Environmental barrier fiber coating

Abstract

A fiber having an environmental barrier coating is provided that includes, in one illustrative form, a Hi Nicalon preform assembled in a tooling for chemical vapor infiltration and cleaned to remove sizing char from fibers of the Hi Nicalon preform; a ytterbium doped silicon carbide coat located over the Hi Nicalon preform; a boron nitride interface coat applied over the ytterbium doped silicon carbide coat; and a silicon carbide coat applied over the boron nitride interface coat.

Claims

1. Fibers having an environmental barrier coating, comprising: a fiber preform; a ytterbium doped silicon carbide coat located directly on the fiber preform; a boron nitride interface coat applied over the ytterbium doped silicon carbide coat; and a silicon carbide coat applied over the boron nitride interface coat.

2. The fibers having the environmental barrier coating of claim 1, wherein the boron nitride interface coat has a thickness of about 0.5 m.

3. The fibers having the environmental barrier coating of claim 1, wherein the silicon carbide coat has a thickness of about 2 m.

4. The fibers having the environmental barrier coating of claim 1, wherein the fiber preform includes about 36% fiber volume.

5. The fibers having the environmental barrier coating of claim 1, wherein the preform is completed with slurry and melt infiltration.

6. The fibers having the environmental barrier coating of claim 1, wherein the ytterbium doped silicon carbide coat is applied by chemical vapor infiltration.

7. The fibers having the environmental barrier coating of claim 1, wherein the silicon carbide coat is applied by chemical vapor infiltration.

8. The fibers of claim 1, wherein the fiber preform comprises carbon fibers, silicon carbide fibers, alumina fibers, aluminosilicate fibers, SiNC fibers or glass fibers.

9. The fibers of claim 8, wherein the fiber preform comprises silicon carbide fibers.

10. The fibers of claim 9, wherein the silicon carbide fibers comprise Hi Nicalon fibers.

11. The fibers of claim 1, wherein the fiber preform does not include sizing char.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a flow diagram showing a process for applying an environmental barrier coating on a fiber or preform matrix;

(2) FIG. 2 is an end sectional view of an illustratively-shaped PRIOR ART composite;

(3) FIG. 3 is an end sectional view of one embodiment of an environmental barrier fiber coating; and

(4) FIG. 4 is an end sectional view of an environmental barrier multi-layer fiber coating.

DETAILED DESCRIPTION

(5) The present disclosure includes a fiber coating that incorporates at least one layer prior to the fiber interface coating to improve chemical compatibility of the fiber and interface coating. Illustratively, the first coating is bonded to the fiber and is followed by an interface coating and, optionally, additional coatings. The coating may be a slightly altered composition of the fiber or a totally different composition. The coating acts as a barrier to oxygen and steam when the composite is cracked or the fiber is exposed on the edges or the surface. The coating may inherently be resistant to high temperature oxygen, steam and other fiber damaging compounds or it may react with the environment to create a stable, protective compound.

(6) The coating may also heal surface flaws on the fiber and increase the effective fiber volume by increasing the diameter of the fiber. The coating may be uniform in composition and structure, graded intentionally to produce a better match between the fiber and the interface coating or consist of multiple thin layers prior to the interface coating. The coating may also be followed by other functional coatings prior to the interface coating to improve structural performance or improve compatibility with the interface coating, or interface coating deposition process.

(7) An oxidation resistant coating may range from about 0.01 m to about 2 m. The coating may be deposited by chemical vapor deposition, physical vapor deposition (including directed vapor deposition) or other suitable means. The fiber in the composite could be carbon, ceramic (silicon carbide, alumina, aluminosilicate, SiNC, etc.) or glass. The coating (or coating layers) may include elemental, binary or ternary compounds of the following elements: carbon, nitrogen, oxygen, silicon, germanium, boron, aluminum, titanium, zirconium, hafnium, vanadium, niobium, tantalum, chromium, molybdenum, nickel, scandium, yttrium, ytterbium and rhenium.

(8) Illustratively, it may be desirable to tailor the coating composition and/or structure to produce a slightly lower modulus than the fiber to reduce stress in the coating layer and delay surface cracking.

(9) Prior to the structural coating, the fiber may be cleaned to remove polymer fiber coatings (sizing). This may be done at any time prior to the coating using solvents, hot air, other hot gases or other means. The cleaning process may enhance the bonding between the fiber and oxidation barrier coating.

(10) A flow diagram depicting a process of applying the environmental barrier coating on fiber 2 is shown in FIG. 1. Process 2 includes first providing a fiber material, textile, or preform for processing at 4. The material may illustratively be prepared by cleaning and heating it as indicated at 6 to remove sizing char, for example. The fiber may then be coated with its first environmental barrier coating at 8. Such a coating may be ytterbium doped silicon carbide. After coating 8, a fiber interface coating 10, such as a boron nitride coating may be applied over top. Next, structural and protective coatings 12 may be applied over the interface coating 10. Such an illustrative example includes a silicon carbide coating. Additional fiber layers may be applied at 14. Lastly, a CMC matrix 16 may be completed with slurry and melt infiltration.

(11) An end cross-sectional view of a PRIOR ART fiber material 18 and coating is shown in FIG. 2. The prior art coating includes an interface coating 20 surrounding the periphery of fiber material 18. Structural layer 22 is then applied over interface coating 20.

(12) In contrast, the end sectional view of fiber material 18 in FIG. 3 includes environmental barrier coating 24. This coating is applied according to step 8 from FIG. 1. An interface coating 26 as applied at 10 in FIG. 1 is then applied over environmental barrier coating 24. And lastly, structural layer 28 is applied over interface coating 26 as described with respect to step 12 in FIG. 1.

(13) Advantages may include extending fiber life and, therefore, composite life; reducing or eliminating damage to fiber surfaces during interface coating deposition (e.g. incompatibility of carbon and boron nitride deposition); providing additional layers that provide an opportunity to manage thermal and mechanical incompatibilities between a fiber and subsequent coatings; increasing ultimate strength resulting from surface defect reduction; and increasing creep strength if the fiber coating has a higher creep capability than the fiber.

(14) The view of FIG. 4 shows fiber 18 having a multi-layer environmental barrier coating 30 applied over top. The interface coating 26 is then applied over coating 30. And a structural layer or EBC multi-layer 32 is applied over interface coating 26.

(15) The following are non-limiting illustrative embodiments of environmental barrier coatings:

(16) Preform Based CMC

(17) 1. A Hi Nicalon preform is constructed at 36% fiber volume and assembled in tooling for Chemical Vapor Infiltration (CVI);

(18) 2. the preform is cleaned using air at about 600 degrees C. to remove sizing char from the fiber;

(19) 3. the fiber is coated with 1 m of ytterbium doped silicon carbide (SiC) by CVI;

(20) 4. a boron nitride (BN) interface coating is applied at 0.5 m;

(21) 5. a SiC coating of 2 m is applied by CVI; and

(22) 6. the CMC matrix is completed with slurry and melt infiltration.

(23) The composite demonstrates improved life after matrix cracking as a result of the well-bonded, environmentally resistant layer on the fiber.

(24) CMC Made with Pre-Coated Fiber

(25) 1. A Hi Nicalon S fiber is coated in tow form with 1 m of yttrium doped SiC by a chemical vapor deposition (CVD) process;

(26) 2. a subsequent CVD process applies a silicon doped boron nitride coating of 0.3 m;

(27) 3. the fiber in the tow is coated with silicon nitride of 0.3 um and SiC of 0.1 m;

(28) 4. the tow is processed with a SiC slurry and binders to form a uni-directional tape;

(29) 5. the tapes are laminated and shaped then cured; and

(30) 6. the resulting body is infiltrated with Si to complete the CMC component.

(31) The composite demonstrates improved life after matrix cracking as a result of the well-bonded, environmentally resistant layer on the fiber.

(32) Preform Based CMC II

(33) 1. A T-300 carbon fiber preform is constructed at 36% fiber volume and assembled in tooling for CVI;

(34) 2. the fiber is coated with alternating layers of SiC (four layers) and boron carbide (three layers) nominally 0.1 m each for a total of 0.7 m;

(35) 3. a silicon doped BN interface coating is applied at 0.5 m; and

(36) 4. matrix densification continues by CVI with alternating layers of SiC and boron carbide nominally 0.1 m thick until full density is achieved.

(37) The composite demonstrates improved life after matrix cracking and interface coating cracking as a result of the well-bonded, environmentally resistant layer on the fiber. It may be beneficial to use both a coating to protect the fiber that is well bonded (this disclosure) in conjunction with a fiber interface coating that demonstrates improved environmental resistance.

(38) While the disclosure has been described in this detailed description, the same is to be considered as exemplary and not restrictive in character, it being understood that only illustrative embodiments thereof have been described and that changes and modifications that come within the spirit of the disclosure are desired to be protected.