| Literature DB >> 31547045 |
Hadas Heller1, Adi Arieli2, Ilan Beitlitum3, Raphael Pilo4, Shifra Levartovsky5.
Abstract
The static and dynamic load-bearing capacities and failure modes of zirconia crowns screwed to multi-unit abutments (MUAs) with and without a titanium base (T-base) were determined. Thirty-six monolithic zirconia crowns screwed to straight MUAs torqued to laboratory analogs (30 Ncm) were assigned to two groups (n = 18). In group A, the zirconia crowns were screwed directly to the MUAs; in group B, the zirconia crowns were cemented to the T-base and screwed to the MUAs. All specimens were aged in 100% humidity (37 °C) for one month and subjected to thermocycling (20,000 cycles). Afterwards, the specimens underwent static and dynamic loading tests following ISO 14801. The failure modes were evaluated by stereomicroscopy (20×). There was an unequivocally similar trend in the S-N plots of both specimen groups. The load at which the specimens survived 5,000,000 cycles was 250 N for both groups. Group A failed mainly within the metal, and zirconia failure occurred only at a high loading force. Group B exhibited failure within the metal mostly in conjunction with adhesive failure between the zirconia and T-base. Zirconia restoration screwed directly to an MUA is a viable option, but further studies with larger sample sizes are warranted.Entities:
Keywords: monolithic zirconia; multi-unit abutment; titanium base
Year: 2019 PMID: 31547045 PMCID: PMC6803877 DOI: 10.3390/ma12193056
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.623
Mean maximal load-bearing capacity (N) and 80% level for each experimental group.
| Specimen | Group A(N) | Group B(N) |
|---|---|---|
| 1 | 872 |
|
| 2 | 811 |
|
| 3 | 675 |
|
| Mean | 786 |
|
| 80% Level | 629 |
|
Group A—screwed restoration; Group B—screwed-cemented restoration; 80% Level—80% of the average static load compressive test result.
Fatigue test results for group A (screwed restoration).
| Specimen | Load (N) | No. of Cycles | Average No of Cycles | Failure Mode |
|---|---|---|---|---|
| 1 | 450 | 35,670 | - | Zirconia + metal (screw) |
| 2 | 450 | 209,543 | 80,545 | Metal (MUA + screw) Zirconia + metal (screw) |
| 3 | 450 | 176,422 | - | |
| 4 | 400 | 1,254,436 | - | Metal (MUA + screw) |
| 5 | 400 | 125,878 | 533,457 | Metal (MUA + screw) |
| 6 | 400 | 220,056 | - | Metal (MUA + screw) |
| 7 | 350 | 160,749 | - | Metal (MUA + screw) |
| 8 | 350 | 546,871 | 266,048 | Metal (MUA + screw) |
| 9 | 350 | 905,205 | - | Metal (MUA + screw) |
| 10 | 300 | 3,401,784 | - | Metal (MUA + screw) |
| 11 | 300 | 437,068 | 2,946,284 | Metal (MUA + screw) |
| 12 | 300 | 5,000,000 | - | Metal (MUA + screw) |
| 13 | 250 | 5,000,000 | - | No Failure |
| 14 | 250 | 5,000,000 | 5,000,000 | No Failure |
| 15 | 250 | 5,000,000 | - | No Failure |
With a maximum load of 250 N, three specimens completed five million cycles without fracturing; Load—maximum load applied in each cycle; Number of cycles—number of cycles before the test was interrupted; Average number of cycles- for particular load values; MUA—multi-unit abutment.
Fatigue test results for group B (screwed-cemented restoration).
| Specimen | Load (N) | No. of Cycles | Average No of Cycles | Failure Mode |
|---|---|---|---|---|
| 1 | 550 | 6607 | - | Adhesive + metal (screw) |
| 2 | 550 | 30,341 | 22,450 | Metal (screw) |
| 3 | 550 | 30,341 | - | |
| 4 | 450 | 99,751 | - | Adhesive + metal (MUA) |
| 5 | 450 | 178,367 | 158,818 | Metal (screw) |
| 6 | 450 | 198,337 | - | Adhesive + metal (MUA) |
| 7 | 350 | 2,950,685 | - | Adhesive + metal (screw) |
| 8 | 350 | 200,751 | 1,764,689 | Adhesive + metal (MUA) |
| 9 | 350 | 2,142,632 | - | Adhesive + metal (MUA) |
| 10 | 300 | 553,418 | - | Adhesive + metal (MUA) |
| 11 | 300 | 2,264,147 | 2,472,765 | Metal (screw) |
| 12 | 300 | 4,600,732 | - | Adhesive + metal (MUA |
| 13 | 250 | 5,000,000 | - | No Failure |
| 14 | 250 | 5,000,000 | 5,000,000 | No Failure |
| 15 | 250 | 5,000,000 | - | No Failure |
With a maximum load of 250 N, three specimens completed five million cycles without fracturing; Load—maximum load applied in each cycle; Number of cycles—number of cycles before the test was interrupted; Average number of cycles- for particular load values; MUA—multi-unit abutment.
Figure 1S-N curve. Chart showing the applied load as a function of the number of cycles. After the samples underwent five million cycles, the test was stopped. The horizontal and vertical lines are used as a guide for the eye.
Figure 2Specimen number seven in group A shows deformation and fracturing within the cone of the multi-unit abutment (MUA) under an applied load of 350 N. This mode of failure was predominant in group A.
Figure 3Specimen number one in group A shows fracturing of the zirconia concomitantly with bending of the restoration screw head under an applied load of 450 N. This failure was observed in group A at only high loading forces.
Figure 4Specimen number 10 in group B exhibits adhesive failure between the zirconia and T-base in addition to deformation and fracturing within the cone of the MUA under an applied load of 300 N. This mode of failure was predominant in group B.
Figure 5Components of the zirconia-abutment restorations. (a) Screwed restoration; (b) screwed-cemented restoration; (c) apical view of the screwed zirconia cap. Note the internal zirconia ledge for the support of the screw head.
Figure 6Test setup following ISO 14801:2016. (a) Schematic illustration of the test design: (1) loading device; (2) nominal bone level; (3) zirconia coping; (4) hemispherical loading member; (5) dental implant analog; and (6) metal specimen holder; (b) setup for the study.