초록 ▼

A fiber reinforced composite article comprising a matrix and reinforcing fibers, and different operating temperature and stress combinations each across opposed surfaces and through the matrix, is made by first measuring each of the combinations. Then discrete regions, each extending completely thro

A fiber reinforced composite article comprising a matrix and reinforcing fibers, and different operating temperature and stress combinations each across opposed surfaces and through the matrix, is made by first measuring each of the combinations. Then discrete regions, each extending completely through the surfaces and the matrix, are selected for each combination. Reinforcing fibers with strength greater than the stress in a selected region are disposed in each selected region, the strengths being different between regions responsive to the different measured combinations.

대표청구항 ▼

1. In a method for making a fiber reinforced matrix composite article comprising a first surface, a second surface, and a matrix and reinforcing fibers therebetween,the article experiencing a plurality of different operating temperature and stress combinations across each of the first and second sur

1. In a method for making a fiber reinforced matrix composite article comprising a first surface, a second surface, and a matrix and reinforcing fibers therebetween,the article experiencing a plurality of different operating temperature and stress combinations across each of the first and second surfaces, each different combination extending completely through the matrix and the first and second surfaces, the steps of: calculating each of the different combinations; selecting for each different combination a discrete region each extending across each of the first and second surfaces and completely through the first and second surfaces and the matrix therebetween, a first region experiencing therethrough a first operating temperature that develops a first stress, a second region experiencing therethrough a second operating temperature, less than the first operating temperature, that develops a second stress greater than the first stress; selecting first fibers having a first coefficient of thermal expansion (CTE) at the first operating temperature to provide a first strength greater than the first stress; selecting second fibers having a second CTE greater than the first CTE at the second operating temperature to provide a second strength greater than the second stress; disposing the first fibers as reinforcing fibers in the matrix in the first region of the article; and, disposing the second fibers as reinforcing fibers in the matrix in the second region of the article. 2. The method of claim 1 in which a second strength of-the second region is greater than the difference between the first stress and the second stress and is determined by the relationship:A1E1α1T1?A2E2α2T2<S2, in which, respectively for the first region (1) and the second region (2): A is the area ratio of a region area to a total area of the regions, E is the elastic modulus of the fiber reinforced matrix, α is the CTE of the fiber reinforced matrix at the operating temperature in ° F., T is the operating temperature in ° F., and S is the strength of the second region. 3. The method of claim 1 in which the first and second fibers are provided in at least one form selected from the group consisting of fabric, weave, braid, and lay-up for disposing in the first and second regions.4. The method of claim 3 in which the first fibers and the second fibers are high temperature fibers are made from at least one material selected from the group consisting of alumina, silica, glass, graphite, carbon, carbides, tungsten boron and their mixtures.5. The method of claim 3 for making a turbine engine fiber reinforced composite article in which:the matrix of the composite article is based on alumina; and, the first fibers and the second fibers are disposed in the matrix in the range of about 20-70 volume %. 6. The method of claim 5 in which:the composite article is a gas turbine engine exhaust flap; the first operating temperature is in the range of about 1600-2000° F.; the second operating temperature is in the range of about 900-1300° F.; and, the first and second fibers are based on alumina. 7. The method of claim 2 in which:the composite article is a gas turbine engine blading component; and, the first fibers and the second fibers are disposed in the matrix in the range of about 20-70 volume %. 8. In a method for making a member for reinforcement of a fiber reinforced composite article, the member comprising a first surface, a second surface, and a matrix and reinforcing fibers therebetween,the member experiencing a plurality of different operating temperature and stress combinations across each of the first and second surfaces, each different combination extending completely through the matrix and the first and second surfaces, the steps of: calculating each of the different combinations; selecting for each different combination a discrete region each extending across each of the first and second surfaces and completely through the first and second surfaces and the matrix therebetween, a first region experiencing therethrough a first operating temperature that develops a first stress, a second region experiencing therethrough a second operating temperature, less than the first operating temperature, that develops a second stress greater than the first stress; selecting first fibers having a first CTE at the first operating temperature to provide a first strength greater than the first stress; selecting second fibers having a second CTE greater than the first CTE at the second operating temperature to provide a second strength greater than the second stress; disposing the first fibers as reinforcing fibers in the matrix in the first region of the member; and, disposing the second fibers as reinforcing fibers in the matrix in the second region of the member. 9. The method of claim 8 in which a second strength of the second region is greater than the difference between the first stress and the second stress and is determined by the relationship:A1E1α1T1?A2E2α2T2<S2, in which, respectively for the first region (1) and the second region (2): A is the area ratio of a region area to a total area of the regions, E is the elastic modulus of the fiber reinforced matrix, α is the CTE of the fiber reinforced matrix at the operating temperature in ° F., T is the operating temperature in ° F., and S is the strength of the second region. 10. The method of claim 8 in which the first and second fibers are provided in at least one form selected from the group consisting of fabric, weave, braid, and lay-up for disposing in the first and second regions.11. The method of claim 10 in which the first fibers and the second fibers are high temperature fibers are made from at least one material selected from the group consisting of alumina, silica, glass, graphite, carbon, carbides, tungsten boron and their mixtures.12. The method of claim 8 for making a member for use as fiber reinforcement in a turbine engine fiber reinforced alumina-based matrix composite article in which:the first temperature is in the range of about 1600-2000° F.; the second temperature is in the range of about 900-1300° F.; and, the first fibers and the second fibers are disposed in the matrix in the range of about 20-70 volume %. 13. The method of claim 12 in which:the composite article is a gas turbine engine exhaust flap; and, the first and second fibers are based on alumina. 14. The method of claim 8 for making a member for use as a fiber reinforcement in a fiber reinforced gas turbine engine blading component in which the first fibers and the second fibers are disposed in the matrix in the range of about 20-70 volume %.