CPC F01D 11/006 (2013.01) [F01D 9/041 (2013.01); F01D 9/042 (2013.01); F01D 11/005 (2013.01); F01D 25/246 (2013.01); F05D 2240/11 (2013.01); F05D 2240/80 (2013.01)] | 17 Claims |
1. A turbine vane platform sealing assembly configured for installation in a gas turbine, the turbine vane platform sealing assembly comprising:
a first sealing member inserted into a first groove formed in a turbine vane platform in a first direction, the first sealing member extending in the first direction;
a second sealing member inserted into a second groove formed in a second direction intersecting the first direction of the turbine vane platform such that an end thereof contacts an upper surface of the first sealing member; and
a third sealing member provided so as to partially extend in the first direction while being partially bent in the second direction at a point where the first and second sealing members are in contact;
wherein
the second sealing member comprises: a plate-shaped sealing body formed with a first thickness, and a sealing head formed with a second thickness greater than the first thickness and having an insertion groove formed in a portion connecting with the sealing body,
the third sealing member comprises: an extension part formed to extend in a first direction and disposed on an upper surface of the first sealing member, a bent part formed by bending in a second direction at a point where the first sealing member and the second sealing member contact, and a protruding tab formed to protrude from an upper surface of the bent part and formed in a shape corresponding to the insertion groove;
the protruding tab is inserted into the insertion groove to restrict the movement of the third sealing member in a third direction lateral to the first direction and the second direction; and
the bent part has a first width in the third direction, and the protruding tab has a second width in the third direction that is less than the first width.
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