Vertically oriented seal system for gas turbine vanes
A seal system for a gas turbine vane includes a first seal layer and an optional second seal layer. Each first seal layer includes multiple seal segments, each of which includes a first leg, a second leg, and an intermediate portion between the first leg and the second leg. Each adjacent pair of seal segments of the first seal is separated by a gap. The seal segments define a substantially complete perimeter of a seal slot in which the first seal is installed. The second seal, which is also segmented, may or may not define the substantially complete perimeter of the seal slot. If present, the second seal segments are circumferentially offset from the first seal segments to block the gaps between the first seal segments. A turbine vane including the present seal system is also disclosed.
1. A seal system comprising:
a first seal layer comprising a plurality of first seal segments, wherein respective first gaps are defined between each respective pair of first seal segments, each first seal segment of the plurality of first seal segments comprising a first leg, a second leg, and an intermediate portion connecting the first leg to the second leg; and
a second seal layer comprising a plurality of second seal segments equal in number to the plurality of first seal segments, the plurality of second seal segments being positioned adjacent the first seal layer to block the first gaps;
wherein each first seal segment is coupled to a single radially adjacent second seal segment by a spot weld, a rosette weld, a braze joint, or a flat-headed rivet and is coupled to a different second seal segment by a non-durable adhesive or a removable fastener, the different second seal segment and the single radially adjacent second seal segment being circumferentially adjacent; and
wherein the first seal layer and the second seal layer define a substantially complete perimeter of a seal slot in which the first seal layer and the second seal layer are vertically installed.
2. The seal system of claim 1 , wherein the intermediate portion defines a curved surface.
3. The seal system of claim 1 , wherein the intermediate portion defines an angular corner.
4. The seal system of claim 1 , wherein the plurality of first seal segments are disposed radially outward of the plurality of second seal segments.
5. The seal system of claim 4 , wherein each second seal segment of the plurality of second seal segments has a straight profile.
6. The seal system of claim 4 , wherein each first seal segment of the plurality of first seal segments has a straight profile.
7. The seal system of claim 1 , wherein the second seal segments of the plurality of second seal segments have a uniform second height.
8. The seal system of claim 1 , wherein each seal segment of the plurality of second seal segments is a straight seal segment; and wherein each straight seal segment is positioned radially inward of a respective one of the first gaps between adjacent pairs of the plurality of first seal segments.
9. The seal system of claim 1 , wherein each seal segment of the plurality of second seal segments comprises a third leg, a fourth leg, and an intermediate portion between the third leg and the fourth leg; wherein each adjacent pair of seal segments of the plurality of second seal segments is separated by a second gap; and wherein the plurality of second seal segments also defines the substantially complete perimeter of the seal slot in which the first seal and the second seal are vertically installed.
10. The seal system of claim 9 , wherein the first gaps between respective adjacent pairs of the plurality of first seal segments are circumferentially offset from the second gaps between respective adjacent pairs of the plurality of second seal segments.
11. A turbine vane comprising:
a metal spar comprising an airfoil-shaped body;
an outer side wall defining an opening through which the metal spar is installed;
a ceramic matrix composite (CMC) vane shell disposed over the airfoil-shaped body of the metal spar, the CMC vane shell having a radially outer vane platform and a radially inner vane platform; and
an inner side wall joined to the ceramic matrix composite vane shell;
wherein a first seal system of claim 1 is disposed between the outer side wall and the radially outer vane platform, and a second seal system of claim 1 is disposed between the inner side wall and the radially inner vane platform;
and wherein each of the first seal system and the second seal system is vertically oriented within a respective platform seal slot and a respective side wall seal slot.