Rotary component of a rotary device for heat engines and a method of manufacturing the same

• US 4,692,099 A
• Filed: 06/17/1986
• Issued: 09/08/1987
• Est. Priority Date: 06/18/1985
• Status: Expired due to Fees

• Current Assignee: Kabushiki Kaisha Toyota Chuo Kenkyusho (Toyota Motor Corporation)
• Original Assignee: Kabushiki Kaisha Toyota Chuo Kenkyusho (Toyota Motor Corporation)
• Inventors: Homma, Takahiko, Wada, Shigetaka
• Primary Examiner(s): Garrett, Robert E.
• Assistant Examiner(s): Pitko, Joseph M.
• Application Number:
  US06/875,195
• Time in Patent Office: 448 Days
• Field of Search: 416/229 R, 416/229 A, 416/230, 416/241 B, 264/63, 264/67, 29/156.4 R
• US Class Current: 416/229.00A
• CPC Class Codes: B29D 99/0025 Producing blades or the like, e.g. blades for turbines, propellers, or wings
• CPC Class Codes: C04B 2235/5224 Alumina or aluminates
• CPC Class Codes: C04B 2235/524 Non-oxidic, e.g. borides, carbides, silicides or nitrides
• CPC Class Codes: C04B 2235/5244 Silicon carbide
• CPC Class Codes: C04B 2235/5248 Carbon, e.g. graphite
• CPC Class Codes: C04B 2235/526 characterised by the length of the fibers
• CPC Class Codes: C04B 2235/5264 characterised by the diameter of the fibers
• CPC Class Codes: C04B 2235/5268 Orientation of the fibers
• CPC Class Codes: C04B 2235/6022 Injection moulding
• CPC Class Codes: C04B 2235/95 Products characterised by their size, e.g. microceramics
• CPC Class Codes: C04B 35/117 Composites
• CPC Class Codes: C04B 35/488 Composites
• CPC Class Codes: C04B 35/565 based on silicon carbide
• CPC Class Codes: C04B 35/584 based on silicon nitride
• CPC Class Codes: C04B 35/597 based on silicon oxynitride, e.g. SIALONS
• CPC Class Codes: C04B 35/80 Fibres, filaments, whiskers, platelets, or the like
• CPC Class Codes: F01D 5/284 Selection of ceramic materials
• CPC Class Codes: F01D 5/34 Rotor-blade aggregates of unitary construction , e.g. formed of sheet laminae; discs formed of sheet laminae F01D5/028; ceramic materials F01D5/284, composite materials F01D5/282
• CPC Class Codes: F05D 2200/261 Sine
• CPC Class Codes: Y10T 29/49321 Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member

Abstract

A rotary component of a rotary device for heat engines, such as a turbine wheel of a gas turbine or a turbocharger, formed in an integral ceramic-fiber-reinforced sintered ceramic structure. The reinforcing ceramic fibers in the edges of the vanes of the rotary component are oriented radially to prevent the chipping of the edges of the vanes liable to occur in a direction perpendicular to the direction of thickness of the vanes. The rotary component is formed by molding a mixture of a ceramic powder, ceramic fibers and organic additive or additives in a mold having a cavity having the same shape as that of the rotary component except that the depth of sections of the cavity corresponding to the vanes is greater than the height of the vanes to be formed, sintering the molding, and cutting the vanes of the molding in a predetermined height.

Claims

1. In a rotary component of a rotary device for heat engines, formed in an integral ceramic-fiber-reinforced sintered ceramic structure comprising:

a shaft;

a hub; and

vanes radially extending from the circumference of the hub, the improvement wherein;

reinforcing ceramic fibers are distributed in an edge portion of each of the vanes, including side surfaces of each of the vanes, and are oriented substantially parallel to the side surfaces of each of the vanes and radially outward of each of the vanes.

2. A rotary component according to claim 1, wherein ceramic mateial forming the matrix of said rotary component is silicon nitride, silicon carbide, alumina, zirconia or sialon, and the ceramic fibers reinforcing said rotary component are those of silicon nitride, silicon carbide, alumina, graphite or boron nitride.

3. A rotary component according to claim 1, wherein said reinforcing ceramic fibers have a diameter in the range of 0.3 to 50 μ

m and a length in the range of 5 to 1000 μ

m.

4. A rotary component according to claim 1, wherein the rotary component is designed for use as a turbine wheel of a gas turbine.

5. A rotary component according to claim 1, wherein the rotary component is designed for use as a turbine wheel of a turbocharger.

6. A rotary component according to claim 1, wherein the ceramic fiber content is of the order of 5 to 70% by weight.

7. A method of manufacturing a rotary component of a rotary device for heat engines, formed in an integral ceramic-fiber-reinforced sintered ceramic structure comprising a shaft, a hub, and vanes radially extending from the circumference of the hub, reinforcing ceramic fibers in the edges of the vanes being oriented substantially in parallel to the side surfaces of the vanes and radially outward of the vanes, which comprises the steps of:

preparing a mold having a cavity of a shape corresponding to that of the rotary component to be formed except that the depth of sections of the cavity corresponding to the vanes is greater than the height of the vanes to be formed;

injecting a fluidized mixture of a ceramic powder, ceramic fibers and an organic additive or additives into the cavity of the mold;

heating a molding thus molded to remove the organic additive or additives;

sintering the molding after the removal of the organic additive or additives to produce a sintered molding; and

cutting the outer extremities of the vanes to form the vanes in a predetermined height after said molding or said sintering.

8. A method according to claim 7, wherein said ceramic powder is that of silicon carbide, silicon nitride, alumina, zirconia or sialon, and said ceramic fibers are those of silicon carbide, silicon nitride, alumina, graphite or boron nitride.