Stator anti-rotation device
A stator vane assembly for a gas turbine engine is disclosed and includes a plurality of vanes received within channels defined within a case. An anti-rotation plate extends from a flange of the case between adjacent ones of the plurality of vanes for preventing rotation of the plurality of vanes relative to the case.
1. A compressor section of a gas turbine engine comprising:
a case including a first flange attached to a second flange parallel to an engine axis;
a stator vane assembly including a plurality of vanes received within channels defined within the case, wherein each of the plurality of vanes includes a platform section including a side parallel with the engine axis and hooks mounted within the channels; and
an anti-rotation plate extending from one of the first flange and the second flange between adjacent ones of the plurality of vanes and abutting the side parallel with the engine axis for preventing rotation of the stator vane assembly, the anti-rotation plate including a mount portion disposed within a recess within one of the first flange and the second flange and a key portion extending radially inward between adjacent ones of the plurality of vanes, wherein the mount portion includes a width greater than the key portion with the anti-rotation plate abutting a side of the hooks within the channels.
2. The compressor section as recited in claim 1 , wherein the anti-rotation plate disposed within the recess even with or below a face of the flange.
3. The compressor section as recited in claim 1 , wherein the case includes two flange interfaces each including the first flange on a first case half and the second flange on a second case half and an anti-rotation plate.
4. The compressor section as recited in claim 3 , wherein one of the anti-rotation plates is disposed within a first flange at a first one of the two flange interfaces and another of the anti-rotation plates is disposed in a second flange of the other of the two flange interfaces.
5. The compressor section as recited in claim 1 , wherein the recess comprises a slot opening to an inner chamber within the case and a mount section radially outward of the slot with the key portion of the anti-rotation plate extending through the slot into the inner chamber.
6. A stator vane assembly for a gas turbine engine comprising:
a plurality of vanes received within channels defined within a case, wherein each of the plurality of vanes includes a platform section including a side parallel with an engine axis and hooks mounted within the channels; and
an anti-rotation plate extending from a flange of the case between adjacent ones of the plurality of vanes and abutting the side parallel with the engine axis for preventing rotation of the plurality of vanes relative to the case, the anti-rotation plate includes a mount portion disposed within the flange and a key portion extending radially inward the adjacent ones of the plurality of vanes with the anti-rotation plate abutting a side of the hooks within the channels, wherein the mount portion includes an axial length greater than an axial length of the key portion.
7. A method of assembling a stator vane assembly for a gas turbine engine comprising:
assembling a plurality of stator vanes into channels defined within a case;
placing an anti-rotation plate into a recess defined within an axially extending flange of the case such that a key portion of the anti-rotation plate extends radially inward between adjacent ones of the plurality of stator vane assemblies;
securing a mount portion of the anti-rotation plate within the recess with a threaded fastener, wherein the mount portion includes an axial length greater than an axial length of the key portion and securing the mount portion includes securing the mount portion within a mount section of the recess that is axially longer than a slot portion through which the key portion extends for controlling radial movement of the plurality of stator vanes; and
abutting one first side of the anti-rotation plate with a side of one of the plurality of stator vanes and abutting a second side of the anti-rotation plate with a side of another of plurality of stator vanes.
8. The compressor section as recited in claim 5 , wherein the mount section includes an axial length greater than an axial length of the slot.
9. The compressor section as recited in claim 8 , wherein the mount portion includes axial ends that extend outward axially from both ends beyond the axial length of the key and fasteners securing the anti-rotation plate within the mount section are disposed within the axial ends.
10. The stator vane assembly as recited in claim 6 , wherein the wherein the mount portion includes axial ends that extend outward axially from both ends beyond the axial length of the key and fasteners securing the anti-rotation plate within the mount section are disposed within the axial ends.