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A jet vane for use in streams of hot gas, comprising a wing having a core area and a cover skin area surrounding the core area, is proposed. The cover skin area is made of a fiber-reinforced material, and the fibers in the cover skin area are oriented substantially parallel to the wing surface, and/

A jet vane for use in streams of hot gas, comprising a wing having a core area and a cover skin area surrounding the core area, is proposed. The cover skin area is made of a fiber-reinforced material, and the fibers in the cover skin area are oriented substantially parallel to the wing surface, and/or the cover skin area is made of a fiber-reinforced material that is reinforced with short fibers.

대표청구항 ▼

1. Jet vane for use in streams of hot gas, comprising: a wing having a core area and a cover skin area completely surrounding said core area;wherein: said cover skin area is made of a fiber-reinforced ceramic material;at least one of: (a) fibers in said cover skin area are oriented substantially par

1. Jet vane for use in streams of hot gas, comprising: a wing having a core area and a cover skin area completely surrounding said core area;wherein: said cover skin area is made of a fiber-reinforced ceramic material;at least one of: (a) fibers in said cover skin area are oriented substantially parallel to a wing surface; and (b) said cover skin area is made of a fiber-reinforced material that is reinforced with short fibers;different areas of the wing that are exposed to different strains are made from different materials that are adapted to the strains; andsaid cover skin area, which is at least one of corrosively and abrasively strained to a greater extent by a stream of hot gas, is made of a material with a higher ceramic content in comparison to a material of the core area which is exposed to higher mechanical strains. 2. Jet vane in accordance with claim 1, wherein said cover skin area is made of a material with a weaker fiber-matrix bond in a carbon fiber-reinforced plastic state in comparison with the core area. 3. Jet vane in accordance with claim 1, wherein a shaft is connected to the wing. 4. Jet vane in accordance with claim 3, wherein a shaft continuation area is located in the core area of the wing. 5. Jet vane in accordance with claim 4, wherein the shaft continuation area is formed substantially symmetrically in relation to a wing axis. 6. Jet vane in accordance with claim 3, wherein the shaft is made of a fiber-reinforced material. 7. Jet vane in accordance with claim 6, wherein fibers of the fiber-reinforced material of the shaft are oriented substantially parallel to a longitudinal axis of the shaft. 8. Jet vane in accordance with claim 6, wherein a shaft continuation area is made of a fiber-reinforced material. 9. Jet vane in accordance with claim 8, wherein fibers in the shaft continuation area are oriented substantially parallel to a wing axis. 10. Jet vane in accordance with claim 1, wherein the fibers in the cover skin area are C fibers or SiC fibers. 11. Jet vane in accordance with claim 1, wherein the cover skin area is made of C/C—SiC or SiC/SiC. 12. Jet vane in accordance with claim 3, wherein at least one of the shaft and a shaft continuation area is made of a material comprising C fibers or SiC fibers. 13. Jet vane in accordance with claim 3, wherein at least one of the shaft and a shaft continuation area is made of a fiber-reinforced ceramic material. 14. Jet vane in accordance with claim 3, wherein at least one of the shaft and a shaft continuation area is made of C/C—SiC or SiC/SiC. 15. Jet vane in accordance with claim 1, wherein at least one of the wing and a shaft is provided with a coating of hard material. 16. Jet vane in accordance with claim 1, wherein the core area comprises a shaft continuation area and an intermediate area. 17. Jet vane in accordance with claim 16, wherein the intermediate area comprises a material reinforced with short fibers. 18. Jet vane in accordance with claim 16, wherein the intermediate area is made of a monolithic ceramic material. 19. Jet vane in accordance with claim 1, wherein the cover skin area is produced using fabric layers. 20. Jet vane in accordance with claim 19, wherein the fabric layers surround the core area. 21. Jet vane in accordance with claim 1, wherein the cover skin area is produced by short fibers. 22. Jet vane in accordance with claim 21, wherein the short fibers are aligned. 23. Jet vane in accordance with claim 21, wherein the short fibers are aligned substantially parallel to the wing surface. 24. Method for manufacturing a jet vane made of a material that is fiber-reinforced in at least partial areas thereof, comprising: producing a jet vane preform with a near net shape by pressing;said jet vane comprising: a wing having a core area and a cover skin area completely surrounding said core area, wherein:said cover skin area is made of a fiber-reinforced ceramic material;at least one of: (a) fibers in said cover skin area are oriented substantially parallel to a wing surface; and (b) said cover skin area is made of a fiber-reinforced material that is reinforced with short fibers;different areas of the wing that are exposed to different strains are made from different materials that are adapted to the strains; andsaid cover skin area, which is at least one of corrosively and abrasively strained to a greater extent by a stream of hot gas, is made of a material with a higher ceramic content in comparison to a material of the core area which is exposed to higher mechanical strains. 25. Method in accordance with claim 24, wherein the thus produced jet vane preform is pyrolyzed. 26. Method in accordance with claim 24, wherein the thus produced jet vane preform is ceramized. 27. Method in accordance with claim 26, wherein the ceramized jet vane preform is at least partially coated with a layer of hard material. 28. Method in accordance with claim 24, wherein the pressing is carried out by means of a stamp entering a hollow mold. 29. Method in accordance with claim 28, wherein at least one of the hollow mold and the stamp is configured to correspond to a final shape of the jet vane to be produced. 30. Method in accordance with claim 24, wherein the pressing is carried out while heat is supplied. 31. Method in accordance with claim 30, wherein a stamp is heated. 32. Method in accordance with claim 30, wherein a hollow mold is heated. 33. Method in accordance with claim 24, wherein a heating operation is carried out on a workpiece after the pressing. 34. Method in accordance with claim 24, wherein the cover skin area and the core area are pressed together during the pressing. 35. Method in accordance with claim 24, wherein the cover skin area is produced using fabric layers. 36. Method in accordance with claim 24, wherein a shaft is made of unidirectional fibers or fabric layers. 37. Method in accordance with claim 36, wherein a shaft continuation area is produced in the core area. 38. Method in accordance with claim 37, wherein the shaft continuation area is made of unidirectional fibers or fabric layers. 39. Method in accordance with claim 36, wherein fibers in at least one of the shaft and a shaft continuation area are aligned substantially parallel to a longitudinal axis of the shaft. 40. Method in accordance with claim 34, wherein an intermediate area is produced in the core area. 41. Method in accordance with claim 40, wherein the intermediate area is made of a fiber-reinforced material that is reinforced with short fibers. 42. Method in accordance with claim 40, wherein the intermediate area is made of a monolithic ceramic material. 43. Method in accordance with claim 24, wherein different functional areas of the jet vane are produced with a material that is adapted to requirements of the respective functional area. 44. Method in accordance with claim 43, wherein at least one of fiber orientation and ceramic content of the corresponding material is set in accordance with the requirements for the respective functional area. 45. Jet vane for use in streams of hot gas, comprising: a wing made of a fiber-reinforced ceramic material;wherein: said fiber-reinforced ceramic material is produced by continuous fabric layers;the material for a core area of the wing has a higher ceramic content than a cover area on either side of said core area; andthe core area extends as far as into wing edges. 46. Jet vane for use in streams of hot gas, comprising: a wing made of a fiber-reinforced ceramic material;wherein: said fiber-reinforced ceramic material is produced by continuous fabric layers;the material for a core area of the wing has a higher ceramic content than a cover area on either side of said core area; andone or more wing edges are formed on the core area. 47. Jet vane in accordance with claim 46, wherein wing edges located opposite each other are formed on the core area. 48. Jet vane in accordance with claim 45, wherein the fabric layers are aligned parallel to at least one area of the wing surface. 49. Jet vane in accordance with claim 48, wherein the fabric layers are aligned parallel to an area of the wing surface having a largest surface area. 50. Jet vane in accordance with claim 45, wherein an SiC content in the core area is higher than in the cover areas. 51. Jet vane for use in streams of hot gas, comprising: a wing made of a fiber-reinforced ceramic material;wherein: said fiber-reinforced ceramic material is produced by continuous fabric layers;the material for a core area of the wing has a higher ceramic content than a cover area on either side of said core area; andthe core area is made of a C/C—SiC-XD material. 52. Jet vane for use in streams of hot gas, comprising: a wing made of a fiber-reinforced ceramic material;wherein: said fiber-reinforced ceramic material is produced by continuous fabric layers;the material for a core area of the wing has a higher ceramic content than a cover area on either side of said core area; andthe cover areas are made of at least one of a C/C—SiC-XB material and a C/C—SiC-XT material.