Dental and Medical Problems

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Dental and Medical Problems

2023, vol. 60, nr 4, October-December, p. 551–557

doi: 10.17219/dmp/153060

Publication type: original article

Language: English

License: Creative Commons Attribution 3.0 Unported (CC BY 3.0)

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Tonin BSH, Peixoto RF, Fu J, De Mattos MdGC, Macedo AP. Influence of the frameworks of implant-supported prostheses and implant connections on stress distribution. Dent Med Probl. 2023;60(4):551–557. doi:10.17219/dmp/153060

Influence of the frameworks of implant-supported prostheses and implant connections on stress distribution

Bruna Santos Honório Tonin1,B,C,D, Raniel Fernandes Peixoto2,A,B,C, Jing Fu3,C,E, Maria Da Gloria Chiarello De Mattos1,A, Ana Paula Macedo1,A,B,C,F

1 Department of Dental Materials and Prosthesis, School of Dentistry of Ribeirão Preto, University of São Paulo, Ribeirão Preto, Brazil

2 Department of Restorative Dentistry, Faculty of Pharmacy, Dentistry and Nursing, Federal University of Ceará, Fortaleza, Brazil

3 Department of Prosthodontics, the Affiliated Hospital of Qingdao University, China

Abstract

Background. The maintenance of marginal bone integrity around dental implants continues to be a clinical challenge. It is still unclear whether loading multiple implant-supported prostheses that have different implant connections influences bone resorption.

Objectives. The aim of this in vitro study was to compare stress distribution around residual edentulous ridges supported by external hexagon (EH) and Morse taper (MT) implants with screw-retained frameworks obtained with the use of different methods.

Material and methods. Three-element implant-supported prostheses with distal cantilevers were manufactured according to different techniques of obtaining the framework: LAS – framework sectioned and welded with a laser; TIG – framework sectioned and welded with tungsten inert gas (TIG); and CCS – framework obtained using a computer-aided design/computer-aided manufacturing (CAD/CAM) system. Occlusal and punctual loading (150 N) was applied to the cantilevers. In the photoelastic stress analysis, the fringe orders (n) were quanitified using the Tardy method, which calculates the maximum shear stress value (τ) at each selected point.

Results. High stress around the implants and tightening were observed in the TIG group, mainly in the crestal bone region for the EH and MT implant connections. The LAS and CCS frameworks exhibited lower stress for the MT connection under occlusal and punctual loading.

Conclusions. The comparative analysis of the models showed that the MT connection type associated with the laser-welded or CAD/CAM frameworks resulted in lower stress values in the crestal bone area, suggesting the preservation of bone tissue in this region.

Keywords: CAD/CAM, dental prosthesis, dental stress analysis, dental implant

Introduction

Residual edentulous ridges may need augmentation procedures before or during implant placement. Some methods are associated with additional surgical intervention, cost, surgical time, and morbidity.1 Another alternative is rehabilitation with an implant-supported prosthesis with a cantilever. All the force applied in the posterior region of the cantilever is transmitted to the implants, and consequently to the adjacent bone, which causes some concerns regarding stress distribution.2 Previous studies compared different implant systems in terms of stress distribution with regard to the bone.3, 4 However, these stu­dies used only one element or multiple elements splinted to implant-retained restorations without a cantilever. Thus, research is still required to make this method safer.

To minimize distortion in the framework, and conse­quently reduce the stress transmitted to the implant-supported system, it is possible to section and weld one-piece frameworks obtained by conventional casting.5 Different welding techniques can be applied, such as conventional welding, gas-torch brazing, laser welding, and tungsten inert gas (TIG) welding. The TIG method has been associated with good flexural strength, and even with the resistance and adaptation values superior to laser welding for different metal alloys.6, 7 Laser welding has been introduced to dental laboratory procedures as an alternative method to soldering, brazing or TIG welding.8 Yttrium aluminum garnet (YAG) doped with neodymium (Nd) crystals is used to emit laser beams (the Nd:YAG laser) to weld dental alloys.9 As the laser energy can be concentrated on a small area, minimal heating or oxidation effects occur in the region surrounding the welded spot; however, this method presents variable resistance results.10

Computer-aided design/computer-aided manufacturing (CAD/CAM) can also be used to fabricate implant-supported frameworks.11, 12 This technique has provided significant improvement in the marginal adaption of frameworks,13 and may result in better stress distribution as compared to frameworks manufactured using traditional laboratory procedures. Although the CAD/CAM technology eliminates several steps, it introduces others, such as scanning, intricate software utilization, design, and machining, which also depend on the experience of the operator and the equipment used.14

With regard to the geometry of implant connections, some studies have reported that the Morse taper (MT) connections provide joint stability and higher frictional resistance against rotational and lateral movements under vertical loading than external connections.15 The external hexagon (EH) connections have been reported to be advantageous in terms of their anti-rotational mechanism and compatibility with different implant systems.16

To evaluate biomechanical behavior, photoelasticity has been used. This stress analysis enables the visualization and quantification of stress distribution in its entirety. It shows how polarized light is affected when passing through a plastic model under experimental loading. The method reveals full-field stress patterns.17 Photoelastic models have been successfully used to explain differences between various kinds of prosthetic treatment, revealing stress behavior of implant-supported prostheses in the peri-implant bone tissue, and to assess the impact of compromised conditions through comparative stress-related outcome analyses.17, 18, 19, 20 In addition to stress location, its intensity and concentration can be interpreted on the basis of the color, number and closeness of the emerging fringes.17, 21

The purpose of the present study was to use the photoelastic method to analyze stress distribution around implants supporting a cantilever fixed partial denture (FPD) under both occlusal and punctual loading conditions. The effects of different implant–abutment connections and frameworks, whole and welded, were compared.

Material and methods

Six photoelastic models were produced from the master polycarbonate models (rectangular block format: 50 mm × 30 mm × 15 mm; 4 mm of height was removed at the posterior region of the model to simulate the resorption of the posterior region of the mandible). The implants (Ø 3.75 mm × 9 mm EH (Ti Titamax; Neodent, Curitiba, Brazil) and Ø 3.75 mm × 9 mm MT (CM Titamax; Neodent)) and a resin tooth were positioned into the models. The implants corresponded to the second premolar and the first molar, and a resin tooth replica (Protemp 4; 3M ESPE, St. Paul, USA) replaced the first premolar. The distance between the center of the tooth and the center of the implant was 7.5 mm; the distance between the centers of the implants was 9.5 mm, according to the odontometric parameters described in previous studies.21, 22, 23 The root of the resin tooth received a 0.3-milli­meter layer of polyether (Impregum Soft; 3M ESPE) to simulate the periodontal ligament (PDL).24

A 3-unit implant-retained prosthesis with a distal cantilever was waxed up on the copings of screw-retained abutments (EH and MT abutments, cobalt-chromium (Co-Cr) copings; Neodent). The prosthesis was duplicated (silicone azul; Polglass, Ribeirão Preto, Brazil) to standardize the specimens in all groups. To obtain frameworks, the waxed 3-unit implant-retained prostheses were reduced by 2 mm, and another silicone mold was made. For the fabrication of CAD/CAM frameworks, the previously reduced frameworks were scanned using a D700 scanner (3Shape, Copenhagen, Denmark) and machined in Co-Cr using a milling machine (Ceramill Motion 2; Amman Girrbach, Koblach, Austria).

The frameworks were fabricated using a Co-Cr alloy (Fit Cast Cobalto; Talmax, Curitiba, Brazil) and separated into the following 3 groups: LAS – conventional cast framework sectioned and welded with a laser; TIG – conventional cast framework sectioned and welded with TIG; and CCS – framework produced with the CAD/CAM system. Using a 0.5-millimeter-thick, sharp stainless steel blade, the LAS and TIG frameworks were sectioned to be welded after conventional casting. The spruing, investing, burnout, and casting techniques were standardized. Subsequently, the frameworks were carefully removed by using glass microspheres (Polidental Indústria e Comércio, São Paulo, Brazil) of 100 µm granulation at a pressure of 60 lbf/in2. Small nodules were removed with high-speed rotary tungsten carbide burs under constant cooling.

The laser welding machine (desktop Compact; Dentaurum, Nova Lianka, São Paulo, Brazil) was set at 310 V and the pulse was fixed at 9 ms. Laser welding was performed at diametrically opposed points until the entire diameter of the section in the framework received the welding points to minimize distortion. Tungsten inert gas welding was performed using a plasma welding machine (NTY 60 K; Kernit, Indaiatuba, Brazil) according to the adapted methodology.25 In an argon gas environment, the tungsten (W) electrode was positioned 3–6 mm from the infrastructure, with the settings of 4 A and 0.15 s. Similarly to laser welding, TIG welding was executed at diametrically opposed points on the section of the framework.

All the steps of pressing the infrastructures with the IPS InLine PoM ceramic (Ivoclar Vivadent, Schaan, Liechtenstein) strictly followed the manufacturer’s recommendations.

Photoelastic stress analysis

The abutments were tightened to the implants, and the prosthesis frameworks were tightened on the abutments. Before each analysis, the models were heated to 50°C for 10 min to release the stress induced within the model. Subsequently, the models were cooled at approx. 23°C for 10 min and the absence of residual stresses was confirmed with a polariscope (FL 200; G.U.N.T. Garätebau, Hamburg, Germany).20 The cantilevers were subjected to a simulated occlusal axial load and a single-point load cell (both of 150 N).26

To perform the qualitative analysis, the polariscope was adjusted to the circular polarization mode. Stress intensity, represented by respective fringe orders (nnumber of fringes), and location were compared subjectively. A greater number of fringes indicated greater intensity of tension, and the closer the fringes were to each other, the greater the stress concentration was.27, 28 Interpretation was performed using the following scale: (1) low stress – 1 fringe or less; (2) moderate stress – between 2 and 3 fringes; or (3) high stress – more than 3 fringes.29

To perform the quantitative analysis, the polariscope was adjusted to the circular mode. Stress distribution with regard to isochromatic fringes at 6 points of interest (3 in the cervical region of the implants, near the simulated crestal bone, 1 in the apical region of each implant, and 1 in the apical region of the first premolar) (Figure 1) was analyzed using the photoelastic model. The isochromatic fringe values (n) for each of the reading points were measured using the Tardy method of compensation.30 The individual shear stress value (τ) for each point was determined using the stress-optic law, as follows (Equation 1):

where:

τ – maximum shear stress [kPa];

n – value of the fringe order at the analyzed point; and

b – thickness of the model [mm] (15 mm).

The optical constant of the photoelastic material Kσ = 3.56 was predetermined in a calibration procedure.29

Results

The photoelastic stress analysis, as showed in Figure 2 and corroborated by the shear stress values in Table 1, indicated varying stress levels across different scenarios. In the LAS-EH configuration, the observed stress levels were as follows: (1) high between the implants (P2; fringe order 4); (2) moderate between the implant and the tooth (P3, fringe order 2); and (3) moderate in the apical region of the implants (P4 and P5; fringe order 3). The TIG-EH and CCS-EH configurations demonstrated low to moderate stress withfringe order of 1 at the dental apex (P6) andfringe order of 2 in the crestal bone re­gion below the cantilever (P1). With regard to the MT connection, TIG-MT exhibited the following stress levels: (1) moderate in the region below the cantilever (P1; fringe order 3); (2) moderate between the implants, and between the implant and the tooth (P2 and P3; fringe or­der 3); and (3) high in the apical region of the implants (P4 and P5, fringe order 4). The LAS-MT and CCS-MT con­figurations showed fringe order fringe order 1 below the cantilever (P1) and between the implants (P2), and fringe orders 3 and 2 at the apical region of the implants (P4 and P5, respectively).

Regarding the differences in stress distribution between the implant connections under occlusal loading, the LAS-EH configuration exhibitedgreater number of fringes between the implants and in the apical regions of the implants. The TIG-MT framework showed the highest stress below the cantilever, in the apical region of the implants, and between the implant and the tooth. Comparing the frameworks fabricated using the CAD/ CAM system, the EH system presented higher stress at all points (except for P1 and P4) as compared to the MT connection.

Underpunctual load of 150 N applied to the cantilever, the photoelastic stress analysis indicated varied stress concentration for the EH and MT implant connections (Figure 3, Table 2). For the EH connection, the LAS group exhibitedfringe order of 4 at P4, corresponding tomaximum shear stress value of 643.8 kPa. The TIG group showedfringe order of 3 at points P1, P4, and P5, with notably high shear stress values at P1 (660.7 kPa) and P4 (589.8 kPa). The CCS group demonstrated similar stress patterns, withfringe order of 3 at P4 andmaximum shear stress value of 637.1 kPa. Other points under the EH connection mostly showedfringe order of 2, indicating moderate stress levels. For the MT connection, the LAS group presentedhigh fringe order of 4 at point P4, where the shear stress reached 704.9 kPa. Tungsten inert gas welding on the MT connection produced the highest shear stress across most points, with the peak at P4 (788.4 kPa), followed by P1 (666.9 kPa) and P5 (600.3 kPa). The CCS-MT configuration also showed high stress at P4, withfringe order of 3 andshear stress value of 483.4 kPa. Fringe order 2 was observed in the remaining points for all MT groups, suggesting lower stress concentration.

The comparative analysis of the implant connections revealed that the EH system generally exhibited higher shear stress values than the MT connection in certain points within the LAS and CCS groups. Specifically, the LAS-EH configuration showed higher stress at points P1 (354.0 kPa), P3 (401.3 kPa), P5 (432.6 kPa), and P6 (45.6 kPa), while the CCS-EH configuration demonstrated higher values at P1 (419.1 kPa), P3 (316.0 kPa), P4 (637.1 kPa), and P6 (138.6 kPa).

Discussion

Under occlusal loading, laser welding exhibited the highest stress pattern at the apices of the EH implants, between the implants, and between the implant and the tooth. However, TIG welding presented the highest shear stress in critical areas, such as the crestal bone, for both implant connections. The lost-wax fabrication process of frameworks is related to a high coefficient of thermal expansion of the wax, and its dimensional stability is subject to air temperature; however, a combination of distortions in different dimensions can cause a significant misfit at the prosthesis–abutment interface. Consequently, it may result in the overload of the bone.31 Although the distortions are difficult to eliminate, they can be minimized by sectioning and welding frameworks.

Laser welding promotes significant mechanical longe­vity of the framework due to its high precision level, bio­compatibility and minimal side effects. Furthermore, this technique yields a framework with reasonable hardness and minimizes the heat-affected zone, which is crucial for maintaining the integrity of the material.32 De Castro et al. evaluated stress distribution in Co-Cr frameworks with the use of laser welding and TIG welding, and concluded that the stress generated around the implants was similar for both techniques.25 In the present study, although laser welding presented high stress between the implants, TIG welding showed the highest shear stress values in the crestal bone region at 3 key points, as well as in the apical region of the implants for both the EH and MT connections. This was consistent across all measured points, except for P3 and P4 in the TIG-EH configuration, where the stress was not the highest as compared to other groups, as detailed in Table 2.

In the case of cantilevers, careful planning is necessary to preserve the bone around the implants, mainly because of the distribution of the stress transmitted to the marginal area of the bone during chewing. The concentration of high-intensity fringes at the distal implant under punctual loading on the cantilever, as exhibited by TIG welding in both implant systems, increases the possi­bility of crestal bone resorption. Some studies have reported an increase in the flexural strength demonstrated by TIG-welded frameworks.6, 7 Several factors may influence the mechanical strength. Tungsten inert gas welding correlates with resistance because of the welding penetration, consequently resulting in fewer pores, cracks and flaws; thus, high stress to the bone in the crestal bone area can be associated with the high mechanical strength provided by TIG welding.7

The study found that the frameworks fabricated using the CAD/CAM technique generally exhibited lower stress values under occlusal and punctual loading. However, this was not consistent across all cases. A detailed examination of Table 1 and Table 2 reveals exceptions, where the CAD/CAM frameworks did not result in the lowest stress values as compared to other techniques. Although the CAD/CAM method has improved the fit of frameworks, distortions can still be present when the procedures employed to apply the ceramic involve the lost-wax process followed by heat pressing. Some studies have reported the superiority of the CAD/CAM technique in terms of fit accuracy of implant-supported FDP as compared to the conventional cast frameworks.11, 13 However, these reports compared CAD/CAM with conventional casting, without taking into consideration the copings for the screw-retained abutments, as in the present study. The overcasting technique uses cylinders with pre-machined metal straps to avoid casting the cylinder base and to minimize distortions.18 This situation may explain the same stress pattern observed for the laser-welded and CAD/CAM frameworks for the MT implants under occlusal and punctual loading on the cantilever.

According to the results, the type of the implant–abutment connection influenced the distribution of stress to the bone. The MT system produced a lower number of fringes and lower shear stress values under both types of loading, except when the framework of the TIG group was tightened. However, a study by Goiato et al. showed a more stable inferface for internal connections due to the intimate contact between the internal part of the implant and the external part of the abutment,33 which favors load distribution.34 Moreover, the cited study did not use cop­ings for the screw-retained abutments, and only a punctual load was applied to the cantilever. Sousa et al. evaluated the EH and MT connections by using the finite element analysis (FEA), and proved that the MT connection significantly decreased the strain levels in the peri-implant bone.35 This result is in partial agreement with the findings of the present study, since the TIG group showed the highest shear stress values, especially for the MT connection, which can be attributed to the high flexural strength resulting from the welding penetration.

Limitations

The photoelastic stress analysis and other in vitro methods present certain limitations, and the results should be considered with caution when extrapolating them to clinical situations. These limitations relate to the different elasticity moduli of oral tissues, and the inability of solid, isotropic photoelastic models to differentiate between the cortical and cancellous bones.21, 36

Despite the differences, photoelasticity is regarded as a fairly accurate method for assessing stress patterns, as the fundamental stress concentration trends are typically consistent with those observed clinically.37

For a more comprehensive understanding, future research could explore three-dimensional (3D) photoelastic stress analysis. This advanced approach would accommodate the complexity of the oral environment more effectively by including shear stress as part of the loading conditions, thereby providing a simulation that would more representative of clinical situations.19

Conclusions

Within the limitations of this study, we conclude that the use of laser-welded and CAD/CAM frameworks with MT implants results in lower stress values in the crestal bone area. Although there was high stress associated with TIG welding on the MT system, the EH system exhibited more stress in other groups in comparison with the MT system.

Ethics approval and consent to participate

Not applicable.

Data availability

The datasets generated and/or analyzed during the current study are available from the corresponding author on reasonable request.

Consent for publication

Not applicable.

Tables


Table 1. Maximum shear stress values (τ) [kPa] for each point with regard to the external hexagon (EH) and Morse taper (MT) implants under occlusal loading

Point

EH

MT

LAS

TIG

CCS

LAS

TIG

CCS

P1

114.9

239.1

110.7

219.8

674.3

456.2

P2

207.9

249.3

304.9

238.9

297.5

186.0

P3

182.5

146.0

127.8

63.6

299.2

77.7

P4

538.4

414.9

401.5

861.9

790.0

429.7

P5

380.2

134.3

249.4

151.2

362.0

49.8

P6

112.5

202.3

132.3

41.3

52.1

58.7

P1 – below the cantilever; P2 – between the implants; P3 – between the implant and the tooth; P4, P5 – in the apical region of the implants; P6 – at the dental apex.
Table 2. Maximum shear stress values (τ) [kPa] for each point with regard to the external hexagon (EH) and Morse taper (MT) implants under punctual loading

Point

EH

MT

LAS

TIG

CCS

LAS

TIG

CCS

P1

354.0

660.7

419.1

176.8

666.9

392.5

P2

212.9

353.8

196.9

259.3

446.3

266.5

P3

401.3

151.3

316.0

148.8

315.7

100.0

P4

643.8

589.8

637.1

704.9

788.4

483.4

P5

432.6

539.9

335.4

322.3

600.3

358.7

P6

45.6

87.9

138.6

44.6

61.2

38.8

Equations


Equation 1

Figures


Fig. 1. Distance between the implants and the tooth, and points selected for the quantitative analysis
Fig. 2. Stress caused by the application of an occlusal load
LAS – conventional cast framework sectioned and welded with a laser;
TIG – conventional cast framework sectioned and welded with tungsten inert gas (TIG); CCS – framework produced with the computer-aided design/computer-aided manufacturing (CAD/CAM) system;
EH – external hexagon implant; MT – Morse taper implant.
Fig. 3. Stress caused by the application of a punctual load

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