreases from its middle towards the trailing edge of said at least one strip such that said trailing edge forms a sharp edge.
6. A blade according to claim 1 , wherein said outer face of the first airfoil, said inner face of the first airfoil, said inner face of the second airfoil, and said outer face of the second airfoil all have different profiles.
7. A blade according to claim 1 , wherein the distance between said inner face of the first airfoil and said inner face of the second airfoil is no greater than three times the maximum thickness of said first or second airfoil.
8. A blade according to claim 7 , wherein the distance is less than 15 mm.
9. A blade according to claim 1 , wherein at least one of said strips is rectilinear.
10. A blade according to claim 1 , wherein at least one of said strips possesses curvature in at least one plane extending in the height direction of said blade.
11. A blade according to claim 1 , further comprising a third airfoil situated between said first airfoil and said second airfoil, said third airfoil possessing a first face and a second face extending between said leading edge and said trailing edge of the blade, said first face being connected to said inner face of the first airfoil by said at least one strip, and said second face being connected to the inner face of the second airfoil by said at least one strip.
12. A bladed wheel including on its circumference a series of blades according to claim 1 .
13. A bladed wheel according to claim 12 , wherein said strips follow substantially the streamlines that would be followed by the flow of air in the space between the first airfoil and the second airfoil if said strips were not present, so as to minimize disturbance to said flow of air.
14. A turbomachine including at least one blade according to claim 1 .