FIELD: manufacturing technology.
SUBSTANCE: stator blade comprises a feather, an outer and an inner rim sections, a first and a second hook sections, a flange section and a reinforcing fabric and a cutout. Outer and inner rim sections are curved in the peripheral direction and extend the outer and inner ends of the stylus, respectively. First and second hook sections are curved outwardly in the radial direction and continue the front and rear end of the outer rim section, respectively. Flange section continues the end in the axial direction of the inner rim section and is bent inward in a radial direction. Reinforcing fiber tissue passes through the stylus, the outer rim section, the first and second hook sections, the inner rim section, and the flange section and is integrally formed with the ceramic. Cutout extends from the leading edge in the axial direction of the feather to the front end of the outer rim. In the manufacture of said stator vane, the fiber reinforcing fiber is elongated in a radial direction to form a feather and the outer end of the feather is bent in a circumferential direction with respect to the axis to form an outer rim section. Front end is bent in the axial direction of the outer rim section outward in the radial direction to form the first hook section. Rear end is bent in the axial direction of the outer rim section outward in a radial direction to form a second hook section. Reinforcing fiber cloth is bent at the inner end of the pen in the peripheral direction to form an inner rim section. End in the axial direction of the inner rim section is bent inward in a radial direction to form a flange section. Fiber reinforced fabric with a ceramic is used as a whole. Machining of the ceramic, made in one piece with the reinforcing fiber cloth, is performed to form a cutout.
EFFECT: group of inventions makes it possible to increase the strength of the stator blade and reduce its weight.
6 cl, 8 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBINE | 2015 |
|
RU2677021C1 |
TURBINE BLADE | 1993 |
|
RU2088764C1 |
TURBINE NOZZLE ASSEMBLY | 2016 |
|
RU2708931C1 |
FIBER PREFORM FOR A HOLLOW TURBINE ENGINE VANE | 2014 |
|
RU2661582C2 |
TURBINE MACHINE BLADE WITH EVEN OR UNEVEN ADDITIONAL GEOMETRY AND METHOD OF ITS MANUFACTURING | 2011 |
|
RU2562983C2 |
TURBINE BLADE AND PROCEDURE FOR ITS MANUFACTURE | 2011 |
|
RU2541078C2 |
GAS TURBINE COMPONENT | 2014 |
|
RU2568763C2 |
CASTING MOULD FOR PRODUCTION OF MONOCRYSTALLINE VANE BY CASTING, INSTALLATION AND METHOD OF MANUFACTURING, USING CASTING MOULD | 2017 |
|
RU2730827C2 |
METHOD FOR MANUFACTURING A TURBINE ENGINE VANE MADE OF A COMPOSITE MATERIAL, RESULTING VANE AND TURBINE ENGINE INCLUDING SAME | 2015 |
|
RU2678479C2 |
SHIELDING ELEMENT AND JET ENGINE, IN WHICH SUCH ELEMENT IS USED | 2015 |
|
RU2673963C1 |
Authors
Dates
2018-09-06—Published
2015-06-29—Filed