US3861953A - Node-free boron composite filament - Google Patents

Abstract

A node-free boron composite filament comprising a filamentary substrate consisting essentially of carbon, a first coating on the substrate consisting essentially of pyrolytic graphite; and second coating consisting essentially of boron, the boron being continuous, of a thickness greater than 0.6 mil and of substantially constant diameter.

Description

United States Patent Basche et a1.

[4 1 Jan. 21, 1975 NODE-FREE BORON COMPOSITE FILAMENT Inventors: Malcolm Basche, West Hartford,

Conn.;Roy Fanti, Springfield, Mass; Francis S. Galasso, Manchester; Urban E. Kuntz, Hartford; Richard D. Schile, Wethersfield, all of Conn.

United Aircraft Corporation, East Hartford, Conn.

Filed: June 16, 1972 Appl. No.: 263,491

Related U.S. Application Data Division of Ser, No. 811,072, March 27, 1969, Pat. No. 3,679,475.

Assignee:

[56] References Cited UNITED STATES PATENTS 3,367,826 2/1968 Hcestand et a1. 117/46 CG. 3,369,920 2/1968 Bourdeau 117/46 CG. 3,409,469 11/1968 Kuntz ll7/D1G. 10 3,464,843 9/1969 Basche 117/46 CG. 3,479,205 11/1969 Morelock 117/46 CG. 3,537,877 11/1970 Reeves et a1 ll7/DlG 10 3,549,424 12/1970 Rice ll7/D1G, 10 3,565,683 2/1971 Morelock 117/D1G. 10 3,668,006 6/1972 Higgins et a1. l17/D1G. 10

Primary Examiner-Michael Sofocleous Attorney, Agent, or Firm-John D. Del Ponti [57] ABSTRACT A node-free boron composite filament comprising a filamentary substrate consisting essentially of carbon, a first coating on the substrate consisting essentially of pyrolytic graphite; and second coating consisting essentially of boron, the boron being continuous, of a thickness greater than 0.6 mil and of substantially constant diameter.

2 Claims, 1 Drawing Figure Zf jg. s 4% Z A Zi y 46 I NODE-FREE BORON COMPOSITE FILAMENT This is a division of application Ser. No. 811,072 filed Mar. 27, 1969, now US. Pat. No. 3,679,475.

BACKGROUND OF THE INVENTION This invention relates generally to a method for producing boron fiber and more particularly relates to a method for continuously depositing a relatively thick, substantially constant diameter boron coating on a carbon filament.

It is known that filamentary boron may be produced by pyrolytic techniques in a process wherein the boron is chemically deposited on a resistively heated carbon monofilament which is exposed to a reactant gas consisting of boron trichloride admixed with hydrogen.

The use of carbon as a filamentary substrate for boron has been recognized as offering the potential of significant improvements in the field of composite materials. Carbon, which in the present disclosure also includes graphitic material, possesses desirable characteristics in the form of electrical conductivity, hot strength, apparent chemical compatibility with boron, low density and an attractive cost feasibility relative to presently used tungsten filamentary substrates. Although the potential of carbon as a substrate is thus recognized, realization of this potential has been limited by the degradation of the carbon fiber during the coating process. It has been observed that, although the deposition of boron on the carbon substrate can be initiated uniformly, the coating quickly takes on a bamboo-like appearance with periodic nodes of boron thickened circumferentially along the fiber. The areas of increased deposition are caused by the appearance of a plurality of hot spots along the fiber and subsequent tests have revealed that the hot spots are caused by fractures in the carbon core which produce an irreversible change in the electrical properties of the fiber. It was found that the fractures occur irrespective of whether the process be static or continuous and with the fiber at a uniform temperature. Further investigations have indicated that the substrate fracturing is attributable to an unexpected growth phenomenon. As the boron is deposited on the carbon it undergoes a period of expansion which, when unchecked, exceeds the strength of the carbon filament and causes fracturing thereof. The exact cause and nature of this phenomenon is imperfectly understood at this time.

Recently, several techniques have been developed to improve the effectiveness of the basic continuous process through the close control of process conditions. In one of these methods, a continuous coating of nodefree amorphous boron is achieved by carefully limiting resident exposure of the carbon substrate in the reactor to a time period shorter than that at which fracturing occurs. At present however, the thickness of node-free boron which can be deposited on a one mil carbon filament by this technique is limited to a maximum of 0.6 mil to give a composite fiber of 2.2 mils.

SUMMARY OF THE INVENTION The present invention relates to the production of relatively large, constant diameter composite fibers, approximating 4 mils, in an improved process wherein filamentary carbon is modified through pretreatment. The invention contemplates a process wherein a nonreactive structural barrier is provided between the carbon and the boron in the nature of an electrically conductive precoating of pyrolytic graphite. In one particular embodiment of the invention, the pyrolytic graphite is deposited in thin layers to provide for relative slippage, without fracture, between the inner carbon bonded layer and the outer boron bonded layer to prevent hot spotting and provide a technique wherein relatively thick node-free boron coatings are achieved in reproducible fashion.

BRIEF DESCRIPTION OF THE DRAWING In the detailed description which follows, it will be convenient to make reference to the drawing which shows, in cross sectional view, an elevation of a reactor usable in the practice of the present invention.

DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring to the drawing, a reactor 10 is shown and described below. It is to be understood, however, that although a single reactor is shown which is suitable for both carbon and boron deposition, a plurality of such reactors are preferably disposed, in sequence, in the practice of the present invention. The reactor 10 comprises a tubular containment vessel 12 having dual gas inlets 14, 16 at the upper end and dual gas outlets or exhaust ports 18, 20 at the lower end thereof. During the deposition of pyrolytic graphite, the inlets I4 and 16 are utilized as a feed for a reactant gas mixture comprising a diluent gas, as for example the inert gas argon, and a carbon-containing gas such as methane. During the boron deposition, the inlets 14 and 16 are utilized as the feed for a reactant gas mixture comprising a boron halide and hydrogen. The containment vessel is typically formed of quartz or Pyrex, although a wide variety of other dielectrics and glasses are suitable. The gas inlet 16 and outlet 20 penetrate and are electrically connected to the metallic end plugs 24 and 26 which provide the end closures for the containment vessel and also, provide a convenient means through which the power may be supplied to the wire for resistance heating purposes.

The end plugs 24 and 26 are respectively formed to provide a well 30 and 32 for containing a conductive sealant 34, such as mercury. The mercury serves the dual purpose of providing a gas seal around the wire where it penetrates the end plugs and further providing electrical contact between the wire and the end plugs, through the gas tubes 20 and 26, the leads 23 and 25, and the DC power source 36. The end plugs are further provided with an annular surface groove 38, which communicates with the mercury well 34 in the plugs through passageways 40 and 42, to provide sealing between the plug and the abutting wall of the containment vessel whereby gas is prevented from escaping from the reactor around the periphery of the plugs.

The respective plugs are further each formed with contrally oriented orifices, 44 and 46, which are large enough to permit free passage of the wire therethrough but which, in combination with the wire, are small enough to retain the mercury, through surface tension forces, in the respective wells. The end plugs can be modified to include an orificed ruby, tungsten or other suitable insert through which the wire passes and which provides the sealant retainment function previously mentioned.

In the process of the present invention, a plurality of reactors are serially disposed and a filamentary substrate 50 is drawn therethrough from a feed reel 52 to a take up reel 54 which maintain the wire under a slight tension as it passes through the orifice openings. Power from DC source 36 to the filament may be conveniently controlled by a resistor 56 although other means are suitable.

In carrying out the process wherein graphite is deposited on the carbon substrate in the reactor, conditions conventionally used for effecting pyrolytic deposition of graphite may be used. For example, the carbon filament substrate may be resistively heated to a temperature in the range of 1,600 to 2,100C, preferably 1,900 to 2,000C. Temperatures above 1,600C are needed to insure the formation of graphite rather than pure carbon. The reaction may be carried out at a pres- 1 sure of one atmosphere. A reactant gas which is introduced into the reactant chamber can be any carboncontaining gas suitable for depositing pure carbon in graphitic form. In particular, methane, in an amount 10 to 50 mol% has given satisfactory results. The restricted concentration of methane in the reactant gas mixture is designed to prevent nodules from forming from too high a concentration and to prevent the formation of soot. The reactant gas mixture also includes a diluent gas such as nitrogen, hydrogen or one of the inert gases. Argon, in an amount of 50 to 90 mol% has been particularly useful. A preferred ratio in the reactant gas mixture is 20 mol% methane and 80 mol% argon. Similarly, those conditions suitable for effecting pyrolytic boron deposition may also be used. For example, the graphite-coated carbon substrate may be resistively heated to a temperature in the range of 700 to 1,400C, preferably 1,l00 to 1,300C. The reaction may be carried out at a pressure of one atmosphere and the reactant gases may contain a boron containing gas (e.g., boron trichloride) in an amount of to 75 mol% and a reducing gas, preferably hydrogen, in an amount 85 to 25 mol%. A preferred ratio of gases is 40% boron trichloride and 60 mol% hydrogen.

During one investigation, a one mil carbon monofilament, from Great Lakes Carbon Corporation, having a clean surface substantially free of imperfection, a circular cross section and an electrical resistance between 500 to 2,500 ohms per inch, was coated with two layers of pyrolytic graphite prior to boron deposition. The monofilament was passed through two reactors such as described above, each having an effective length of 3% inches. In each reactor, the argon was provided at 800 cc/min. and the CH at 200 cc/min. with a wire speed of 150 ft./hr. A substantially constant current of 145 ma gave a substrate temperature of 1,900C. The original diameter ofthc filament was 1.05 mil and, after the first pyrographite coating, the diameter was 1.16 mils. After the second pyrographite coating, the diameter was 1.3 mils.

The pyrolytic graphite coated fiber was then passed through a boron reactor. The first boron layer was achieved with boron trichloride feed of 400 cc/min. and a hydrogen feed of 600 cc/min. with a fiber speed of 300 ft./hr. through the 3% inch reactor. The fiber temperature was approximately 1,200C and the diameter measured 2.11 mils. The second boron layer was accomplished with a boron trichloride feed of 400 cc./min. and a hydrogen feed of 600 cc./min. with a fiber speed of ft./hr. The fiber temperature was 1,170C during deposition and the diameter measured 2.9 mils. The third boron layer was achieved with a BCI feed of 400 cc./min. and a hydrogen feed of 600 cc./min. with a fiber speed of 150 ft./hr. The fiber temperature during this pass was maintained at about 1,200C. There were no hot spots and no breakage of the carbon monofilament and the diameter of the final composite filament was smooth and uniform and measured 3.73 mils constant within i 0.0003 inch.

By way of comparison, a boron-carbon fiber was produced without pyrographite precoatings on the carbon. A one mil carbon monofilament was run through the reactor at a speed of 230 ft./hr. and at a temperature of 1,170C with a BCl feed of 400 cc./min. and an H feed of 600 cc./min. The resulting composite exhibited the undesirable bamboo structure as previously discussed. The fiber had an average diameter of 3 mils with nodes as large as 4 mils in diameter which were spaced 7 to 10 mils apart.

What has been set forth above is intended primarily as exemplary to enable those skilled in the art in the practice of the invention and it should therefore be understood that, within the scope of the appended claims, the invention may be practiced in other ways than as specifically described.

What is claimed is:

1. A node-free composite filament for use in fabrication of fiber reinforced articles comprising:

a filamentary substrate consisting essentially of carbon;

a first coating on the substrate consisting essentially of pyrolytic graphite; and

a second coating thereover consisting essentially of boron, said boron coating being continuous, of a thickness greater than 0.6 mil and of substantially constant diameter.

2. The composite filament of claim 1 wherein said first coating is in the form of at least two layers.

l I l UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION PATENT NO. 3,861,953 DATED January 21, 1975 INVENTOR(S) I MALCOLM BASCHE ET AL it is certified that error appears in the ab0ve-identified patent and that said Letters Patent are hereby corrected as shown below:

Column 2, line 59 "contrally" should read "centrally-'- Signed an sealed this 24th. day of June 1975.

(SEAL) fittest:

C. ZZARI'SE-LXLL DANN RUTH C. HA3 1? Commissioner of Patents Attasting Officer and Trademarks

Claims (2)

1. A NODE-FREE COMPOSITE FILAMENT FOR USE IN FABRICATION OF FIBER REINFORCED ARTICLES COMPRISING: A. FILAMENTARY SUBSTRATE CONSISTING ESSENTIALLY OF CARBON; A FIRST COATING ON THE SUBSTRATE CONSISTING ESSENTIALLY OF PYROLYTIC GRAPHITE; AND A SECOND COATING THEREOVER CONSISTING ESSENTIALLY OF BORON, SAID BORON COATING BEING CONTINUOUS, OF A THICKNESS GREATER THAN 0.6 MIL AND OF SUBSTANTIALLY CONSTANT DIAMETER.

2. The composite filament of claim 1 wherein said first coating is in the form of at least two layers.

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