Tuned airfoil assembly
An airfoil assembly may include a shroud and an airfoil. The shroud may include a first attachment arm, a second attachment arm, and a shroud rail extending from a first surface of the shroud. A first channel may be defined between the first attachment arm, the first surface, and the shroud rail and a second channel may be defined between the second attachment arm, the first surface, and the shroud rail. The airfoil may extend from a second surface of the shroud opposite the first surface. In various embodiments, a height of the shroud rail, as measured from the first surface of the shroud, is non-uniform.
1. An airfoil assembly comprising:
a shroud comprising a first attachment arm, a second attachment arm, and a shroud rail extending from a first surface of the shroud, wherein:
a first channel is defined between the first attachment arm, the first surface, and the shroud rail; and
a second channel is defined between the second attachment arm, the first surface, and the shroud rail; and
an airfoil extending from a second surface of the shroud opposite the first surface;
wherein a height of the shroud rail, as measured from the first surface of the shroud, tapers in a first direction across an entire width of the shroud rail in the first direction, wherein the first direction is from first attachment arm to the second attachment arm and is parallel to the first surface; and
wherein the shroud is a single, unitary body that is formed and shaped to have the first attachment arm, the second attachment arm, and the shroud rail.
2. The airfoil assembly of claim 1 , wherein the height of the shroud rail varies in a second direction normal to an axis extending between the first attachment arm and the second attachment arm, wherein the second direction is parallel to the first surface.
3. The airfoil assembly of claim 2 , wherein the height of shroud rail tapers in the second direction across an entire width of the shroud rail in the second direction.
4. The airfoil assembly of claim 1 , wherein
the height of the shroud varies in a second direction normal to the first direction and parallel to the first surface.
5. The airfoil assembly of claim 1 , wherein a distance between the first surface and the second surface is substantially uniform.
6. A manufacturing method comprising:
forming a shroud rail extending from a first surface of a shroud of an airfoil assembly, wherein the shroud rail is formed and shaped from a single material of the shroud such that the shroud rail is an integral extension of the shroud;
forming an airfoil extending from a second surface of the shroud opposite the first surface; and
determining both a desired aeromechanical response and a desired aerodynamic performance of the airfoil assembly;
shaping the shroud rail based on the desired aeromechanical response in order to impart a desired frequency mode to the airfoil assembly, wherein shaping the shroud rail comprises customizing a height of the shroud rail, as measured from the first surface, based on the desired aeromechanical response of the airfoil assembly; and
shaping the airfoil based on the desired aerodynamic performance in order to optimize aerodynamics of the airfoil assembly.
7. The method of claim 6 , further comprising coupling a sealing panel to the shroud rail of the airfoil assembly, wherein the sealing panel extends over and is coupled to respective shroud rails of one or more circumferentially adjacent singlet stator vanes.
8. An airfoil assembly comprising:
a shroud comprising a first attachment arm, a second attachment arm, and a shroud rail extending from a first surface of the shroud, wherein:
a first channel is defined between the first attachment arm, the first surface, and the shroud rail; and
a second channel is defined between the second attachment arm, the first surface, and the shroud rail; and
an airfoil extending from a second surface of the shroud opposite the first surface;
wherein a height of the shroud rail, as measured from the first surface of the shroud, tapers in a second direction across an entire width of the shroud rail in the second direction, wherein the second direction is normal to an axis extending between the first attachment arm and the second attachment arm and is parallel to the first surface; and
wherein the shroud is a single, unitary body that is formed and shaped to have the first attachment arm, the second attachment arm, and the shroud rail.
9. The airfoil assembly of claim 8 , wherein the height of the shroud rail varies in a first direction from the first attachment arm to the second attachment arm, wherein the first direction is parallel to the first surface.
10. The airfoil assembly of claim 9 , wherein the height of shroud rail tapers in the first direction across an entire width of the shroud rail in the first direction.
11. The airfoil assembly of claim 8 , wherein:
the height of the shroud rail varies in a first direction from the first attachment arm to the second attachment arm.
12. The airfoil assembly of claim 8 , wherein a distance between the first surface and the second surface is substantially uniform.