2953 Effect of Fiber Penetration into Veneer Region of Bi-Layer Beams
S.R. DYER1, L.V.J. LASSILA2, and P.K. VALLITTU2, 1Oregon Health & Science University, Portland, USA, 2University of Turku, Institute of Dentistry, Finland

Objective: To test fiber reinforced composite (FRC) substructure arrangements within a bi-layer beam on the load to initial (IF) and final failure (FF) in a mode II delamination test. Methods: Three groups of FRC and particulate reinforced composite (PRC) were tested: PE (Ultra high molecular weight polyethylene ribbon (Connect) and BelleGlass, Kerr), W (woven E-glass (Vectris Frame) and Targis, Ivoclar), and U (unidirectional R-glass (Vectris Pontic) and Targis, Ivoclar).  Twelve specimens were fabricated by placing an FRC layer into 25 x 6 x 0.75 mm3 mold.  PRC (10mm x 0.75mm) was added to the specimen center. The FRC was placed into unpolymerized PRC layer at 3 depths to the veneer surface: 0%, 50%, or 100%. After light-polymerization, the specimens were standardized and measured by digital caliper, then stored 1 week in 37oC water.  Four specimens were randomly selected for sectioning/pre-test evaluation.  The remaining 8 specimen (=n) were loaded in a static 4-point bend test (20mm upper/ 10mm lowers spans) veneer side down until failure (recording IF and FF).  A fracture ratio (FR) was developed (IF/FF x 100). Results: Means and standard deviations (SD) were calculated (within fiber groups, same letter are not statistically different: ANOVA, Tukey post hoc, p< 0.05). Conclusion: Glass fiber positions with 50% penetration into the PRC significantly increased the load to IF.

PE 0%

PE 50%

PE 100%

W 0%

W 50%

W 100%

U 0%

U 50%

U 100%

IF (SD) in N

13.1 (1.5)a

12.3 (2.7)a

9.0 (3.1)

20.3 (2.5)d

29.3 (8.8)e

27.8 (8.0)d,e

47.6 (6.6)h

60.7 (13)

40.8 (8.8)h

FF (SD) in N

39.0 (10)y

37.6 (5.4)y,z

29.7 (3.7)z

60.4 (8.4)t

62.0 (19)t

41.4 (14)

214 (40)w

188 (35)w

176 (35)w

FR (IF/FF)100

35.1 (8.3)l

33.1

(7.4)l

30 (8.9)l

34.4

(7.1)m

52.2 (26)m,n

71.1 (24)n

22.9 (5.5) p

33.5 (9.7)p

24.2

(8.0)p

 

 

 

 

 

 

 

Seq #315 - CAD/CAM and Fiber Composites
8:00 AM-9:30 AM, Saturday, 13 March 2004 Hawaii Convention Center 321-B

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