Altering structural response of two-piece hollow-vane assembly
A hollow vane assembly including an open body including an interior; a cover brazed to the open body to form at least one flow passage; and at least one surface feature on an interior surface of the cover.
1 . A process of tailoring vibratory characteristics of a cover for an open body hollow vane assembly comprising:
forming the open body, the open body including an interior;
forming a cover, the cover being configured to attach to the open body to form at least one flow passage;
forming at least one surface feature on an interior surface of the cover prior to brazing the cover to the open body, the surface feature configured to be proximate the interior; and
brazing the cover to the open body.
2 . The process according to claim 1 , further comprising:
forming the at least one surface feature integral with the interior surface of the cover independently of the open body.
3 . The process according to claim 2 , wherein the at least one surface feature is selected from the group consisting of a groove, a rib, a channel, a trench, a furrow, a dimple, a nub, a post, and an iso-grid.
4 . The process according to claim 1 , further comprising:
forming an airfoil from the combination of the open body brazed together with the cover.
5 . The process according to claim 1 , further comprising:
forming a single walled structure having contoured surfaces including the at least one surface feature formed by additive and/or subtractive processes.
6 . The process according to claim 1 , further comprising:
modifying a vibratory characteristic of the cover with the at least one surface feature.
7 . The process according to claim 1 , further comprising:
changing a modal shape of the cover with the surface feature to enhance the stiffness of the cover locally responsive to aerodynamic forces created by a working fluid flowing over the hollow vane assembly.
8 . A process for modifying a vibratory characteristic of a cover to an open body comprising:
forming an open body, the open body includes a leading edge opposite a trailing edge, the open body includes a pressure side and suction side opposite the pressure side, the open body including an interior;
forming a cover, the cover being configured to couple with the open body proximate the pressure side to form at least one flow passage;
forming at least one surface feature on an interior surface of the cover prior to attaching the cover to the open body; and
brazing the cover to the open body.
9 . The process of claim 8 , further comprising:
modifying a vibratory characteristic of the cover with the at least one surface feature.
10 . The process of claim 8 , further comprising:
changing a modal shape of the cover to enhance the stiffness of the cover locally responsive to aerodynamic forces created by a working fluid flowing over the hollow vane assembly.
11 . The process of claim 8 , further comprising:
forming a single walled structure having contoured surfaces including the at least one surface feature formed by additive and/or subtractive processes.
12 . The process of claim 8 , further comprising:
forming an airfoil from the combination of the open body brazed together with the cover having the at least one surface feature, the airfoil being responsive to the at least one surface feature.
13 . The process of claim 8 , further comprising:
forming the surface feature by removing material from the interior surface of the cover.