Turbofan engine including integrated pylon and fan outlet guide vane with noise reduction features
A turbofan engine and an outlet guide vane structure for the turbofan engine is provided. The outlet guide vane structure includes a non-uniform plurality of outlet guide vanes utilized in a bypass duct and between a radially inward wall and a radially outward wall. The non-uniform plurality of outlet guide vanes have varying chord lengths at the base of the outlet guide vanes along the radially inward wall. The non-uniform plurality of outlet guide vanes may include structural outlet guide vanes, non-structural outlet guide vanes, and cut-out outlet guide vanes. The non-uniform plurality of outlet guide vanes include at least one outlet guide vane integrated with a pylon and/or a bifurcation of the turbofan engine. The cut-out outlet guide vane may be integrated with the pylon and/or bifurcation. The cut-out may include a leading edge and a trailing edge disposed in front of a leading edge of the pylon.
1. A turbofan engine including outlet guide vanes comprising: a bypass duct having a radially inward wall and a radially outward wall; and a plurality of non-uniform outlet guide vanes disposed between the radially inward wall and the radially outward wall of the bypass duct, wherein the plurality of non-uniform outlet guide vanes includes at least one first integral outlet guide vane coupled to a pylon of the turbofan engine, wherein chord lengths of two or more of the plurality of non-uniform outlet guide vanes at a base adjacent the radially inward wall are different, wherein the plurality of non-uniform outlet guide vanes includes the at least one first integral outlet guide vane, at least one structural outlet guide vane, at least one cut-out outlet guide vane, and at least one non-structural outlet guide vane.
2. The turbofan engine of claim 1 , further comprising at least one bifurcation, wherein the plurality of non-uniform outlet guide vanes further includes at least one second integral outlet guide vane coupled to the at least one bifurcation.
3. The turbofan engine of claim 1 , wherein the at least one first integral outlet guide vane further comprises a cut-out at a base of the at least one first integral outlet guide vane adjacent the radially inward wall of the bypass duct.
4. The turbofan engine of claim 3 , wherein the cut-out extends about 10% to 90% of a radial length of the at least one first integral outlet guide vane measured from the base of the at least one first integral outlet guide vane toward the radially outward wall, wherein the radial length extends from the radially inward wall toward the radially outward wall.
5. The turbofan engine of claim 3 , wherein the at least one first integral outlet guide vane integrated with the pylon further comprises a leaned stacking at the base of the at least one first integral outlet guide vane.
6. The turbofan engine of claim 1 , wherein each of the plurality of non-uniform outlet guide vanes further comprises a lean at a leading edge, wherein the lean is uniform for each of the plurality of non-uniform outlet guide vanes.
7. The turbofan engine of claim 1 , further comprising an acoustic liner disposed on, coupled to, inside of, or within one or more of the plurality of non-uniform outlet guide vanes or the pylon.
8. The turbofan engine of claim 1 , wherein at least one cut-out outlet guide vane is integrally coupled with the pylon and the at least one structural outlet guide vane is disposed adjacent to the at least one cut-out outlet guide vane.
9. The turbofan engine of claim 8 , wherein a cut-out of the at least one cut-out outlet guide vane is disposed at a base of the at least one cut-out outlet guide vane adjacent the radially inward wall.
10. The turbofan engine of claim 9 , wherein the cut-out extends about 10% to 90% of a radial length of the at least one cut-out outlet guide vane measured from the base of the at least one cut-out outlet guide vane toward the radially outward wall, wherein the radial length extends from the radially inward wall toward the radially outward wall.
11. The turbofan engine of claim 9 , wherein the cut-out extends between about 1% to 99% from the radially inward wall toward the radially outward wall.
12. The turbofan engine of claim 9 , wherein the cut-out of the at least one cut-out outlet guide vane further comprises a circumferential lean at the base of the at least one cut-out outlet guide vane.
13. The turbofan engine of claim 1 , wherein the plurality of non-uniform outlet guide vanes includes a leading edge that extends to a splitter of the radially inward wall.
14. The turbofan engine of claim 1 , wherein the plurality of non-uniform outlet guide vanes includes a leading edge that extends between 1% to 100% from a leading edge of the pylon towards a splitter of the radially inward wall.
15. The turbofan engine of claim 1 , wherein the at least one structural outlet guide vane is the at least one first integral outlet guide vane.
16. The turbofan engine of claim 15 , wherein the at least one cut-out outlet guide vane is adjacent to the at least one structural outlet guide vane.
17. The turbofan engine of claim 15 , wherein two cut-out outlet guide vanes are on each side of the at least one structural outlet guide vane.
18. The turbofan engine of claim 15 , wherein two structural outlet guide vanes are on each side of the at least one cut-out outlet guide vane.
19. The turbofan engine of claim 1 , wherein the at least one cut-out outlet guide vane is the at least one first integral outlet guide vane.
20. The turbofan engine of claim 19 , wherein the at least one structural outlet guide vane is adjacent to the at least one cut-out outlet guide vane.