Device for forwarding a medium

• US 5,951,255 A
• Filed: 03/05/1998
• Issued: 09/14/1999
• Est. Priority Date: 03/05/1997
• Status: Expired due to Fees

• Current Assignee: Deutsches Zentrum Fã¼R Luft- Und Raumfahrt E.V.
• Original Assignee: Deutsches Zentrum Fã¼R Luft- Und Raumfahrt E.V.
• Inventors: Krenkel, Walter, Kochendoerfer, Richard
• Primary Examiner(s): RYZNIC, JOHN E
• Application Number:
  US09/035,389
• Time in Patent Office: 558 Days
• Field of Search: 416/230, 416/241 R, 416/241 A, 416/241 B, 416/186 R, 416/195, 416/213 R
• US Class Current: 416/230
• CPC Class Codes: C04B 2237/083 Carbide interlayers, e.g. silicon carbide interlayers
• CPC Class Codes: C04B 2237/365 Silicon carbide
• CPC Class Codes: C04B 2237/38 Fiber or whisker reinforced
• CPC Class Codes: C04B 2237/76 Forming laminates or joined articles comprising at least one member in the form other than a sheet or disc, e.g. two tubes or a tube and a sheet or disc
• CPC Class Codes: C04B 2237/80 Joining the largest surface of one substrate with a smaller surface of the other substrate, e.g. butt joining or forming a T-joint
• CPC Class Codes: C04B 37/005 consisting of glass or ceramic material
• CPC Class Codes: F04D 29/181 Axial flow rotors F04D29/185 take precedence
• CPC Class Codes: F04D 29/2227 for special materials
• CPC Class Codes: F05C 2203/0813 Carbides
• CPC Class Codes: F05C 2253/04 Composite, e.g. fibre-reinforced
• CPC Class Codes: F05D 2300/224 Carbon, e.g. graphite
• CPC Class Codes: F05D 2300/2261 of silicon
• CPC Class Codes: F05D 2300/2283 of silicon
• CPC Class Codes: F05D 2300/6033 Ceramic matrix composites [CMC]

Abstract

A device is disclosed for forwarding a medium in the form of a gas, liquid, or loose particles. The medium can contain additives and/or contaminants in an aggregate state other than that of the medium itself. The device'"'"'s major components are form-fit and force-fit together and comprise at least one supporting component along with blade-like components fastened to it. The supporting component is, or the supporting components are, made of a fiber-filled composite. The device is in particular an impeller for a pump, turbine, or similar mechanism. It is characterized in that the supporting component is, or the supporting components are, made of a lattice of essentially continuous fibers of carbon and/or ceramic and of a matrix that contains carbon and in that the fibers are sheathed with silicon carbide resulting from the infiltration of liquid silicon and from its reaction essentially with the carbon in the matrix.

Claims

1. In a device for forwarding a medium in the form of a gas, liquid, or loose particles, whereby the medium can contain additives and/or contaminants in an aggregate state other than that of the medium itself, the device'"'"'s major components are form-fit and force-fit together and comprise at least one supporting component along with blade-like components fastened to it, and at least one supporting component is made of a fiber-filled composite, the improvement wherein at least one supporting component is made of a lattice of essentially continuous fibers formed of at least one of carbon and a ceramic and of a matrix that contains carbon;

wherein the fibers are sheathed with silicon carbide resulting from the infiltration of liquid silicon and from its reaction essentially with the carbon in the matrix and wherein the fibers in areas of the surface of the components that come into contact with the medium being forwarded extend in a plane essentially parallel or tangential to the direction the medium flows in.

2. The device defined in claim 1, wherein the blade-like components are medium-forwarding or channeling blades or vanes uniformly distributed along the supporting component.

3. The device defined in claim 1, wherein, if the supporting component is in the form of a disk, the fibers in its lattice extend essentially along its plane in the form for example of layers of fabric and, if the supporting component is an annular supporting component, the fibers are oriented along its circumference.

4. The device defined in claim 1, wherein the blade-like components are made of a lattice of essentially continuous carbon fibers and/or ceramic and of a matrix that contains carbon and wherein the fibers are sheathed with silicon carbide resulting from the infiltration of liquid silicon and from its reaction essentially with the carbon in the matrix.

5. The device defined in claim 4, wherein the blade-like components are streamlined and have a core at the thicker, upstream end with several layers of fiber wrapped around it, tapering in toward and resting together at the downstream end.

6. The device defined in claim 1, wherein the fibers are woven and/or knit.

7. The device defined in claim 6, wherein, in order to increase strength and elasticity, the fibers are woven or knit bidirectionally, each more or less isotropic to the one below it.

8. The device defined in claim 1, wherein, in order to decrease fragility, the fibers are sheathed in carbon or boron nitride.

9. The device defined in claim 8, characterized in that the sheath is 50 to 500 nm thick.

10. The device defined in claim 1, wherein the lattice is between 30 and 70%, and preferably more than about 50%, carbon by volume of the composite.

11. The device defined in claim 1, wherein the lattice is between 50 and 100% carbon fibers.

12. The device defined in claim 1, wherein the blade-like components are monolithic ceramic.

13. The device as in claim 12, wherein the monolith is sintered, pressed, or reaction-bonded silicon carbide or silicon nitride.

14. The device defined in claim 1, wherein the blade-like components are carbon, especially graphite.

15. The device defined in claim 14, wherein the carbon is reinforced with carbon fibers.

16. The device defined in claim 1, wherein a supporting component contains less than 5% free silicon per total mass.

17. The device defined in claim 1, wherein the assembled components are coated to protect them from at least one of corrosion, abrasion, and oxidation.

18. The device defined in claim 17, wherein the protective coat is 20 to 200 μ

m thick.

19. The device defined in claim 17, wherein the protective coat is silicon carbide or mullite.

20. The device defined in claim 19, wherein the protective coat is chemical-vapor deposited silicon carbide.

21. The device defined in claim 1, wherein the silicon carbide is formed when liquid silicon infiltrates a prescribed system of pores in the fiber lattice and reacts with the carbon therein.

22. The device defined in claim 21, wherein the silicon infiltrates in a vacuum at temperatures above 1420°

C., preferably at temperatures ranging from 1450 to 1500°

C., and wherein the silicon carbide is formed by maintaining the temperature at approximately 1650°

C. for approximately two hours or by increasing the temperature to approximately 2000°

C. and maintaining it there for an accordingly abbreviated time of up to approximately one hour.

23. The device defined in claim 1, wherein the supporting component is composed of several laminated disks or rings two-dimensionally reinforced with fibers paralleling their major plane.

24. The device as in claim 1, wherein the supporting component and the blade-like components are permanently bonded together with a layer of essentially silicon carbide.

25. In a device for forwarding a medium in the form of a gas, liquid, or loose particles, whereby the medium can contain additives and/or contaminants in an aggregate state other than that of the medium itself, the device'"'"'s major components are form-fit and force-fit together and comprise at least one supporting component along with blade-like components fastened to it, and at least one supporting component is made of a fiber-filled composite, the improvement wherein at least one supporting component is made of a lattice of essentially continuous fibers formed of at lease one of carbon and a ceramic and of a matrix that contains carbon;

wherein the fibers are sheathed with silicon carbide resulting from the infiltration of liquid silicon and from its reaction essentially with the carbon in the matrix;

wherein the silicon carbide is formed when liquid silicon infiltrates a prescribed system of pores in the fiber lattice and reacts with the carbon therein; and

wherein the silicon infiltrates in a vacuum at temperatures above 1420°

C., preferably at temperatures ranging from 1450 to 1500°

C., and wherein the silicon carbide is formed by maintaining the temperature at approximately 1650°

C. for approximately two hours or by increasing the temperature to approximately 2000°

C. and maintaining it there for an accordingly abbreviated time of up to approximately one hour.