| Literature DB >> 35744373 |
Oswaldo Erazo1, Judith Vergara-Figueroa1, Paulina Valenzuela1, William Gacitúa1,2.
Abstract
The influence of load on the cellulose microfibrils of single cells or thin wood foils is known. It can decrease the cellulose microfibril angles and, in turn, increase the stiffness. However, this modification of a piece of wood, which is made up of multiple cells, is unknown. The aim of this research was to study the effect of tensile creep on the longitudinal stiffness of radiata pine wood. The modulus of elasticity of each specimen was determined before and after being subjected to tensile creep. The samples were loaded at 1170 N and 1530 N for 20 min at 70 °C. The load was determined as a function of a percentage of the force at the proportional limit. The moduli of elasticity before and post-tensile creep showed no effect on the stiffness of wood at the macroscopic level, but neither were there damage to the cell structure. It can be assumed that there are changes at the microscopic level, but they are not enough to be reflected at the macro scale. It is also challenging to achieve the modifications that occur at the level of a single cell or in thin wood foils; however, the implications of this would be favorable for the development of stronger wood-based products.Entities:
Keywords: longitudinal tensile creep; mechanical properties; modulus of elasticity; radiata pine
Year: 2022 PMID: 35744373 PMCID: PMC9231006 DOI: 10.3390/ma15124314
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.748
Figure 1Diagram for obtaining the specimens in a strip: (A) sections in a wooden strip: tangential and radial; (B) dog bone specimens per section; (C) dimensions in millimeters (mm) of the dog bone specimen.
Figure 2Clip-on extensometer. Determination of the force at the proportional limit.
Figure 3Tensile creep test: (A) testing machine equipped with temperature chamber; (B) specimen during tensile creep test.
Moduli of elasticity of the specimens before (control) and post-tensile creep.
| Basic Density | |||||
|---|---|---|---|---|---|
| 0.39 g cm−3 | 0.43 g cm−3 | ||||
| Cutting Planes | Load | Modulus of Elasticity | CV | Modulus of Elasticity | CV |
| Tangential | Control | 10.93 ± 1.91 a | 17.52 | 11.06 ± 2.12 c | 19.13 |
| Load 1530 N | 10.95 ± 1.97 a | 17.99 | 10.94 ± 1.99 c | 18.22 | |
| Control | 10.87 ± 1.67 a | 15.33 | 11.40 ± 2.61 c | 22.87 | |
| Load 1170 N | 10.74 ± 1.66 a | 15.47 | 11.27 ± 2.47 c | 21.92 | |
| Radial | Control | 8.48 ± 1.94 b | 22.91 | 11.21 ± 1.35 c | 12.08 |
| Load 1530 N | 8.54 ± 1.87 b | 21.90 | 11.07 ± 1.31 c | 11.86 | |
| Control | 8.82 ± 1.94 b | 22.03 | 11.36 ± 1.31 c | 11.50 | |
| Load 1170 N | 8.76 ± 1.92 b | 21.88 | 11.29 ± 1.27 c | 11.26 | |
Values are presented as means ± standard deviation. Values followed by different superscript letters in the same column indicate significant differences (p < 0.05). CV% = coefficient of variation.
Figure 4Evolution of the pieces with a density of 0.39 g cm−3 subjected to tensile creep: Load 1530 N: (A) tangential; (B) radial. Load 1170 N: (C) tangential; (D) radial.
Figure 5Evolution of the pieces with a density of 0.43 g cm−3 subjected to tensile creep: Load 1530 N: (A) tangential; (B) radial. Load 1170 N: (C) tangential; (D) radial.
Figure 6SEM images of radiata pine wood samples: untreated (A) earlywood (EW); (B) latewood (LW). Samples subjected to tensile creep: (C) EW section of a piece loaded 1170 N; (D) LW section of a piece loaded 1170 N; (E) EW section of a piece loaded 1530 N; (F) LW section of a piece loaded 1530 N.