Filament wound composite tools and related methods

Abstract

Composite products and related methods are disclosed. In some examples, methods of filament winding composite components and products, such as a sleeve and/or a mandrel for use in down-hole applications, are disclosed. The winding of components can involve using a percentage of fiber roving strands that are blown during manufacture such that they have fiber loops that when wound as layers forms bridges across the discrete layers to enhance the inter-laminar strength of the composite product.

Claims

1. A mandrel made of a composite material comprising: fiber bands forming plurality of filament wound layers that include a first filament wound layer and a second filament wound layer defining an elongated body with a hollow core; each of the first filament wound layer and the second filament wound layer comprising a first strand of the fiber bands comprising a standard roving strand substantially without strand loops; each of the first filament wound layer and the second filament wound layer comprising a second strand of the fiber bands comprising a blown roving strand having strand loops surrounding a core bridging between the plurality of filament wound layers of the elongated body to enhance interlaminar shear strength; and resin for binding the first and second filament wound layers; wherein the standard roving strand of the first filament would layer and the blown roving strand of the second filament wound layer are intermingled to form an intertwined bundle; and wherein the blown roving strand of the first filament wound layer are intermingled with the blown roving strand of the second filament wound layer.

2. The mandrel of claim 1, wherein a first layer of fiber band is wound at 86 degree angle relative to a lengthwise axis of the elongate body to within +/5 degrees.

3. The mandrel of claim 2, wherein a second layer of fiber band is wound at 45 degree angle relative to a lengthwise axis of the elongate body.

4. The mandrel of claim 1, wherein the mandrel is part of a frac or bridge plug down-hole tool.

5. The mandrel of claim 1, further comprising a resin matrix that binds the different bands together.

6. The mandrel of claim 1, further comprising a sleeve wound to the mandrel and wherein the sleeve comprises strand loops bridging between filament wound layers for forming the sleeve.

7. The mandrel of claim 1, wherein the fiber bands are formed of the standard roving strand and the blown roving strand intermingled in a ratio of 5% to 95% of the blown roving strand compared to the standard roving strand.

8. The mandrel of claim 7, wherein the intertwined bundle is formed of two strands of the standard roving strand and one strand of the blown roving strand.

9. The mandrel of claim 1, wherein the blown roving strand of at least one of the first filament wound layer and the second filament wound layer comprises a section having sectional portions of individual strands each having different lengths respectively.

10. A method of filament winding a down-hole product comprising: using blown glass fiber roving strands comprising strand loops with standard roving strands substantially without strand loops as fiber bands, the standard roving strands and the blown glass roving strands of the first filament would layer and the second filament wound layer being intermingled to form an intertwined bundle; and winding a plurality of filament wound layers using the fiber bands to form the down-hole product having a body, the plurality of filament wound layers include a first filament wound layer and a second filament wound layer, and enhanced interlaminar shear strength; wherein the blown glass fiber roving strands of the first filament wound layer are intermingled with the blown glass fiber roving strands of the second filament wound layer inside a resin matrix.

11. The method of claim 10, further comprising forming an enlarged sleeve at an end of the down-hole product, the enlarged sleeve comprising a composite layer having blown glass fiber roving strands comprising strand loops with standard roving strands.

12. The method of claim 10, wherein the down-hole product is a mandrel comprising an elongated body comprising a bore.

13. The method of claim 10, further comprising a final over-layer wound at a different angle than angles used to form the plurality of filament wound layers.

14. The method of claim 13, wherein the final over-layer is wound at around a 3 to 10 degree angle relative to a lengthwise axis of the body.

15. The method of claim 10, wherein the down-hole product is a sleeve comprising the body with a bore.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) These and other features and advantages of the present device, system, and method will become appreciated as the same becomes better understood with reference to the specification, claims and appended drawings wherein:

(2) FIG. 1 is a downhole tool formed, at least in part, in accordance with the methods and techniques of the present disclosure.

(3) FIG. 2 is a side view showing a roll of composite roving material.

(4) FIG. 3 is a side view showing a section of a standard composite or fiber roving strands.

(5) FIG. 4 is a side view showing a section of blown fiber roving strands.

(6) FIG. 5 is a fiber band having both standard roving strands and blown roving strands.

(7) FIG. 6 is a section of a tube, tool, or mandrel manufactured or formed in accordance with the methods and techniques of the present disclosure.

(8) FIG. 7 is a cross-sectional side view of a section of the tube of FIG. 6, which shows the fiber loops bridging between the wound layers.

DETAILED DESCRIPTION

(9) The detailed description set forth below in connection with the appended drawings is intended as a description of the presently preferred embodiments of high strength composite components made using a percentage of blown fiber roving strands provided in accordance with aspects of the present device, system, and method and is not intended to represent the only forms in which the present device, system, and method may be constructed or utilized. The description sets forth the features and the steps for constructing and using the embodiments of the present device, system, and method in connection with the illustrated embodiments. It is to be understood, however, that the same or equivalent functions and structures may be accomplished by different embodiments that are also intended to be encompassed within the spirit and scope of the present disclosure. As denoted elsewhere herein, like element numbers are intended to indicate like or similar elements or features.

(10) With reference now to FIG. 1, a downhole tool 100 provided in accordance with aspects of the present disclosure is shown situated in a well bore 102, which can be a production casing, an intermediate casing, or a surface casing. The downhole tool 100 is a frac plug system and includes a ball seat 104 for receiving a closing ball or frac ball (not shown). However, in other embodiments, the downhole tool can be a bridge plug that utilizes the high strength winding method and system of the present disclosure involving blow roving strands.

(11) As shown, the tool 100 has a first end 90 and a second end 80 and a mandrel 108 running through the tool, which may be a composite formed by winding roving strands comprising loops for bridging between adjacent layers. A sleeve 106 is shown attached to the mandrel 108, which has a bore 110 for fluid flow. In one example, the sleeve 106 is attached to the mandrel 108 without any pin, i.e., a pin-less connection. In alternative embodiments, one or more pins are used to secure the sleeve and the mandrel in combination with adhesive, as further discussed below. As further discussed below, the sleeve 106 may also be made from a composite material comprising blown roving strands.

(12) A spacer ring 112 is abutted against a shoulder 114 defined by the sleeve 106 and optionally pinned to the sleeve with one or more pins 116. The spacer ring 112 supports a slip back up or slip ring 118, which has a tapered interior surface for riding up against a tapered surface of the slip wedge 120 to bite against the casing when set. A second set of slip wedge 120 and slip ring 118 is provided closer to the second end 80 for gripping the tool assembly 100 against the casing.

(13) A packer shoe 122 is provided adjacent the packer assembly 124, which in the current embodiment has three packer rings 126. In other examples, a different number of packer rings is used, such as one, two, or more than three. The upper and lower packer shoes 122 are configured to compress the packer assembly 124 when the downhole tool 100 is set, which causes the three packer rings 126 to expand outwardly away from the mandrel 108 to seal against the casing.

(14) A nose section 128 is provided at the second end 80 of the downhole tool 100, which may be used to engage a crown (not shown) of another downhole tool. In the present embodiment, the nose section 128 is attached to the mandrel 108 without any pin, i.e., a pin-less connection. In alternative embodiments, one or more pins are used to secure the nose section 128 and the mandrel in combination with adhesive, as further discussed below. In yet other examples, the nose section 128 is threaded to the mandrel 108.

(15) Fiberglass strands called rovings are used for filament winding, which may be used to form the mandrel 108 and/or the sleeve 106 described herein. In other examples, other materials such as carbon fiber is used in conjunction with or instead blown glass roving. The rovings for winding can be bundled strands or woven roving cloth, in which large strands are weaved into sheets. Typical rovings are made from a collection of glass filaments. In other examples, other composite materials are used, such as carbon and aramid. The filaments are smooth, have relatively constant diameter, generally equal in length, and are bundled together to make a roll of roving material 130, as shown in FIG. 2. To enhance interlaminar shear strength between the wound layers of rovings, a process is disclosed whereby the roving is blow or blown so that the fiber produced during the manufacturing of the filaments form filament loops that stand out from the roving. This is analogous to bundling a plurality of strands with length X and strands with length X+Y and forcing the ends of both types to align so that the longer strands fold randomly to form filament loops. A typical blown roving will have about 10% to 30% of the strands that stand out from the basic roving bundle as loops. When one examines a standard roving 132, it is smooth, such as that shown in FIG. 3. When on examines a blown roving 134 it is fuzzy in appearance, such as that shown in FIG. 4. The fuzzy appearance is caused, at least in part, by a plurality of loops 136 that undulate around a general core. The loops 136 are generally continuous about the length of the roving material. However, it is possible to have broken stray strands.

(16) If a percentage of blown roving strands 134 is used in conjunction with standard roving strands 132 to make up a fiber band 138 (FIG. 5) laid down by a filament winding machine, the fiber strand loops 136 of the blown roving strands inter-mingle between filament wound layers that have been laid down to create enhanced interlaminar strength. With reference to FIG. 5, a fiber band 138 comprising three filament strands is shown with two of the strands being standard rovings 132 and one being a blown roving strand 134 formed as an intertwined bundle or band 138. The fiber band 138 is used with a filament winding machine to wind around a removable core or mandrel, which acts as a temporary structure to enable winding. The winding is repeated with each layer laid down at alternating angles or at different angles relative to the axis of the removable core. In some examples, more than three strands are used to form the fiber band 138, which can vary in ratio of 5% to 95% blown roving strands 134 compared to standard roving strands 132. Thus, in one example, there are 4-30 strands of standard roving strands 132 and 3-27 blown roving strands 134 forming the fiber band 138 used for filament winding to form an elongated tube, such as a mandrel and/or a sleeve for use in downhole tools.

(17) Thus, an aspect of the present disclosure is understood to include a fiber band 138 having at least two different types of strands, such as standard roving strands 132 and blown roving strands 134 in a ratio of 5% to 95% blown roving strands with the balance of standard roving strands. The blown roving strands 134 are understood to include undulating loops 136 formed or surrounding a core. In the example shown, the loops are formed by joining strands of different lengths and forcing the ends of the different lengths to meet. A further aspect of the present disclosure is understood to include a method of forming a fiber band 138 having at least two different types of strands, such as standard roving strands 132 and blown roving strands 134 in a ratio of 5% to 95% blown roving strands with the balance of standard roving strands. The method can further comprising winding the fiber band 138 around a temporary core to form a mandrel or a sleeve. The winding of the fiber band 138 can comprise winding each layer laid down at alternating angles or at different angles relative to the axis of the removable core.

(18) FIG. 6 is a side view of a section of an elongated composite tube 140 formed by filament winding a plurality of fiber bands 138 having strands of both standard rovings 132 and blown roving strands 134. For example, a +/45 degree layer may be first wound onto the tooling used to make the elongated tube. In other examples, the first layer is wound at a 86 degree angle to within +/5 degrees. For example, the first layer can be wound at 81 degrees or at 91 degrees or anywhere in between. The first layer 137 has inter-weaving of the fibers as the material is laid down in +45 degree and then 45 degree orientation (or 45 then +45 degree orientation). The next layer 137 is then applied over the top of the prior layer 137 until adequate thickness is achieved, which can range from 0.25 inches to 1.5 inches or on standard 5.5 inch casing plugs and significantly more for larger casing plugs. In other examples, different winding angles are used, for example anywhere from +/25 degrees to +/60 degrees. The layers 137, when cured with resin as a matrix for holding the bands 138 together, have much stronger interlaminar strength, i.e., strength between the layers 137, due to the numerous strand loops 136 that span between the layers 137 to act as multiple composite links or bridges that join the layers together. The interlaminar strength of the disclosed composite tube formed by fiber bands 138 comprising standard rovings 132 and blown rovings 134 is much stronger than layers formed with just standard strands and resin and without strand loops 136, which are shown laid down by the resin used to hold the bands.

(19) Also shown in FIG. 6 is an over-layer 142 that is wound at a different angle, such as 3-10 degrees, than the base layers 137 to increase the shear strength of the composite tube connection to bonded sleeves.

(20) FIG. 7 is a schematic cross-sectional side view of a section of the composite tube 140 of FIG. 6. As shown, the fiber loops 136 bridge across between wound layers 137. In other words, fiber loops 136 are captured between the layers 137 inside the resin. In a composite, it is the fiber that creates the strength and the resin is what holds the fibers together. The ratio of blown roving strands and standard roving strands used to create the fiber lay-down band when winding can be tailored to meet the interlaminar shear strength requirements for the composite tube application. For example, frac and bridge plug applications may require different blends of standard to blown roving strands and different tube thicknesses. Tests have shown that the shear strength between the layers can easily be increased by 20% or more by using the disclosed method involving winding of fiber bands 138 comprising both standard roving strands and blown roving strands in different ratios to form the disclosed mandrel or composite tube. This increase in strength can make the frac or bridge plug suitable for higher temperature and/or higher pressure down-hole applications in a cost effective way.

(21) Strands of blown roving can also be interspersed between layers of woven cloth as the cloth is convolute wrapped as a means to enhance the interlaminar shear strength between layers of cloth by incorporating fiber loops that bridge between the layers. Thus, an aspect of the present disclosure is a composite mandrel, sleeve, or both comprising woven cloth with the cloth having blown roving strands interspersed therein. A further aspect of the present disclosure is a method for forming a mandrel, a sleeve, or both comprising convolute wrapping a plurality of layers around a removable core with woven cloth and wherein the woven cloth comprises blown roving strands interspersed therein.

(22) Although limited methods and embodiments for forming a composite tube or mandrel using a blend of standard and blown roving strands and their components have been specifically described and illustrated herein, many modifications and variations will be apparent to those skilled in the art. Also, well known processes within the composite manufacturing industry has not been described, such as curing time and temperature and the type of resins that can be used. Similarly, while glass, carbon fiber and other specific composite materials have been identified, other commercially available fibers may be used provided fiber bands comprising blown fiber rovings are incorporated. Accordingly, it is to be understood that the composite tube or mandrel for high pressure and temperature applications constructed according to principles of the disclosed device, system, and method may be embodied other than as specifically described herein. The disclosure is also defined in the following claims.