摘要:
A high-temperature-steam-oxidation-resistive coated reinforcement fiber applicable to a fiber reinforced composite, is provided with: a reinforcement fiber; a coating layer covering the reinforcement fiber and including a rare-earth silicate; an exfoliative layer intervening in an interface between the coating layer and the reinforcement fiber; and a supplemental coating layer covering the reinforcement fiber, the exfoliative layer and the coating layer.
摘要:
A coating used in a vapor-oxidative atmosphere has a first layer including SIALON and a second layer covering the first layer and being exposed to the atmosphere, the second layer including mullite, wherein the first layer and the second layer get in contact with each other.
摘要:
A turbine component includes an airfoil section elongated in a longitudinal direction; a dovetail section continuous with an end of the airfoil section and bulging in a width direction across the longitudinal direction; a plurality of first reinforcement fibers running continuously from the airfoil section to the dovetail section; a plurality of second reinforcement fibers running at least partly in the width direction in the airfoil section; and a matrix joining an entirety of the first reinforcement fibers and the second reinforcement fibers. In the airfoil section, the second reinforcement fibers are woven into the first reinforcement fibers to form a three-dimensional fabric. In the dovetail section, the first reinforcement fibers are not gathered in the width direction by other fibers but deploy in the width direction.
摘要:
A ceramic matrix composite component (10) coated with environmental barrier coatings includes a substrate (12) formed of a silicide-containing ceramic matrix composite, a silicon carbide layer (14) deposited on a surface of the substrate (12), a silicon layer (16) deposited on a surface of the silicon carbide layer (14), a mixed layer (18) made of a mixture of mullite and ytterbium silicate and deposited on a surface of the silicon layer (16), and an oxide layer (20) deposited on a surface of the mixed layer (18).
摘要:
A ceramic matrix composite (10) includes a substrate (14) which contains a fibrous body (12) formed from a silicon carbide fiber, and a matrix (16) which is formed in the substrate (14), and which contains RE 3 Al 5 O 12 , RE 2 Si 2 O 7 , and the balance being an oxide of RE, Al, and Si, or RE 2 SiO 5 , where the RE is Y or Yb.
摘要:
[Object] A design support apparatus, design support method, and program capable of predicting, with good accuracy, a material shape before deformation processing from a 3-dimensional shape model of a product which uses a fiber-reinforced composite material are proposed. [Solution] A design support apparatus for supporting designing of a product which uses a fiber material includes a processor that creates a predicted shape model by predicting a shape of the product before deformation processing, wherein the processor: creates a 3-dimensional shape model of the product; creates curved shape models by separating the 3-dimensional shape model into two or more fiber layers; sets a correspondence relationship between the curved shape models; creates an orientation vector field in the curved shape models; and predicts the shape of the product before the deformation processing by developing the curved shape models on a flat surface on the basis of the correspondence relationship between the curved shape models and the orientation vector field in the curved shape models, and creates the predicted shape model on the basis of the predicted shape.
摘要:
A mixed gas containing a precursor gas, an additive gas and a carrier gas is supplied to a preform (100) stored in an electric furnace (10), and silicon carbide is deposited by chemical vapor deposition or chemical vapor phase impregnation to form a film. The preform (100) includes multiple fiber bundles, and the fiber bundles include multiple fibers. This heat-resistant composite material includes a ceramic fiber preform impregnated with silicon carbide, and producing the composite material involves a step in which silicon carbide is deposited between the fibers to integrate the fibers which configure the fiber bundles, and a step in which silicon carbide is deposited between the fiber bundles to integrate the fiber bundles. Hereby, uniformity of embedding and growth rate of the silicon carbide film are both attained.
摘要:
Proposed are an image analyzing apparatus and program capable of extracting voids from a three-dimensional image of CMC in a short time and accurate manner. In an image analyzing apparatus for extracting voids from a three-dimensional image of a fiber-reinforced composite material, the image analyzing apparatus comprises a processor which executes image processing to the three-dimensional image, and the processor binarizes the three-dimensional image and creates a binary image, transforms the binary image into a distance and creates a distance image, executes closing processing to the binary image by using the distance image, extracts voids from differences between images before and after the closing processing, among the extracted voids, classifies voids that are adjacent to a background voxel as open voids, and classifies voids that are not adjacent to a background voxel as closed voids, and executes opening processing to the open voids in order to eliminate fake voids.
摘要:
In the manufacturing of a heat-resistant composite material composed of a ceramic fiber preform impregnated in silicon carbide, to support both high growth rate and good filling uniformity at film formation of silicon carbide. By using chemical vapor deposition or chemical vapor infiltration, silicon carbide is deposited on a preform 100 accommodated in a reaction furnace 11 for film formation, and the amount of additive gas added to raw material gas and carrier gas to be supplied to the reactive furnace 11 is used to control the growth rate and filling uniformity at film formation of silicon carbide. When the film formation of silicon carbide follows a first-order reaction, the amount of added additive gas is used to control the sticking probability of the film-forming species. When the film formation of silicon carbide follows a Langmuir-Hinshelwood rate formula, the amount of added additive gas is used to make a control so that a zero-order reaction region of the Langmuir-Hinshelwood rate formula is used.