Stator outer platform sealing and retainer
A system for retaining stators and reducing air leakage in a gas turbine engine having an axis includes a stator having an inner platform, an outer platform, a low pressure side, a high pressure side, and at least one foot, and designed to turn air. The system also includes a case positioned radially outward from the stator and having at least one recess designed to interface with the at least one foot to resist movement of the stator relative to the case. The system also includes a bladder positioned between the outer platform of the stator and the case and designed to receive pressurized fluid having a greater pressure than ambient pressures experienced at the low pressure side of the stator and to further resist movement of the stator relative to the case in response to receiving the pressurized fluid.
1. A system for reducing air leakage in a gas turbine engine having an axis, comprising:
a first plurality of stators and a second plurality of stators, each stator having an inner platform, an outer platform, a low pressure side, and a high pressure side, and configured to turn air;
a case having a first semi-annular portion positioned radially outward from the first plurality of stators and a second semi-annular portion positioned radially outward from the second plurality of stators, the first semi-annular portion being separate from the second semi-annular portion;
a first elastic strap configured to be coupled to the first plurality of stators, to extend across the outer platform of each stator of the first plurality of stators, and to be positioned radially between the first plurality of stators and the first semi-annular portion of the case, a first end of the first elastic strap connected to a first circumferential end of the first plurality of stators and a second end of the first elastic strap connected to a second circumferential end of the first plurality of stators; and
a second elastic strap configured to be coupled to the second plurality of stators, to extend across the outer platform of each stator of the second plurality of stators, and to be positioned radially between the second plurality of stators and the second semi-annular portion of the case.
2. The system of claim 1 , wherein the system is positioned in a compressor section or a turbine section of the gas turbine engine.
3. The system of claim 1 , wherein each of the first elastic strap and the second elastic strap includes an elastomeric material.
4. The system of claim 3 , wherein each of the first elastic strap and the second elastic strap further includes a plurality of fibers embedded in or on the elastomeric material.
5. The system of claim 1 , wherein the first elastic strap is stretched prior to being coupled to the first circumferential end and the second circumferential end such that tension in the first elastic strap resists relative movement of each stator of the first plurality of stators.