A plate for use in fixating the position of a first bone segment relative to a second bone segment, the plate comprising a body portion having a plurality of attachment mechanisms located therein, wherein the attachment mechanisms include: a first group of three attachment mechanisms substantially positioned within 90°-150° of one another about a circle, and preferably within substantially 120° of one another, whereby the first group of attachment mechanisms is designed to facilitate attachment of a plurality of adjustable length struts to the plate; and a second group of attachment mechanisms substantially positioned about the circle that are designed to facilitate attachment of accessories to the plate, wherein the total number of the attachment mechanisms is a multiple of three.

Patent
   RE40914
Priority
Oct 20 1997
Filed
Apr 05 2001
Issued
Sep 08 2009
Expiry
Oct 20 2017

TERM.DISCL.
Assg.orig
Entity
Large
75
68
all paid
1. An orthopaedic spatial fixation system for holding bone parts comprising a plurality of fixation plates wherein each plate includes a body portion having n holes attachment structures positioned therein, whereby said holes attachment structures are substantially positioned along an arc of α° of a circle defined by a diameter d, and the cord a chord length between adjacent holes attachment structures is substantial substantially equal to 1 and is substantially equal between all attachment structures, and d = l ( 1 tan 2 ( α 2 n ) + 1 ) )
and whereby the diameter d for each plate within the system is unique, and the value for n(360/α) for each consecutive plate diameter d in the system is a multiple of 3, and
wherein at least two of the fixation plates are connected to each other by at least six substantially rigid, adjustable length struts, wherein each of the struts is disposed substantially diagonally with respect to its adjacent struts.
0. 15. An orthopaedic spatial fixation system, comprising a plurality of arcuate shaped fixation plates, wherein each plate comprises a plurality of attachment structures, at least some of which have substantially uniform sizes and a geometrical arrangement defined whereby the attachment structures are: (a) in sets of three, (b) spaced substantially 120 degrees apart from each other along an arc of the fixation plate, and (c) substantially equally spaced apart; wherein rotating a first one of the fixation plates substantially 120 degrees from a starting position in a plane substantially parallel to another one of the fixation plates causes the first fixation plate to present the same geometrical arrangement of attachment structures as the geometrical arrangement of the attachment structures of the another plate, and
wherein at least two of the fixation plates are connected to each other by at least six substantially rigid, adjustable length struts, wherein each of the struts is disposed substantially diagonally with respect to its adjacent struts.
0. 25. An orthopaedic spatial fixation system, comprising a plurality of fixation plates wherein each plate comprises a plurality of attachment structures, at least some of the attachment structures being in sets of three attachment points, each plate having a geometrical arrangement defined whereby the three attachment points in a set are spaced substantially 120 degrees apart from each other along an arc of the fixation plate; wherein at least two of the fixation plates are connected to each other by at least six substantially rigid, adjustable length struts, wherein each of the struts are disposed substantially diagonally with respect to its adjacent struts, and the number of attachment structures on each plate being a multiple of 3, whereby rotating the first fixation plate substantially 120 degrees from a starting position in a plane substantially parallel to another one of the fixation plates presents the same geometrical arrangement of attachment points as the geometrical arrangement of attachment points presented to the struts when the first fixation plate is in the starting position.
2. The orthopaedic spatial fixation system of claim 1 further comprising bone pins for interfacing the bone parts and plates; and,
a plurality of wherein the struts that extend between the plates to hold the plates in a selected position relative to one another and relative to the bone parts;
wherein the struts are attached to the plates at the holes attachment structures; and,
wherein a plurality of the struts have adjustable length sections for varying the length of the strut to adjust the relative position of the plates.
3. The orthopaedic spatial fixation system of claim 2 wherein the holes attachment structures on at least one of the plates are one hundred twenty degrees (120°) apart.
4. The orthopaedic spatial fixation system of claim 1 wherein rotation of one plate one hundred twenty degrees (120°) relative to an adjacent plate results in the same alignment of adjacent holes attachment structures as before such rotation of the plates.
5. The orthopaedic spatial fixation system of claim 1 wherein the plates are symmetrically configured so that if one plate is placed over an adjacent plate, the holes attachment structures in each plate can be aligned.
6. The orthopaedic spatial fixation system of claim 5 wherein the plates are symmetrically configured so that one plate can be flipped over without affecting the alignment of adjacent holes attachment structures.
7. The orthopaedic spatial fixation system of claim 2 wherein there are two plates and each plate includes 3 holes attachment structures.
8. The orthopaedic spatial fixation system of claim 7 wherein
there are the struts comprise only six struts each having a first end and a second end;
the first end of each strut is attached to one of the plates and the second end of each strut is attached to the other plate;
the ends of the struts are attached to the plates at the holes attachment structures; and, each hole attachment structure accommodates two strut ends, one from each of two adjacent struts.
0. 9. The orthopaedic spatial fixation system of claim 1, wherein the attachment structures are holes.
0. 10. The orthopaedic spatial fixation system of claim 1, wherein the circle comprises a groove and the attachment structures are clamps attached to the groove.
0. 11. The orthopaedic spatial fixation system of claim 1, further comprising markings or etches to designate the attachment structure positions.
0. 12. The orthopaedic spatial fixation system of claim 1, further comprising one or more plates being multiple diameter plates having a second set of attachment structures.
0. 13. The orthopaedic spatial fixation system of claim 12, wherein the second set of attachment structures is not spaced according to the diameter equation and chord length limitations.
0. 14. The orthopaedic spatial fixation system of claim 1, wherein the chord length between adjacent attachment structures is between about 0.48 inches and about 0.52 inches.
0. 16. The orthopaedic spatial fixation system of claim 15, whereby rotating the first fixation plate substantially 60 degrees from the starting position in a plane substantially parallel to another one of the fixation plates presents the same geometrical arrangement of attachment structures as the geometrical arrangement of the attachment structures of the another plate.
0. 17. The orthopaedic spatial fixation system of claim 15, wherein the number of attachment points is a multiple of six, providing 2×3 symmetry.
0. 18. The orthopaedic spatial fixation system of claim 15, wherein at least one of the fixation plates is ring shaped.
0. 19. The orthopaedic spatial fixation system of claim 15, wherein the plurality of attachment structures is positioned such that in use, at least some of the attachment structures on one of the plates move into alignment with at least some of the attachment structures on another plate as adjustment is effected.
0. 20. The orthopaedic spatial fixation system of claim 15, wherein the attachment structures are positioned along an arc of α° of a circle defined by a diameter d, and a chord length between adjacent attachment structures is substantially equal to l, and the defined relationship comprises d = l ( 1 tan 2 ( α 2 n ) + 1 ) )
0. 21. The orthopaedic spatial fixation system of claim 15, wherein the orthopaedic spatial fixation system is adapted to be positioned on a patient.
0. 22. The orthopaedic spatial fixation system of claim 15, wherein the struts comprise only six adjustable struts, a first end of each of the struts connected to one of the attachment structures on one of the fixation plates and a second end of each of the struts connected to one of the attachment structures on another one of the fixation plates, wherein the attachment structures connected to the struts are each connected to two struts.
0. 23. The orthopaedic spatial fixation system of claim 15, wherein the struts comprise only six adjustable struts, each strut connected at a first end to one of the attachment structures of one of the fixation plates and each strut connected at a second end to one of the attachment structures of another one of the fixation plates, wherein each attachment structure that is connected to a strut is only connected to one strut.
0. 24. The orthopaedic spatial fixation system of claim 15, wherein a chord length between adjacent attachment structures is between about 0.48 inches and about 0.52 inches.
0. 26. The orthopaedic spatial fixation system of claim 25, further comprising an accessory adapted to be attached to one or more of the fixation plates.
0. 27. The orthopaedic spatial fixation system of claim 25, wherein the orthopaedic spatial fixation system is adapted to be positioned on a patient.
0. 28. The orthopaedic spatial fixation system of claim 25, wherein the struts comprise only six struts, a first end of each of the struts connected to one of the attachment structures on one of the fixation plates and a second end of each of the struts connected to one of the attachment structures on another one of the fixation plates, wherein the attachment structures connected to struts are each connected to two struts.
0. 29. The orthopaedic spatial fixation system of claim 25, wherein a chord length between adjacent attachment structures is between about 0.48 inches and about 0.52 inches.

1. Field of the Invention

The present invention relates to a plate for use as part of an external fixation device, and more particularly to a unique hole pattern within the plate.

2. General Background and Description of the Prior Art

Traditional circular ring external fixation devices consist of Ilizarov-type devices that are based on a circumferential external fixator system disclosed by G. A. Ilizarov during the early 1950's. The Ilizarov system includes at least two rings or “halos” that encircle a patient's body member (e.g., a patient's leg), connecting rods extending between the two rings, transfixion pins that extend through the patient's boney structure, and connectors for connecting the transfixion pins to the rings. Use of the Ilizarov system to deal with angulation, translation and rotation is disclosed in “Basic Ilizarov Techniques,” Techniques in Orthopaedics®, Vol. 5, Nov. 4, December 1990, pages 55-59.

The Ilizarov system provides an external fixation frame that allows for gradual correction along and about six axes; however such frames require many parts and are relatively complicated to build and use in a clinical situation. In addition, often orthopedic external fixators such as Ilizarov frames must be modified after their initial application. Such modification may be necessary to convert from one correctional axis to another. Alternatively, such modifications may allow conversion from an initial adjustment type of frame to a weight bearing type frame, since some of the correctional configurations are not stable enough for weight bearing.

The rings used in the Ilizarov devices include a plurality of spaced apertures or holes that allow for the attachment of various accessories to the device. The pattern of Ilizarov ring holes is primarily determined as a function of the diameter of the ring. Conventional wisdom teaches that for any given diameter, the ring should include the maximum number of equally spaced arcuately positioned holes. Those skilled in the art believe that such hole positioning provides the surgeon with the greatest degree of flexibility in constructing the often times complicated and elaborate Ilizarov frame configuration. The Ilizarov ring holes, although equally spaced about a circle, are positioned such that the location of any given hole relative to another hole on additional rings attached thereto, is completely irrelevant.

Applicants have recently developed a new external fixation device known as the Taylor Spatial Frame™ external fixator. This device is described and claimed in the allowed U.S. patent application Ser. No. 08/782,731 entitled “Orthopaedic Fixation Device.” In addition, applicants have developed a unique method of using the Taylor Spatial Frame™ fixator that is the subject of allowed U.S. patent application Ser. No. 08/726,713 entitled “Method of Using An Orthopaedic Fixation Device.” Both of these patent applications are incorporated herein by reference. As disclosed in these prior patents, the Taylor Spatial Frame™ fixator, in its preferred embodiment, consists of two ring plates interconnected by six adjustable length struts. This device can be configured to correct virtually an infinite number of deformities, each of which would have otherwise required the construction of a specific custom Ilizarov frame.

As with the prior art Ilizarov fixator, the Taylor Spatial Frame™ fixator plates include a plurality of spaced apertures or holes therethrough for attaching accessories to the device. In addition, the plates include plurality of cavities or holes for attachment of the struts to the rings. Applicants have now developed a unique hole placement scheme for the Taylor Spatial FRAME™ fixator rings. This unique hole placement scheme takes advantage of the unique nature of the Taylor Spatial Frame™ fixator and the unique method of using the same, and provides substantial advantages over the unsystematically placed hole patterns utilized in Ilizarov rings.

It is an object of the present invention to provide a novel external fixation plate that can be used as part of the Taylor Spatial FRAME™ fixator, and facilitates the unique method of using the Taylor Spatial Frame™ fixator.

It is a further object of the present invention to provide a novel external fixation plate that easy to manufacture, and simplifies the fixator construction process.

It is a further object of the present invention to provide a novel external fixation plate that offers various clinical advantages over prior art designs by providing a convenient frame of reference to aid a surgeon in preoperative planning and surgical application of the device.

It is a further object of the present invention to provide a system of plates, wherein each plate within the system offers unique symmetrical properties and common hole spacing.

It is a further object of the present invention to provide a hole scheme for an external fixation plate that provides a clear geometric relationship between the holes on such plate relative to other holes on the same plate or holes on attached plates.

These and other objects are realized by a fixation plate that includes a plurality of attachment mechanisms located thereon. The attachment mechanism preferably consists of a plurality of equally spaced and symmetrically positioned holes. In accordance with a preferred embodiment, the present invention includes a plate having a body portion that includes a plurality of substantially equally spaced apertures or holes positioned arcuately therein. The holes are designed to facilitate attachment of a plurality of adjustable length struts that interconnect one or more plates, and the attachment of various accessories to the plates. The strut holes and the accessory holes may be indistinguishable or they may be different. The arrangement of the holes provides triple symmetry, and preferably 2×3 symmetry. Based on a defined geometric relationship between plate holes, a system of plates can be designed that offer triple symmetry or 2×3 symmetry.

FIG. 1 is a top view of a plate in accordance with one embodiment of the present invention.

FIG. 2 is a perspective view of an external fixation device incorporating one embodiment of the novel plate of the present invention.

FIG. 3 is an enlarged view of a portion of one of the plates shown in FIG. 2.

FIG. 4 is a perspective view of an external fixation device incorporating an alternative embodiment of the novel plate of the present invention.

FIG. 5 is an enlarged view of a portion of a plate of the present invention, and illustrates the geometric relationship between two adjacent holes.

FIG. 6 is a top view of a plate in accordance with an alternative embodiment of the present invention.

FIG. 7 is a top view of a plate in accordance with an alternative embodiment of the present invention.

FIG. 8 is a top view of a plate in accordance with an alternative embodiment of the present invention.

FIG. 9 is a top view of a plate in accordance with an alternative embodiment of the present invention.

FIG. 10 is a top view of a plate in accordance with an alternative embodiment of the present invention.

FIG. 11 is a perspective view of an external fixation device incorporating an alternative embodiment of the novel plate of the present invention.

Because of the unique nature of the Taylor Spatial FRAME™ fixator and the unique method of using the Taylor Spatial FRAME™ fixator, the position of a given hole relative to another hole, either on the same plate or a different plate, is very important. Indeed, we have found that the correct positioning of the holes simplifies the manufacturing and device construction processes, simplifies the method of using the device by simplifying the geometric analysis of the system, and provides a number of clinical advantages.

FIG. 1 illustrates a fixator plate in accordance with a preferred embodiment of the present invention. The plate 2 includes a circuit body portion 4 fabricated from a suitably strong and rigid material such as a metal, alloy, plastic, composite, or ceramic. The body portion 4 includes a plurality of substantially equally spaced apertures or holes 8 positioned arcuately therein. In the specific embodiment shown in FIG. 1, the center of the holes 8 form a complete circle as illustrated by the broken line 10, wherein the circle has a center c and a radius of r. It is important to note that each hole 8 may have a different diameter or shape as long as the center of the hole substantially intersects with the circle 10.

As illustrated in FIG. 2 and FIG. 4, the holes 8 are designed to facilitate attachment of a plurality of adjustable length struts 20 that interconnect one or more plates 2. In accordance with the preferred embodiment of the present invention, six struts 20 are used to interconnect two plates 2. In addition, the holes 8 are designed to facilitate attachment of various accessories to the plate 2, such as for example, wires (not shown), clamps 24, pins 26, additional plates, etc. In accordance with the embodiment shown in FIG. 1 and FIG. 4, the strut holes and the accessory holes are indistinguishable, i.e. any hole 8 can be selected to serve as a strut hole or an accessory hole. In accordance with an alternative embodiment, as shown in FIG. 2, the accessory holes 14 and the strut holes 12 are different.

As illustrated in FIG. 2, in accordance with one embodiment of the present invention, each plate 2 has three actual strut attachment positions 16. In addition, each plate 2 includes three additional strut positions 18 that are not actually used. The unused strut positions 18 are included to provide a 2×3 symmetrical design, which is discussed in greater detail below. In the preferred embodiment of the invention as shown in FIG. 2, the used strut attachment holes 16 should be positioned approximately 120° from one another so as to form a substantially equilateral triangle. Similarly, the unused strut attachment holes 18 should be positioned approximately 120° from one another so as to form a second substantially equilateral triangle. The two overlapping triangles are illustrated by broken lines in FIG. 1, and are designated triangle A and triangle B. Alternatively, one or more strut attachment holes 16, 18 can deviate slightly from its ideal 120° position. Such deviation, however, should be less than 30°, but preferably no more than 15°, and ideally less than 6°.

Unlike the unsystematically positioning of prior art Ilizarov ring holes, the holes 8 in the present device are preferably strategically positioned within plate 2 to provide 2×3 symmetrically throughout a complete system of plates. 2×3 symmetry is achieved when the holes are positioned such that the plate can be rotated in increments of 180° about a first axis and increments of 120° about a second axis, and each time maintain identical hole positions. For example, the plate 2 can be rotated 180° about an axis passing through center c and within the plane of the plate 2, i.e. the x axis shown in FIG. 2. Such a rotation would essentially flip plate 2 over. For both of the two possible positions, the hole pattern within plate 2 would be identical. This characteristic represents the “2” of the 2×3 symmetry. Similarly, plate 2 can be rotated in increments of 120° about an axis perpendicular to the plate and passing through center c, i.e. the y axis shown in FIG. 2. There are three possible positions that the plate 2 could assume by making 120° rotation about the y axis. Following each rotation, however, the resulting hole positions will remain unchanged. This characteristic represents the “3” of the 2×3 symmetry. In accordance with the present invention, a system of plates is provided, as described hereinbelow, wherein each plate within the system offers at least triple symmetry (i.e., the “3” symmetry), and preferably each plate offers complete 2×3 symmetry.

In order to obtain the 2×3 symmetry, as noted above, plate 2 should include two sets of three strut holes with each strut hole 12 positioned about 60° apart in a circle. In addition, 2×3 symmetry requires that the total number of holes 8 (including both strut holes 12 and accessory holes 14) be a multiple of six (6). For triple symmetry alone, however, the total number of holes 8 need only be a multiple of three (3). Furthermore, the accessory holes should be equally spaced. One skilled in the art will appreciate that asymmetrical “dummy” holes can be added to the plate 2. Such a plate would nonetheless fall within the scope of the present invention.

As illustrated in FIG. 3, the spacing between the accessory holes 14 can be measured in terms of the arc length larc along circle 10 or in terms of the chord length lchord. In accordance with the preferred embodiment, the distance between holes 14 is measured by the chord length Ichord, and such lengths are equal. Furthermore, the distance between each strut hole 12 and its adjacent accessory hole 14 need not be the same as the distance between two adjacent accessory holes 14. As illustrated in FIG. 3, this distance can be measured along arc as darc or along the chord as decor. In accordance with the preferred embodiment of the present invention, the chord lengths between every accessory hole 14 and its adjacent accessory hole 14 or strut hole 12 are equal, that is dchord=lchord. In addition, the chord length is should be greater than about 0.475 inch, but preferably is between about 0.48-0.52 inch, and most preferably equal to about 0.5 inch.

In accordance with the specific embodiment of the present invention illustrated in FIG. 2, the exact positions of the holes 8 are determined as follows. The process is very different from the unsystematic positioning of the holes in prior art Ilizarov devices, which starts with determining the ring diameter. The Taylor Spatial Frame™ fixator hole positions are determined by first determining the hole spacing, and then determining the number of holes that will be used. The present hole positioning scheme starts with the number of holes because it is important that the number be a multiple of three to maintain the requisite symmetry. Once the distance between the holes and the number of holes is determined, the diameter of the ring is defined by the formula: diameter = l ( ( 1 tan 2 ( 180 N ) + 1 ) )
where l is the chord distance between holes 8, and N is the total number of holes.

As illustrated in FIG. 5, for any given two adjacent holes 8, the angle between the holes is θ, and the chord between the holes is 1. An isosceles triangle T is formed by connecting the two adjacent plate holes 8 and the center c of the circle 10. If a line 28 having length b is formed in the middle of the isosceles triangle T, two right triangles are formed, and the following relationships exists: b 2 + ( 1 / 2 l ) 2 = r 2 and ( 1 ) TAN ( 1 / 2 θ ) = 1 / 2 l b ( 2 )
where r represents the radius of the circle 10. If for convenience we define v=½l and Q=tan (½θ), the following relationships can be derived from the above equations:

From Equation (1) b 2 = r 2 - v 2 ( 3 ) b = r 2 - v 2 ( 4 )

From Equation (2) Q = v b ( 5 )

Combining (4) and (5) Q = v r 2 - v 2 ( 6 )
solving for the radius r gives: r = v 2 Q 2 + v 2 or r = v 2 ( 1 Q 2 + 1 ) ( 7 )
Therefore, for any plate having N holes and a chord distance of 1 between adjacent holes, the diameter of the circle that defines the hole locations can be expressed mathematically as diameter = 2 ( ( l 2 ) 2 ( 1 tan 2 ( 1 / 2 θ ) + 1 ) ) ( 8 ) = l ( ( 1 tan 2 ( 1 / 2 θ ) + 1 ) ) ( 9 )
If the total number of holes in the ring will be N, then θ=360°/N, and diameter = l ( ( 1 tan 2 ( 180 N ) + 1 ) ) ( 10 )
Using the relationship defined in equation 10, a system of rings including a variety of ring diameters can be developed wherein each ring has triple symmetry and the hole spacing for each ring is the same. The following table illustrates such a system wherein the hole spacing in 0.5 inch:

TABLE I
Chord
Length (l) Number of Diameter angle (θ)
(inches) Holes (N) (inches) (degrees)
0.5 3 0.5776 130
0.5 6 1.0030 60
0.5 9 1.4519 40
0.5 12 1.9319 30
0.5 15 2.4049 24
0.5 18 2.8794 20
0.5 21 3.3548 17.143
0.5 24 3.8306 15
0.5 27 4.3069 13.333
0.5 30 4.7834 12
0.5 33 5.2601 10.939
0.5 36 5.7369 10
0.5 39 6.2138 9.281
0.5 42 6.6907 8.571
0.5 45 7.1678 8
0.5 48 7.6449 7.5
0.5 51 8.1220 7.059
0.5 54 8.5992 6.657
0.5 57 9.0764 6.316
0.5 60 9.5537 6
0.5 63 10.0309 5.714286
0.5 66 10.5082 5.454545
0.5 69 10.9855 5.217391
0.5 72 11.4628 5
0.5 75 11.9401 4.8
0.5 78 12.4174 4.615385
0.5 81 12.8948 4.444444
0.5 84 13.3721 4.285714
0.5 87 13.8497 4.137931
0.5 90 14.3269 4
0.5 93 14.8042 3.870968
0.5 96 15.2816 3.75
0.5 99 15.7590 3.635364
0.5 102 16.2364 3.529412
0.5 105 16.7138 3.428571
0.5 108 17.1912 3.333333
0.5 111 17.6686 3.243243
0.5 114 18.1460 3.157895
0.5 117 18.6234 3.076923
0.5 120 19.1008 3
0.5 123 19.5782 2.826829
0.5 126 20.0556 2.857143
0.5 129 20.5330 2.790698

The triple symmetry for the complete system is realized by only including rings where the numbers of holes in each plate is a multiple of three. Similarly, a system with complete 2×3 symmetry can be designed by using plates where the number of holes in each plate is a multiple of six.

As noted above, the arc length, as opposed to the chord length, between adjacent holes 8 can be fixed. If the arc length between the holes 8 is fixed, for a given arc length k and holes N, the circumference of the circle 10 will equal k×N. Therefore the diameter would be:
diameter=kN/π
Using this relationship, a plate system such as following can be made:

TABLE II
Arc
Length Number Diameter
(inches) of Holes (inches)
0.5 6 0.9549
0.5 9 1.4324
0.5 12 1.9099
0.5 15 2.3873
0.5 18 2.8648
0.5 21 3.3423
0.5 24 3.8197
0.5 27 4.2972
0.5 30 4.7746
0.5 33 5.2521
0.5 36 5.7296
0.5 39 6.2070
0.5 42 6.6845
0.5 45 7.1620
0.5 48 7.6394
0.5 51 8.1169
0.5 54 8.5944
0.5 57 9.0718
0.5 60 9.5493
0.5 63 10.0268
0.5 66 10.5042
0.5 69 10.9817
0.5 72 11.4592
0.5 75 11.9366
0.5 78 12.4141
0.5 81 12.8916
0.5 84 13.3690
0.5 87 13.8465
0.5 90 14.3239
0.5 93 14.8014
0.5 96 15.2789
0.5 99 15.7563
0.5 102 16.2338
0.5 105 16.7113
0.5 108 17.1887
0.5 111 17.6662
0.5 114 18.1437
0.5 117 18.6211
0.5 120 19.0986
0.5 123 19.5761
0.5 126 20.0535
0.5 129 20.5310

FIG. 4 illustrates an alternative embodiment of the present invention. Unlike the embodiment illustrated in FIG. 2, the adjoining struts 20 in FIG. 4 do not connect to the plates 2 at a single common hole 8. As a result, each plate 2 in FIG. 4 includes six (6) strut holes 32 that are connected to a strut 20. As illustrated, the adjacent connecting strut holes 32 are separated by a single unused hole 30. In other embodiments of the present invention, the adjacent connecting strut holes 32 may be separated by no holes or by more than one unused hole 30. When adjacent struts 20 do not terminate at a common hole a theoretical strut hole should be determined. As illustrated in FIG. 6, the theoretical strut hole 34 is positioned along the arc of circle 10 half way between the two actual strut holes 32, i.e. along the circle 10 at the bisector of the two actual strut holes. When adjacent struts terminate at a single strut hole as in FIG. 2, the theoretical strut hole is the actual strut hole. In accordance with the present invention, the theoretical strut holes 34 on plate 2 should form two overlapping triangles A, B in the same manner described above regarding the embodiment illustrated in FIG. 2. As with the actual strut holes, the chords connecting the theoretical strut holes 34 preferably form two substantially equilateral triangles. The theoretical strut holes 34, however, may deviate from their ideal 120° positions to the same extent described above with regard to actual strut holes.

The extent to which an actual strut hole 32 can deviate from its theoretical strut hole is limited. As this deviation increases, the range of movement between the two plates 2 is reduced. The reduced range limits the various configurations that the device can assume, and therefore, limits the types of deformities that can be corrected with the device. As a result, the deviation of an actual strut hole 32 from its theoretical strut hole should be less than about 30°, but can be less than 12°, and preferable no more than about 6°.

The hole spacing scheme of the present invention can be utilized to design plates having holes that do not form a complete circle. For example, a half plate or a ⅙ plate, as illustrated in FIGS. 7 and 8 respectively, can be designed. In addition, the plate itself need not be circular, as illustrated in the embodiment shown in FIG. 9.

The mathematical relationships between hole spacing, the number of holes and the diameter that are set forth above specifically relate to a hole pattern that forms a complete circle and includes equally spaced hole around the entire circle. These mathematical relationships, however, can be adapted to describe the hole pattern for a partial circle. For example, assume that you wanted n holes positioned about a partial ring that has an arc length of α°, i.e. 180° for a half ring, 90° for a quarter ring, etc. The number of such partial rings required to form a complete circle would be 360/α. The number of holes in such a theoretical circle (N) equals n(360/α). One would then use the number of holes for the theoretical complete ring (N) in the equations set forth above to define the hole positions needed to form the requisite partial plate.

In accordance with another embodiment of the present invention, a plate can include holes corresponding to more than one diameter within a given system. As noted above each system is defined by the hole spacing. An example is illustrated in FIG. 10 using the system defined above in Table I. The plate 2 includes two sets of holes 8. The first set 38 includes sixty (60) holes equally spaced (lchord−0.5 inch) along circle 10. As indicated above in Table I, the diameter of circle 10 is 9.5537 inches, and the radius r1=4.7769 inches. The second set of holes 40 consists of six groups of three holes, i.e. six partial plates. These hole are spaced along the next highest diameter within the system. Therefore, the diameter of circle 36 is 10.5082 and the radius r2=5.2541. Multiple diameter plates, such as shown in FIG. 10 are very useful. In such plates, the struts can be attached at one diameter, using for example hole set 40, and the accessories can be attached using the other diameters, using for example hole set 38.

It is important to emphasize that although the present invention is described in terms of accessory holes and strut holes, other attachment mechanisms can be used and still fall within the scope of the present invention. For example, each hole could be replaced with a peg that would facilitate attachment of a strut or accessory. Alternatively, an illustrated in FIG. 11, the plate 42 could include one continuous circular grove 44 that traces circle 10. Clamps 46 could be provided that attach to the groove 44 at any location. Such clamps 46 can easily be positioned to mimic the hole patterns described above. Indeed, such a plate 42 could included indicia such as markings 48 or etches 50 within the plate, that designate the hole positions described above.

The unique hole placement scheme described herein provides a number of advantages over the prior art. In particular, a ring that has 2×3 symmetry substantially simplifies the manufacturing process and the fixator construction process. With 2×3 symmetrical rings, one ring can serve as either the upper ring or the lower ring. As a result, a manufacturer need only make half as many ring designs for a system. In addition, if a surgeons using the device want to attach additional rings to the base Taylor Spatial Frame™ fixator, they need not overly concern themselves with having the proper ring, nor the proper orientation of the ring.

Key advantages also result from having a defined relationships between the various holes on a plate, and a defined relationship between various holes on different plates. In general, this facilitates the use of mathematical methods to analyze a fixation system, and determine the proper mode for correcting a deformity. From a clinical standpoint, it gives a surgeon a great deal of flexibility and aids in preoperative planning and surgical application of the device. For example, in cases of sever deformities the various bone fragments are completely out of alignment. In such cases it is difficult for a surgeon to place various plates with the same orientation on the various fragments. With the current invention, a surgeon when attaching the device can place reference wires at the same predetermined anatomical position on each unaligned bone fragment. One the surgeon determines the appropriate positioning of the first plate on the first bone fragment, the first plate is secured to the reference wire. Subsequent plates can then be easily positioned on the remaining bone fragments. A surgeon would attached the subsequent plates to the reference wires on the remaining fragments using the accessory holes at the same locations used with the first plate. The various plates would then be aligned after the correction is made. Such strategic placement of plates relative to one another facilitates the use of the unique method of using the Taylor Spatial FRAME™ fixator. Moreover, this provides an easy gauge during the course of the correction that allows the surgeon to judge if the correction is accurate or needs adjustment. Indeed, if the plate holes are not moving into alignment, the surgeon knows that an adjustment is needed. Furthermore, once the plates have returned to their neutral positions, with the holes in the upper and lower plates are perfectly aligned, and a surgeon can simply insert horizontal rods. Such rods could provide accessory stabilization if required.

Taylor, J. Charles, Taylor, Harold S

Patent Priority Assignee Title
10010346, Apr 20 2016 STRYKER EUROPEAN HOLDINGS III, LLC Ring hole planning for external fixation frames
10010350, Jun 14 2016 STRYKER EUROPEAN HOLDINGS III, LLC Gear mechanisms for fixation frame struts
10080585, Aug 11 2010 STRYKER EUROPEAN HOLDINGS III, LLC External fixator system
10082384, Sep 10 2015 STRYKER EUROPEAN HOLDINGS III, LLC Systems and methods for detecting fixation frame parameters
10149701, Oct 05 2009 STRYKER EUROPEAN HOLDINGS III, LLC Dynamic external fixator and methods for use
10194944, Feb 19 2013 Stryker European Operations Holdings LLC Software for use with deformity correction
10213261, Feb 03 2012 STRYKER EUROPEAN HOLDINGS III, LLC External fixator deformity correction systems and methods
10251705, Jun 02 2016 STRYKER EUROPEAN HOLDINGS III, LLC Software for use with deformity correction
10285734, Aug 11 2010 STRYKER EUROPEAN HOLDINGS III, LLC External fixator system
10376285, Aug 11 2010 STRYKER EUROPEAN HOLDINGS III, LLC External fixator system
10405888, Aug 23 2012 STRYKER EUROPEAN HOLDINGS III, LLC Bone transport external fixation frame
10470800, Mar 13 2013 DePuy Synthes Products, Inc. External bone fixation device
10603112, Jun 02 2016 STRYKER EUROPEAN HOLDINGS III, LLC Software for use with deformity correction
10610304, Feb 03 2012 STRYKER EUROPEAN HOLDINGS III, LLC Orthopedic treatment device co-display systems and methods
10835318, Aug 25 2016 DEPUY SYNTHES PRODUCTS, INC; Synthes GmbH Orthopedic fixation control and manipulation
10874433, Jan 30 2017 STRYKER EUROPEAN HOLDINGS III, LLC Strut attachments for external fixation frame
10881433, Feb 19 2013 Stryker European Operations Holdings LLC Software for use with deformity correction
10932857, May 19 2010 DePuy Synthes Products, Inc. Orthopedic fixation with imagery analysis
11020186, Jun 02 2016 STRYKER EUROPEAN HOLDINGS III, LLC Software for use with deformity correction
11083495, Apr 20 2016 STRYKER EUROPEAN HOLDINGS III, LLC Ring hole planning for external fixation frames
11090086, Aug 23 2012 STRYKER EUROPEAN HOLDINGS III, LLC Bone transport external fixation frame
11141196, Aug 11 2010 STRYKER EUROPEAN HOLDINGS III, LLC External fixator system
11259873, Feb 03 2012 STRYKER EUROPEAN HOLDINGS III, LLC External fixator deformity correction systems and methods
11304757, Mar 28 2019 Synthes GmbH Orthopedic fixation control and visualization
11334997, Apr 03 2020 Synthes GmbH Hinge detection for orthopedic fixation
11439436, Mar 18 2019 Synthes GmbH Orthopedic fixation strut swapping
11457965, Nov 12 2021 University of Utah Research Foundation Rotational guided growth devices, systems, and methods
11504160, Jun 14 2016 STRYKER EUROPEAN HOLDINGS III, LLC Gear mechanisms for fixation frame struts
11553965, Jun 02 2016 Holdings LLC Software for use with deformity correction
11648035, Mar 18 2019 Synthes GmbH Orthopedic fixation strut swapping
11653978, Feb 03 2012 Stryker European Operations Holdings LLC External fixator deformity correction systems and methods
11723690, Jan 30 2017 STRYKER EUROPEAN HOLDINGS III, LLC Strut attachments for external fixation frame
11744616, Aug 23 2012 Stryker European Operations Holdings LLC Bone transport external fixation frame
11771466, Apr 20 2016 Stryker European Operations Holdings LLC Ring hole planning for external fixation frames
11819246, Feb 19 2013 Stryker European Operations Holdings LLC Software for use with deformity correction
11893737, Apr 03 2020 Synthes GmbH Hinge detection for orthopedic fixation
11896313, May 19 2010 DePuy Synthes Products, Inc. Orthopedic fixation with imagery analysis
8205445, Jun 05 2007 GM Global Technology Operations LLC Tunable impedance load-bearing structures
8333766, Mar 10 2009 STRYKER EUROPEAN HOLDINGS III, LLC External fixation system
8448436, Jun 05 2007 GM Global Technology Operations LLC Tunable impedance load-bearing structures
8574232, Nov 13 2012 Texas Scottish Rite Hospital for Children External fixation connection rod for rapid and gradual adjustment
8641714, Feb 01 2008 STRYKER EUROPEAN HOLDINGS III, LLC Clamping pin
8834467, Aug 11 2010 STRYKER EUROPEAN HOLDINGS III, LLC External fixator system
8858555, Oct 05 2009 STRYKER EUROPEAN HOLDINGS III, LLC Dynamic external fixator and methods for use
8864750, Feb 18 2008 Texas Scottish Rite Hospital for Children Tool and method for external fixation strut adjustment
8864763, Mar 13 2013 Depuy Synthes Products, LLC External bone fixation device
8906020, Oct 05 2009 STRYKER EUROPEAN HOLDINGS III, LLC Dynamic external fixator and methods for use
8945128, Aug 11 2010 STRYKER EUROPEAN HOLDINGS III, LLC External fixator system
8951252, Apr 18 2008 STRYKER EUROPEAN HOLDINGS III, LLC External fixation system
9011438, Apr 18 2008 STRYKER EUROPEAN HOLDINGS III, LLC Radiolucent orthopedic fixation plate
9039706, Mar 13 2013 DEPUY SYNTHES PRODUCTS, INC External bone fixation device
9044271, Mar 10 2009 STRYKER EUROPEAN HOLDINGS III, LLC External fixation system
9078700, Feb 12 2008 Texas Scottish Rite Hospital for Children Fast adjust external fixation connection rod
9101398, Aug 23 2012 STRYKER EUROPEAN HOLDINGS III, LLC Bone transport external fixation frame
9155559, Feb 08 2008 Texas Scottish Rite Hospital for Children External fixator strut
9204937, Feb 19 2013 Stryker European Operations Holdings LLC Software for use with deformity correction
9220533, Aug 11 2010 STRYKER EUROPEAN HOLDINGS III, LLC External fixator system
9295493, Feb 05 2008 Texas Scottish Rite Hospital for Children External fixator ring
9351763, Oct 05 2009 STRYKER EUROPEAN HOLDINGS III, LLC Dynamic external fixator and methods for use
9381042, Nov 13 2012 Texas Scottish Rite Hospital for Children External fixation connection rod for rapid and gradual adjustment
9443302, Aug 20 2010 ORTHOFIX S R L Method and system for roentgenography-based modeling
9456849, Feb 12 2008 Texas Scottish Rite Hospital for Children Fast adjust external fixation connection rod
9524581, Feb 03 2012 STRYKER EUROPEAN HOLDINGS III, LLC Orthopedic treatment device co-display systems and methods
9642649, May 19 2010 DEPUY SYNTHES PRODUCTS, INC Orthopedic fixation with imagery analysis
9675382, Mar 13 2013 DEPUY SYNTHES PRODUCTS, INC External bone fixation device
9681892, Feb 08 2008 Texas Scottish Rite Hospital for Children External fixator strut
9717527, Aug 11 2010 STRYKER EUROPEAN HOLDINGS III, LLC External fixator system
9724129, Feb 19 2013 Stryker European Operations Holdings LLC Software for use with deformity correction
9730730, Aug 11 2010 STRYKER EUROPEAN HOLDINGS III, LLC External fixator system
9788861, Mar 13 2013 DePuy Synthes Products, Inc. External bone fixation device
9788908, Feb 03 2012 STRYKER EUROPEAN HOLDINGS III, LLC External fixator deformity correction systems and methods
9808289, Feb 05 2008 Texas Scottish Rite Hospital for Children External fixator ring
9820775, Aug 23 2012 STRYKER EUROPEAN HOLDINGS III, LLC Bone transport external fixation frame
9839445, Aug 11 2010 STRYKER EUROPEAN HOLDINGS III, LLC External fixator system
9895167, Apr 20 2016 STRYKER EUROPEAN HOLDINGS III, LLC Ring hole planning for external fixation frames
Patent Priority Assignee Title
1308799,
2055024,
2250417,
2391537,
2487989,
3176805,
3727610,
3941123, May 20 1975 Apparatus for joint movement restitution
3977397, Nov 27 1974 Surgical compression-distraction instrument
3985127, Jun 11 1975 Apparatus for surgical treatment of the knee joint
4033340, Dec 14 1973 Surgical compression-distraction instrument
4100919, Dec 08 1976 Tsentralny Nauchno-Issledovatelsky Institut Travmatologii I Ortopedii Apparatus for surgical treatment of bones and joints
4112935, Nov 03 1976 Apparatus for surgical treatment of scoliosis
4127119, Aug 09 1976 Fracture reducing and joint immobilizing apparatus
4308863, Oct 18 1979 Depuy Ace Medical Company External fixation device
4361144, Jun 02 1980 External compression frame for stabilizing unstable pelvic fractures
4365624, Jan 16 1979 Jaquet Orthopedie SA External bone-anchoring element
4482266, Oct 23 1981 Tokico Ltd. Ball joint
4483334, Apr 11 1983 External fixation device
4502473, Aug 06 1981 British Technology Group Limited Apparatus for external fixation of bone fractures
4541422, Dec 09 1981 Functional attachment system for osteosynthesis
4554915, Mar 08 1983 SMITH & NEPHEW RICHARDS, INC Bone fixation frame
4570625, Aug 06 1981 British Technology Group Limited Apparatus for external fixation of bone fractures
4615338, Sep 18 1985 KURGANSKY NAUCHNO-ISSLEDOVATELSKY INSTITUT EXPERIMENTALNOI I KLINICHESKOI ORTOPEDII I TRAVMATOLOGII Automatic compression-distraction apparatus
4620533, Sep 16 1985 HOWMEDICA OSTEONICS CORP External bone fixation apparatus
4624249, Dec 04 1984 Medicuba Orthopedic external fixing apparatus
4628922, Sep 28 1984 University College London Fracture reduction apparatus
4662365, Dec 03 1982 MECRON, MEDIZINISCHE PRODUKTE GMBH, NUNSDORFER RING 23-29, D-1000 BERLIN 48, WEST GERMANY Device for the external fixation of bone fragments
4768524, Feb 28 1986 Device for immobilizing a bone structure, especially intended for orthopedic use
4889111, Apr 02 1984 Bone growth stimulator
4928546, Aug 17 1988 Robotic devices
4973331, Mar 08 1989 BLUE LINE PARTNERS; EDWARDS, CHARLES, DR ; PATON, WILLIAM; STURGULEWSKI, ARLISS; WILSON, JOE AND CAROL; DRAPER, TIM Automatic compression-distraction-torsion method and apparatus
4988244, Sep 01 1989 Giddings & Lewis, LLC Six-axis machine tool
5028180, Sep 01 1989 Giddings & Lewis, LLC Six-axis machine tool
5062844, Sep 07 1990 Smith & Nephew, Inc Method and apparatus for the fixation of bone fractures, limb lengthening and the correction of deformities
5170790, Apr 06 1990 PROJECT TROJAN INTELLECTUAL PROPERTY ACQUISITION, LLC; AUSLO RESEARCH LLC Arm having an end movable in translation, and therapeutic treatment apparatus constituting an application thereof
5179525, May 01 1990 UNIVERSIYT OF FLORIDA RESEARCH FOUNDATION, INCORPORATED; University of Florida Research Foundation, Incorporated Method and apparatus for controlling geometrically simple parallel mechanisms with distinctive connections
5180380, Mar 08 1989 BLUE LINE PARTNERS; EDWARDS, CHARLES, DR ; PATON, WILLIAM; STURGULEWSKI, ARLISS; WILSON, JOE AND CAROL; DRAPER, TIM Automatic compression-distraction-torsion method and apparatus
5209750, Oct 12 1990 Compagnie Generale De Materiel Orthopedique External holding and reducing brace for bone fractures
5259710, Aug 26 1991 INGERSOLL MACHINE TOOLS, INC ; CAMOZZI PNEUMATICS, INC Octahedral machine tool frame
5275598, Oct 09 1991 Quasi-isotropic apparatus and method of fabricating the apparatus
5354158, Aug 28 1990 Kearney & Trecker Corporation Six axis machine tool
5372597, May 12 1993 SMITH & NEPHEW RICHARDS, INC Supination-pronation device
5388935, Aug 03 1993 GIDDINGS & LEWIS, INC Six axis machine tool
5405347, Feb 12 1993 TRAUMAMARK, LLC Adjustable connector for external fixation rods
5461515, Jul 07 1992 Exelis, Inc Assembly defining a tetrahedral geometry for mounting an optical element
5466085, Sep 01 1989 Giddings & Lewis, LLC Gimbal assembly for six axis machine tool
5490784, Oct 29 1993 Virtual reality system with enhanced sensory apparatus
5702389, Mar 01 1995 Smith & Nephew Richards, Inc. Orthopaedic fixation device
5728095, Mar 01 1995 Smith & Nephew, Inc Method of using an orthopaedic fixation device
5776132, Dec 26 1996 Hospital for Special Surgery External fixation assembly
5797908, Feb 04 1997 TRAUMAMARK, LLC External fixator assembly and clamp therefor
5971984, Mar 01 1995 Smith & Nephew, Inc Method of using an orthopaedic fixation device
6030386, Aug 10 1998 Smith & Nephew, Inc Six axis external fixator strut
DE2546046,
DE295031476,
DE295144111,
EP589565,
FR2576774,
FR2756025,
GB108119,
GB2077847,
SU1255118,
SU1519673,
SU820813,
WO9106253,
WO9217313,
WO9626678,
///
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Nov 05 1998TAYLOR, HAROLD SSmith & Nephew, IncASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0227970276 pdf
Apr 05 2001Smith & Nephew, Inc.(assignment on the face of the patent)
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