Endosseous dental implant loading fixture

Abstract

An apparatus for fatigue testing an article includes a base having a platform for receiving an article to be tested, a shaft extending toward said platform for applying a force to said article, a coupling assembly connected to said shaft, said coupling assembly comprising a joint that pivots about an axis, and flex pivots disposed to be aligned with said axis about which said joint pivots.

Claims

1. A method of fatigue testing an article, comprising: providing an apparatus for fatigue testing an article, the apparatus including (i) a base having a platform, (ii) a shaft extending toward the platform, (iii) a coupling assembly connected to the shaft, the coupling assembly including a first clevis, a second clevis, and pivot block, and (iv) flex pivots that pivotally couple said first clevis and said second clevis to said pivot block; positioning an article to be tested on the platform of the base of the apparatus; applying a force to the article with the shaft; and pivoting the shaft about a first axis defined by a first subset of said flex pivots and about a second axis defined by a second subset of said flex pivots.

2. The method of claim 1, comprising rigidly transmitting an axial force with the flex pivot.

3. The method of claim 1, wherein the article is a dental implant.

4. The method of claim 1, wherein the platform is positionable at various angles of loading to the article relative to the shaft.

5. The method of claim 4, comprising sliding the platform along a curved holder to vary an angle between the shaft and the article.

6. The method of claim 4, wherein a vector normal to a top surface of the platform defines a variable angle relative to a load axis defined by the shaft.

7. A method of fatigue testing an article, comprising: providing an apparatus for fatigue testing an article, the apparatus including (i) means for receiving an article to be tested, (ii) means for transmitting a compressive force to the article, and (iii) means for coupling the means for transmitting a compressive force to an actuator, the means for coupling including a first clevis, a second clevis, and pivot block and flex pivots that pivotally couple said first clevis and said second clevis to said pivot block; receiving the article to be tested on the apparatus; transmitting the compressive force to the article; and pivoting the means for coupling wherein the first clevis is pivoted about a first axis and the second clevis is pivoted about a second axis substantially orthogonal to the first axis.

Description

BRIEF DESCRIPTION OF THE FIGURES

(1) FIG. 1 shows a dental implant to be tested by a loading fixture;

(2) FIG. 2 shows an isometric view of a loading fixture for testing the dental implant shown in FIG. 1;

(3) FIG. 3 shows a dental implant to be tested using the loading fixture of FIG. 2;

(4) FIG. 4 shows the coupling assembly of the loading fixture of FIG. 2;

(5) FIG. 5 shows a cut-away view of a flex pivot to be used with the coupling assembly shown in FIG. 4; and

(6) FIG. 6 shows a hip implant to be tested by a loading fixture.

DETAILED DESCRIPTION

(7) Referring to FIG. 2, a loading fixture 20 for fatigue testing of a dental implant 12 features a base 22, a shaft 24, and a coupling assembly 26 that couples the shaft 24 to an actuator (not shown).

(8) The base 22 encloses various load sensors and features a platform 28 for receiving the dental implant 12 that is implanted into and protrudes from a top surface 30 thereof. This platform 28 engages a track 32 formed on a curved holder 34 such that the platform 28 can slide along the curved holder 34 along a range of angles. In doing so, a vector normal to the top surface 30 of the platform 28 defines a variable angle relative to a load axis defined by the shaft 24.

(9) At a distal end 36 of the shaft 24 is a contact face 38 that contacts the dental implant 12 and transmits a load from the shaft 24 to the implant 12.

(10) As shown in FIG. 3, a dental implant 40 typically has a hemispherical top surface 41 that receives repeated loading during a typical fatigue test. As a result, the force is concentrated on a small portion of the contact face 38. To avoid permanent deformation of the contact face 38 from repeated loading, it is useful to use a hard material for the contact face 38. Examples of such materials include, but are not limited to, hardened steel, diamond, and zirconia. Particularly useful materials have a hardness between 1000 Hv and 8000 Hv. Also useful for use on the contact face 38 are materials having a hardness between 1300 Hv and 8000 Hv.

(11) Referring now to FIG. 4, the coupling assembly 26 includes a first clevis 42 having first and second arms 44, 46 connected by a base 48. The distal ends of the first and second arms 44, 46 have through holes 49, 50 that are aligned with each other. The coupling assembly 26 also includes a second clevis 52 having first and second arms 54, 56 connected by a base 58, with through holes 60, 62 at the distal tips of the first and second arms 54, 56. As was the case in the first clevis 42, these through holes 60, 62 are also aligned with each other. The first and second devises 42, 52 are orthogonal to each other such that a line normal to the first and second arms 44, 46 of the first clevis 42 is orthogonal to a line normal to the first and second arms 54, 56 of the second clevis 52.

(12) The coupling assembly 26 also includes a pivot block 64 having a length and width chosen to fit between the first and second arms 44, 46 of the first clevis 42 and the first and second arms 54, 56 of the second clevis 52 respectively. A thickness of the pivot block 64 is chosen to accommodate recesses 66A-66D that are the same size and shape as the through-holes 48, 50, 60, 62 on the arms 44, 46, 54, 56 of the devises 42, 52. When assembled, these through-holes 49, 50, 60, 62 align with corresponding recesses 66A-66D in the pivot block 64. Four flex pivots 68A-68D pass through corresponding through-holes 49, 50, 60, 62 and are secured into corresponding recesses in the pivot block 64.

(13) A side of the pivot block 64 has a groove 67A for receiving a corresponding arm 46 of the first clevis 42. to accommodate one of the arms. A similar groove 67C is provided on an opposite side of the pivot block 64 to receive the opposite arm 44 of the first clevis 42. These grooves 67A, 67C cooperate to restrain the corresponding flex pivots 68A, 68C from rotating beyond their fatigue rated rotation angles as the first clevis 42 pivots about the pivot block 64. A similar pair of grooves 67B, 67D on the remaining two sides of the pivot block 64 cooperate to restrain the corresponding flex pivots 68B, 68D from rotating beyond their fatigue rated rotation angles as the second clevis 52 pivots about the pivot block 64.

(14) As a result, the shaft 24 can pivot about a first rotational axis defined by first and third flex pivots 68A, 68C and a second rotational axis defined by second and fourth flex pivots 68B, 68D. This enables the application of a force without any constraint to motion in a lateral direction.

(15) Referring now to FIG. 5, a typical flex pivot 68A includes two coaxial cylinders 70A, 70B adjacent to each other. A vertical web 72A extending across the diameter of the cylinders 70A, 70B joins them together. Horizontal webs 72B, 72C extend across the cylinders along a direction orthogonal to that of the vertical web 72A. The horizontal and vertical webs 72A, 72B, 72C thus cooperate to urge the cylinders 70A, 70B to remain collinear in response to any radial force and to provide a restoring force when the cylinders 70A, 70B are rotated relative to each other.

(16) Flex pivots 68A-68D as described herein are essentially frictionless devices that allow pivoting for limited angles. Such pivots 68A-68D do not require lubrication or maintenance and do not wear. As a result, such pivots 68A-68D do not cause fine metal dust or shavings to be formed during use.

(17) An additional advantage of such flex pivots 68A-68D is the elimination of backlash. When flex pivots 68A-68D are used, there is no slack to be taken up as is the case when, for example, a ball bearing is used. A flex pivot 68A-68D eliminates the small but finite clearance in a ball bearing. Eliminating this clearance also eliminates the noise that results from backlash. As a result, when an actuator applies a force, the shaft 24 immediately and quietly transmits that force to the implant 12.

(18) Preferably, the implant 12 experiences no lateral forces during testing. However, as the shaft 24 swings from side to side, at least some lateral force is inevitable. To minimize this lateral force, it is preferable to make the shaft 24 as long as possible.

(19) When a shaft 24 of length l experiences an excursion of distance d as a result of pivoting about an angle θ, the shaft 24 inevitably exerts a lateral force F.sub.lat, that is equal to the axial force F.sub.axial weighted by the tangent of that angle θ, i.e. F.sub.lat=F.sub.axial tan(θ). Since the angle θ is the arcsine of the ratio of the excursion distance d to the length l, for a fixed excursion d, the longer the shaft 24 the lower the lateral force will be.

(20) As described herein, the loading fixture 20 is used to test dental implants 12. However, the principles described herein are applicable to testing of any article subject to similar constraints.

(21) In particular, the loading fixture 20 described herein can be used in a variety of applications in which one wishes to perform fatigue testing of a cantilevered article that is anchored at a point at some distance from where a compressive load is to be applied. For example, FIG. 6 shows a hip implant 74 anchored through a mounting surface 16 on a base 22. This hip implant 74 is to be fatigue tested by repeated application of a load from a contact face 38. A loading fixture 20 as described above can be adapted to perform fatigue testing of the hip implant 12.

(22) Additional applications include testing of electronic components. For example, to test the integrity of solder joints connecting an integrated circuit to a circuit board, one might apply a loading force along a direction parallel to the circuit board. Or, in testing a composite material having an asymmetric distribution of fibers, it may be useful to apply a compressive force at some angle relative to the axis of the fibers to determine an extent to which bending or rotation may occur.