Integral Composite Piano Hinge, Composite, Assemblies With An Integral Piano Hinge, And Methods Of Manufacture

Abstract

An integral composite piano hinge assembly, and a method of making such an assembly. The assembly is made from a series of separate plies that are saturated with hardened resin to define a multi-layer composite structure, and a series of interleaved knuckles made from one or more composite tubes located within the plies such that at least one ply lies below the tube and at least one ply lies above the tube. The piano hinge may be an integral part of a structure such as a transom bracket.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

Various other objects, features and advantages of the present invention will become fully appreciated as the same becomes better understood when considered in conjunction with the accompanying drawings, in which like reference characters designate the same or similar parts throughout the several views, and wherein:

FIG. 1 is a cross section of a simple form of composite trim tab with integral transom bracket to trim plane piano hinge according to this invention, before it is cut into separate trim tab and transom bracket pieces;

FIGS. 2A, 2B and 3 illustrate steps in the process for producing the composite trim tab of FIG. 1;

FIG. 4 is a plan view of the composite trim tab produced according to the process illustrated in FIGS. 2 and 3 following cutting of the loops to form the knuckles of the two hinge half portions;

FIG. 5 is an isometric view of the trim tab of FIG. 4;

FIG. 6 is an exploded view of the trim tab assembly using the trim tab of FIGS. 1-5;

FIG. 7 is an isometric view of the assembled trim tab of FIG. 6;

FIG. 8 is a plan view of another embodiment of a composite trim tab of the invention following cutting of the loops to form the knuckles;

FIG. 9A is an isometric view of a back draft damper of the invention that includes an inventive integral composite piano hinge; and

FIG. 9B is an isometric view of the damper of FIG. 9A in place in an exhaust duct.

DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION

Referring to the drawings, FIG. 1 illustrates a cross section of a simple form of composite trim tab 20 according to the invention. Integral trim tab 20 comprises composite loop (tube) 22, and two outwardly extending flat or planar composite plates made of multiple layers or plies of composite material. One plate forms the transom bracket 24, and the other forms trim plane 26. Loop 22 is comprised of a prefabricated tube, preferably formed by pultrusion and having integral carbon fibers.

In an alternate embodiment of the invention the fabrication of loop 22 is facilitated by use of a removable insert or mandrel, removed after fabrication of the integral planar plate making up bracket 24 and trim plane 26, rather than a separate inserted tube 22.

Referring to FIGS. 2A and 2B of the drawings, the composite trim tab 20 of the invention is produced preferably by the interlaminar vacuum infusion process, wherein the prefabricated cured composite loop tube 22 is capped with an insert 48 with an outer diameter that matches the inner diameter of tube 22 such that the tube is sealed from resin infiltration. The then capped tube 22 is placed within the composite ply sequence (also called a “preform” herein) comprising dry laminae 28, 30, 32, 34, 36, 38, 40 and 42, within a two part tool (mold) in of which one half 44 contains a trough 46 to receive the prefabricated loop tube, while the opposing half 50 remains planar relative to the opposing planar surface of plate 44. In an alternate embodiment of the invention, both plate 44 and plate 50 contain a receiving trough relative to the loop tube and laminae. In yet another embodiment of the invention both plate 44 and plate 50 remain planar to each other.

To enable the resin infusion process, infusion flow reinforcement layer 32 is placed within the laminae of the preform. The use of a three-dimensional spacer fabric such as disclosed in U.S. Pat. No. 7,048,985 (the disclosure of which is incorporated herein by reference) is preferable with respect to the trim tab fabrication as the fabric can be designed to impart damage tolerance to the composite structure. In the preferred embodiment, the spacer fabric is Polybeam® 703 fabric from Polynova Composites, Milford, Mass. Polybeam is made from thermoplastic fibers (typically made from PET). The thermoplastic material, particularly in the transverse (or “Z direction”) fibers, provides a vibration damping characteristic to the structure that includes the fabric. HIFLUX90™, also available from Polynova Composites, is made from high tenacity PET and so would also impart such damping characteristics. As trim tabs are inherently subject to substantial stresses, the spacer fabric may increase the useful life of the trim tab. As taught in the patent incorporated herein by reference, the spacer fabric also speeds resin distribution through the preform, which decreases the manufacturing cost. The infusion flow reinforcement 32 is extended beyond the two opposing edges of tool 44 and 50 such that contact with resin inlet 52 and vacuum outlet 54 is maintained where inlet 52 and outlet 54 are each made up of a tee connector 56, spiral wrap 58, and tubing 60.

Referring to FIG. 3 in this example the assembly of FIGS. 2A and 2B is placed on surface 62 and surrounded by a two-sided sealant tape 64 over which a flexible vacuum bag (not shown in the drawings) is placed, thus forming a vacuum envelope. Sealant tape 64 is placed over tube 54 at location 66, thereby providing a means of communication within the envelope without breaking the vacuum bag seal. Inlet 52 is then closed and vacuum pressure is applied through tube 54 to collapse the flexible vacuum bag under atmospheric pressure against the assembly. The vacuum serves to consolidate the assembly via atmospheric pressure, thereby shaping the fibers in the mold, and to remove any entrapped air. Resin is then introduced into the envelope via inlet 52, and the vacuum serves to draw the resin through the fiber pre-form via the three-dimensional spacer fabric. Vacuum pressure is maintained until the laminate is fully saturated with resin and subsequently cures.

Referring to FIG. 4, loop tube 22 of composite 20 is cut as illustrated by gap 68 via water jet or other means to provide an aligned series of evenly spaced tubular knuckles 70 formed integrally along the mating edges of the transom bracket 24 and the trim plane 26. FIG. 5 is an isometric view of FIG. 4.

FIG. 6 is an exploded view of a trim tab assembly incorporating composite trim tab 20. Bracket 24 is adapted to be mounted on the transom “t” of a boat near the surface of the water “w”. Bracket 24 is attached to the transom by fasteners 72 passing through openings 74, then through openings 76 of blacking plate 78.

The trim plate 26 is pivotally mounted to the transom bracket 24 at mating tubular knuckle 70 and held in place with hinge pin 80. The diameter of hinge pin 80 matches the inner diameter of loop 22. Pin 80 is preferably made of pultruded carbon fiber. As loop 22 is a cured composite tube, it will not consolidate as the preform is cured. This allows the tube to remain open to its normal diameter. In contrast, the use of a prepreg tube subjects the tube to consolidation (collapse) during the autoclave cure process, thus requiring a mandrel to be used in the tube to keep the tube open through the cure cycle. The mandrel is an extra step, and can also be very difficult to remove due to the clamping force on the mandrel caused by tube collapse. Horizontal movement of trim plane 26 is restricted by the use of bushings 82 placed in the spaces between the hinge knuckles created by the cutting process. Angular penetration of the trim plane to the water surface is facilitated by an actuator 84 attached to the transom via bracket 86 and to the trim plane via bracket 88.

FIG. 7 is an isometric view of the assembled trim tab of FIG. 6.

FIG. 8 is a plan view of an alternative embodiment of a trim tab for the invention. Trim tab assembly incorporating integral trim tab 100 includes two identical closely spaced loop tubes 106 and 108. Loop tube 106, when cut as shown by gap 110, defines the series of spaced knuckles on the edge of transom bracket 104, while loop tube 108, when cut as shown by gap 112, defines the series of spaced mating knuckles on the edge of trim plane 102. The use of two loop tubes allows the removal of alternate lengths from each tube (for example, length 118 between knuckles 115 and 117) that, together with the two end cuts that define the ends of the removed length, is the same length as a knuckle, to provide a space into which an adjacent knuckle from the other half of the hinge just fits. Thus, adjacent interleaved knuckles (for example knuckles 115, 116 and 117) are long enough such that the gap between adjacent knuckles in the assembled hinge is very small. This may allow the hinge assembly to forego the use of bushings that in the first embodiment are used to inhibit relative horizontal movement of the transom bracket and trim plane.

FIGS. 9A and 9B show another example of an assembly using an inventive composite piano hinge. Back draft damper assembly 200 includes plates 202 and 204 joined by piano hinge 210. Assembly 200 can be made in the same manner as the transom bracket described herein. Piano hinge 210 comprise knuckles 220, 222 and 223 that are on the inner edge of one of plates 202 and 204, and interleaved knuckles 224 and 225 that are on the inner edge of the other of these plates. Piano hinge 210 allows the plates to pivot relative to one another about the longitudinal axis of the hinge, so that the open area within exhaust tube 250 can be controlled as desired. One application of this is to close tube 250 when the exhaust fan (not shown) is off, to prevent a backdraft down the exhaust tube. Composite damper assembly 200 is corrosion resistant and can be made to provide insulating properties over the metal sheets currently used as dampers.

The invention is applicable to any assembly that can use a piano hinge and would benefit by having a composite hinge (whether or not the rest of the assembly is itself made from composite material). For example, a composite hinge that could be fastened to non-composite members could be fashioned to have a shape similar to damper assembly 200, but likely with rectangular shaped plates adjacent the hinge rather than the semicircular plates shown in FIGS. 9A and 9B. Such plates could be screwed or bolted to the members that are being connected by the composite hinge.

Alternatively, as is the case with the two exemplary assemblies shown in the drawings, the entire assembly can be fabricated of composite material. In this case, preferably the assembly would be made integrally as described above, and then separated into relatively moveable parts such as by cutting through the composite, also as described above. Alternatively, the two relatively moveable parts could each be integral and manufactured separately, and then connected together by the hinge pin.

Non-Limiting Example of the Invention

The following is an example of a simple form of composite trim tab with integral transom bracket to trim plane piano hinge 20 of the invention.

Referring to FIG. 2A and FIG. 2B, where tool 44 and tool 50 are 11.75″×16″ in dimension, the dry laminae (28 through 42) in the preform before resin introduction consisted of 0.75 oz./ft.² chopped strand mat (Owens Corning M723A) 28, E-LT 1800 (Vectorply) 30, 0.196″ OD 0.118″ ID carbon fiber loop tube 22 (Air Dyne) capped at both ends with a 0.118″ OD solid insert 48 such that the tube is sealed from resin infiltration, 42 oz./yd. 3WEAVE (3TEX) 34 and 36, Polybeam® 703 (Polynova Composites) 32, 42 oz./yd.² 3WEAVE (3TEX) 38 and 40, and 0.75 oz./ft.² chopped strand mat (Owens Corning M723A) 42.

Upon assembly of the laminae (28 through 42), a vacuum port 54 consisting of a single 0.375″ (ID) vacuum tube 60 fitted to a tee 56, with 0.25″ ID spiral wrap 58 was placed in contact with the infusion flow reinforcement. The spiral wrap 58 maintains an open contact with the infusion flow reinforcement during processing. A like resin port 52 was placed across from vacuum port 54.

Referring to FIG. 3, a flexible vacuum bag was then fitted and sealed about the tool 44 and 50, the resin input tube 52 was sealed with a clamp, and vacuum was drawn. A gauge affixed to a standard resin trap read the vacuum, generated by a Dekker RVL020H rotary vane pump. When vacuum was stabilized at 29 inches of mercury the clamp was removed from the resin inlet tube, and the tube was subsequently placed in a vessel containing initiated vinyl ester resin (250 cPs Novoc 4020 Resin (initiated with 1% Norac Norox CHP)). The resin clamp was reaffixed to the inlet tube when the resin front reached the vacuum port (17 minutes) and the laminate was allowed to cure under vacuum. This results in a laminate that is fully saturated with resin and cured under vacuum, that remains consolidated after the resin fully cures and hardens.

A comparison of the properties of type 304 stainless steel, a common trim tab material, and the calculated properties of the above example composite trim tab are presented in Table 1.

TABLE 1
		High Strength
Property	Unit	Steel	Example 1
Thickness	Inches	0.105	0.218
Weight	Lbs./ft.2	4.39	2.06
0° Tensile Strength (Ultimate)	kSI	42.1	35.4
90° Tensile Strength (Ultimate)	kSI	42.1	35.4
0° Flexural Stiffness	lb-in	3,123	2,116
90° Flexural Stiffness	lb-in	3,123	2,623

As to a further discussion of the manner of usage and operation of the present invention, the same should be apparent from the above description. Accordingly, no further discussion relating to the manner of usage and operation will be provided.

With respect to the above description then, it is to be realized that the optimum dimensional relationships for the parts of the invention, to include variations in size, materials, shape, form, function and manner of operation, assembly and use, are deemed readily apparent and obvious to one skilled in the art, and all equivalent relationships to those illustrated in the drawings and described in the specification are intended to be encompassed by the present invention.

Therefore, the foregoing is considered as illustrative only of the principles of the invention. Further, since numerous modifications and changes will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation shown and described, and accordingly, all suitable modifications and equivalents may be resorted to, falling within the scope of the invention.

Claims

1. A composite trim tab assembly, comprising: a composite transom bracket;a composite trim plane; anda composite piano hinge connecting the trim plane to the transom bracket, to allow relative movement between the trim plane and the transom bracket.

2. The composite trim tab assembly of claim 1 in which the piano hinge comprises a series of interleaved knuckles, with some of the knuckles an integral part of the transom bracket and other knuckles an integral part of the trim plane.

3. The composite trim tab assembly of claim 2 in which the knuckles are made from one or more composite tubes.

4. The composite trim tab assembly of claim 3 in which the knuckles are made from a single tube that is cut to define the knuckles.

5. The composite trim tab assembly of claim 4 in which the transom bracket and the trim plane are made from a single multi-layer composite structure, with the tube located between distinct layers of the composite structure.

6. The composite trim tab assembly of claim 3 in which the knuckles are made from two composite tubes.

7. The composite trim tab assembly of claim 6 in which the tubes are proximate to one another.

8. The composite trim tab assembly of claim 6 in which the transom bracket and the trim plane are made from a single multi-layer composite structure, with the tubes located between distinct layers of the composite structure.

9. The composite trim tab assembly of claim 1 in which the transom bracket and the trim plane are made from a single multi-layer composite structure.

10. The composite trim tab assembly of claim 9 in which at least one of the layers comprises a three-dimensional spacer fabric.

11. An integral composite piano hinge assembly, comprising: a series of separate plies that are saturated with hardened resin to define a multi-layer composite structure; anda series of interleaved knuckles made from one or more composite tubes located within the plies such that at least one ply lies below the tube and at least one ply lies above the tube.

12. The integral composite piano hinge assembly of claim 11 in which the knuckles are made from a single tube that is cut to define the knuckles.

13. The integral composite piano hinge assembly of claim 11 in which the knuckles are made from two composite tubes.

14. The integral composite piano hinge assembly of claim 13 in which the tubes are proximate to one another.

15. The integral composite piano hinge assembly of claim 11 in which at least one of the layers comprises a three-dimensional spacer fabric.

16. A method of manufacturing integral composite piano hinge assembly, comprising: laying up in a mold a series of separate plies that define a multi-layer composite preform;locating one or more composite tubes in the preform such that at least one ply lies below the tube and at least one ply lies above the tube;consolidating the preform along with the one or more tubes under vacuum pressure;introducing into the consolidated preform a liquid resin to fully saturate the preform with resin;maintaining the vacuum while the resin hardens, to produce a consolidated composite assembly;cutting the assembly along the one or more tubes to produce a series of knuckles;interleaving the knuckles; andintroducing a hinge pin through the knuckles.

17. The method of claim 16 in which at least one of the plies comprises a three-dimensional spacer fabric.