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00547 Maik Gehloff - Timber Design Society

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PERFORMANCE OF MOMENT RESISTING SELF-TAPPING<br />

SCREW ASSEMBLY UNDER REVERSE CYCLIC LOAD<br />

Maximilian Closen 1 , Frank Lam 2<br />

ABSTRACT: This paper evaluates the performance of a moment resisting self-tapping screw assembly with tension<br />

and compression plates as connecting members in a typical beam to column connection subjected to reverse cyclic<br />

loads. Throughout the test series two main connection failure modes were observed. Failure mode one shows significant<br />

wood crushing in combination with transverse shear failure in the column member with a generally slow load decrease<br />

and continuous rotation of the beam member. Failure mode two shows sudden failure caused by tension fracture of the<br />

self-tapping wood screws in the beam member. The results show that this connection exceeds the bending moment<br />

design capacity of the glulam material by a factor of 2 in positive direction and a factor of 1.9 in the negative direction.<br />

In general strong performance with very little capacity and stiffness degradation was observed.<br />

KEYWORDS: Stress/failure analysis, timber structures, full thread self-tapping screws<br />

1 INTRODUCTION 123<br />

<strong>Timber</strong> connections with stocky dowels or bolts are<br />

critical structural members that are generally prone to<br />

brittle failure. Brittle failure occurs due to the poor<br />

tensile perpendicular to grain and longitudinal shear<br />

strengths of wood. When not intended in the design these<br />

connections can fail prematurely when subjected to<br />

stresses other than shear. During seismic events<br />

connections are likely to experience additional stresses<br />

caused by bending moments that were not considered<br />

during the design. Furthermore [1], reports the issue of<br />

restrained shrinkage in connections with slotted-in steel<br />

plates that use dowels or bolts as connecting members as<br />

critical with a potential for wood splitting and significant<br />

connection capacity reductions.<br />

Past research [2], [3], [4] proposes reinforcements that<br />

effectively reduce the tendency of wood splitting<br />

perpendicular to the grain by using structural full thread<br />

self-tapping wood screws (STS). [5] reports outstanding<br />

performances of bolted timber moment connections with<br />

STS reinforcement’s perpendicular to the wood grain.<br />

The reinforcing effect of STS in wood is based on<br />

principals that are similar to rebar’s in concrete. The<br />

special thread shape with assymetrical-symetrical thread<br />

1 Maximilian Closen, Department of Wood Science, University<br />

of British Columbia, 2842 - 2424 Main Mall, Vancouver, BC,<br />

V6T 1Z4, Canada. Email: mclosen@interchange.ubc.ca<br />

2 Frank Lam, Department of Wood Science, University of<br />

British Columbia, 2424 Main Mall, Vancouver, BC, V6T 1Z4,<br />

Canada. Email: frank.lam@ubc.ca<br />

pitches firmly bounds to the wood fibre over multiple<br />

layers (Figure 1). The bite of the thread forms a stiff<br />

connection to the wood. As stiff structural elements<br />

typically attract loads; therefore, it can be assumed that<br />

the majority of occurring stresses perpendicular to the<br />

grain is transferred as a tensile stress along the screw<br />

axis. Since STS are hardened after rolling on the thread a<br />

high tensile strength is achieved. The combination of<br />

high tensile strength and threads that firmly bite into the<br />

wood fibre are an effective method of splitting<br />

reinforcement.<br />

Figure 1: Screw thread embedded in the wood<br />

Current research has intensely addressed the reinforcing<br />

potential and withdrawal capacities of STS in timber<br />

connections; however, the potential of these fasteners as<br />

primary connector has been neglected. Utilizing the<br />

previously described properties of these screws as<br />

primary fastener strong, reliable and cost efficient timber<br />

connections can be created. [6] reports the application of<br />

STS as primary fastener in rigid frame corners with


significant higher load bearing potential when compared<br />

to glued finger joints and dowels. The configuration of<br />

the STS for this joint type however requires modelling of<br />

internal stress flows using the principles of strut-and-tie<br />

systems. Because many engineers have limited access to<br />

appropriate high cost modelling software this promising<br />

approach may not be commonly applied in practice until<br />

design equations are derived.<br />

In this study an experimental investigation was<br />

conducted to evaluate the performance of a moment<br />

resisting STS assembly (see Figure 5). The capacity of<br />

the assembly primarily depends on the shear and<br />

withdrawal resistance of the STS which can according to<br />

[7], in most cases, conservatively be estimated in major<br />

Canadian species using the design equations presented in<br />

[8]. A total of ten specimens were subjected to reverse<br />

cyclic loading conditions. In the following the<br />

performance of the moment resisting STS assembly in<br />

terms of ultimate capacities, stiffness and ductility is<br />

presented. In addition, a detailed description of all<br />

observations made during testing is provided.<br />

compression plates (ZD-plates). To allow for<br />

construction tolerances, the housing was oversized by 2<br />

mm in depth and 4 mm in width. These tolerances<br />

proofed to be sufficient for the specimen assembly in the<br />

lab. Each ZD-plate received four 10 mm x 240 mm<br />

ASSY VG countersunk head screws driven-in at a<br />

±30°angle to the wood grain of the beam member (see<br />

Figure 4). Detailed information about strength<br />

parameters and characteristics of the ASSY VG screws<br />

such as minimum requirements on the raw wire material,<br />

yield moment and tensile strength are summarized in [9]<br />

with links to proposed design equations in [8] and [10].<br />

In [11] a proposed design approach which estimates the<br />

capacity of connections with ZD-plates can be found.<br />

2 MATERIALS AND METHOD<br />

All specimens for this test series were cut from the<br />

centre lamellas of 130 mm x 912 mm Canadian Douglas<br />

fir glulam of stress grade 20f-E. As a typical example for<br />

the investigated connection a beam to column or column<br />

base connection can be assumed. Both connection<br />

application examples are typically needed in timber<br />

moment frames or simply as a column base-fixture.<br />

A custom made steel shoe assembly (see Figure 2) using<br />

9.5 mm thick steel plates was welded to fit the 130 mm x<br />

304 mm vertical beam member. On each side of the<br />

shoe, steel brackets were welded to the vertical steel<br />

plates for additional stiffening. To connect the vertical<br />

steel plates a 200 mm x 304 mm bracing-steel plate was<br />

welded in between. To be able to fit the beam member<br />

into the steel shoe a 12 mm wide and 220 mm deep slot<br />

needed to be cut into the lower beam end. Bearing of the<br />

beam member on the bottom steel plate and the bracing<br />

steel plate during load application was avoided by<br />

providing a 20 mm gap by simply slotting the beam to a<br />

depth of 220 mm. A second 9.5 mm thick bottom steel<br />

plate was fastened to the horizontal column member<br />

using 10 mm x 240 mm ASSY VG screws. A total of<br />

twelve 12.5 mm Grade 5 bolts were used to connect the<br />

steel shoe to the bottom steel plate through 13 pre-drilled<br />

holes with 12.5 mm receiver nuts welded on the bottom.<br />

Each bolt and nut was equipped with a 35 mm washer<br />

and tightened to a pre-set torque of 200 Nm. All timber<br />

members were fabricated using the Hundegger K2 5-axis<br />

fully automated joinery machine that was available at the<br />

Centre of Advanced Wood processing at the University<br />

of British Columbia (UBC). The previously mentioned<br />

12 mm x 220 mm slot in the beam member was cut using<br />

the Hundegger K2 circular saw. The required 40 mm x<br />

25 mm round housing for the receiver nut and washer at<br />

the column member was milled using a 25 mm finger<br />

mill. The 25 mm mill was also used to mill the column<br />

member housing for the 27 mm x 86 mm tension and<br />

Figure 2: Custom steel shoe and bottom steel plate<br />

(some parts were removed from drawing for clarity)<br />

(all measures in mm)<br />

Moisture content measurements with a resistance<br />

moisture meter at all specimen ranged between10.3 %<br />

and 11.8 % prior to assembly.<br />

To reduce the impact of wood crushing on data<br />

recordings at the location of the horizontal tie downs five<br />

10 mm x 240 mm ASSY VG screws were driven-in<br />

perpendicular to the grain (see Figure 3). The tie down<br />

steel pipe was now bearing on the screw head preventing


the wood from crushing under large loads. Because large<br />

loads and heavy deformations were expected on the steel<br />

shoe they were replaced after each test.<br />

cycle was selected with a deformation of 0.05∆ followed<br />

by a primary cycle of 0.075∆. This sequence progresses<br />

up to 2.0∆.<br />

Figure 3: Typical bearing reinforcement<br />

Figure 5: Test set-up<br />

The horizontal force component applied at the top of the<br />

beam member was recalculated using the displacement<br />

recording of a linear position transducer mounted<br />

vertically under the actuator (see Figure 6). Furthermore<br />

two cable extension position transducers were attached<br />

to the beam member in two different heights. These<br />

recordings were used to calculate the horizontal<br />

movement of the member from which moment rotation<br />

plots can be derived. A multi-purpose test system<br />

controlled the single ended MTS actuator with 250 mm<br />

stroke in positive and negative direction during load<br />

application.<br />

Figure 4: ZD-plate specifications from SWG-Production<br />

(all measures in mm)<br />

The entire research project was conducted at the UBC<br />

<strong>Timber</strong> Engineering and Applied Mechanics (TEAM)<br />

test facility. An illustration of the general test setup is<br />

shown in Figure 5. Ten specimens were subjected to<br />

displacement controlled reverse cyclic loading according<br />

the test procedure developed by [12]. This protocol<br />

consists of initiation cycles, trailing cycles and primary<br />

cycles with equal positive and negative amplitudes. The<br />

initiation cycles at the beginning serve to check the test<br />

equipment and the load deformation response. Primary<br />

cycles mark the beginning of a new displacement phase<br />

and are followed by trailing cycles with 75% of the<br />

amplitude of the respective primary cycle of each phase.<br />

The loading sequence was calibrated to the average<br />

reference deformation ∆ ultimate = 3° which was obtained<br />

from two monotonic tests with a constant loading rate of<br />

16 mm per minute. To account for variations between<br />

monotonic and cyclic testing and damage accumulation<br />

the suggested deformation ∆ =0.6∆ ultimate was applied to<br />

determine the final loading procedure. The first initiation<br />

3 RESULTS AND DISCUSSION<br />

The recorded loads, displacements and geometric data<br />

were used to derive moment rotation plots. A straight<br />

line segment connecting the point of 0.4M max with the<br />

origin of the moment rotation curve was used to define<br />

the initial connection stiffness. Where applicable, a yield<br />

moment derived from the point of intersection of the<br />

initial stiffness line and a tangent to the moment rotation<br />

curve having 1/6 of the slope of the initial stiffness line<br />

was calculated. In specimen with a steep load drop after<br />

the maximum moment was reached no yield moment<br />

was derived.<br />

The moment resistance of the assembly was calculated at<br />

the centre of rotation of the steel shoe.


Figure 6: General test layout and testing equipment (all measures in mm)<br />

Therefore, the horizontal force component was<br />

multiplied with the respective corrected distance (C in<br />

Figure 6) to the centre of rotation. Respective rotations<br />

of the beam member were derived from the geometric<br />

measurements of points B, D and E in Figure 6. The STS<br />

assembly with tension and compression plates shows<br />

high moment capacities with small rotations throughout<br />

the entire test series. Because of the layout of the steel<br />

shoe with a large number of bolts and bracings a tension<br />

fracture failure of the screws was promoted. Mostly this<br />

tension fracture resulted in brittle connection failures at<br />

small rotations of the beam member. Due to the high<br />

horizontal forces that the connection resisted during<br />

testing, compression failures in the beam member at the<br />

point of load application were observed. As a result up<br />

and down shifting of the load application fixture started<br />

to occur in progressed cycles (Figure 7). Compression<br />

failures of the wood were also observed on the column<br />

member at the location of the tie down steel pipes. At<br />

this location 16 mm steel plates and 10 mm x 240 mm<br />

full thread screws were applied to resist the expected<br />

high compression stresses. Three specimens did however<br />

fail regardless of the reinforcement and enlarged bearing<br />

area in a failure combination of compression<br />

perpendicular to grain and transverse shear (Figure 7).<br />

Furthermore, the intense crushing and splitting of the<br />

column member caused gaps to develop between the<br />

concrete strong floor and the bottom of the column. At<br />

maximum load these gaps measured approximately 15<br />

mm to 20 mm in positive and negative direction. Finally<br />

this resulted in higher rotations of respective specimens<br />

(see Figure 8). The intended 20 mm gap between the<br />

bottom of the beam member and the steel shoe proved to<br />

be sufficient throughout the test series. No bearing of the<br />

beam member on the steel shoe in either positive or<br />

negative direction with potential for increasing the<br />

moment resistance was observed.<br />

Figure 7: Typical wood crushing at point of load<br />

application (beam member) and compression -<br />

transverse shear failure (column member)<br />

Figure 8: Developed gap due to intense wood crushing<br />

and transverse shear failure at bottom of column member


The M16 (10.9) bolts used to connect the steel shoe to<br />

the ZD-plates of the beam member showed signs of<br />

heavy local stresses on the thread shortly under the hexhead.<br />

Up and down movement of the bolts was observed<br />

throughout all tests in progressed cycles. Heavy bending<br />

of the short, stocky bolts was found in three tests after<br />

the specimen were disassembled (see Figure 9). In these<br />

tests withdrawal resistance and push out failure of the<br />

full thread screws on one side of the beam member<br />

occurred and a gap between the ZD-plate bottom and the<br />

wood was formed. This gap caused an increased bending<br />

stress on the screws forcing them to yield therefore<br />

reducing the connection stiffness and capacity. Typically<br />

the combination of high tensile stresses and screw<br />

bending causes brittle fractures in hardened fasteners.<br />

In [11] failure of the thread inside the ZD-plates and<br />

failure at the bolt thread is reported. In addition [11]<br />

reports bending of the ZD-plates under heavy loads. This<br />

observation cannot be confirmed. One may assume that<br />

the shorter ZD-plates (86 mm length) used for tests in<br />

this project compared to the 100 mm used in [11]<br />

provide higher stiffness’s and therefore larger bending<br />

strength.<br />

As it can be seen in Figure 10 the M16 bolts were<br />

pushed out (away from the steel plate surface) in a way<br />

that no bearing of the bolt head on the steel plate was<br />

prevented. The cab formed ranged between<br />

approximately 2 mm and 4 mm. In general the largest<br />

gap formed at the top bolt with decreasing gap size<br />

toward the bottom of the beam member. A possible<br />

reason for the loosening of the bolts may be the large<br />

number of cycles that the specimen was subjected to and<br />

the small vibrations that were caused by the friction<br />

between the steel plate and the wood.<br />

Table 1 and Table 2 summarize the results for the ten<br />

tests which were derived from the moment-rotation<br />

relationships and the geometric data recordings as<br />

outlined in previous chapters. In Figure 11 a typical<br />

moment-rotation plot from specimens with significant<br />

wood crushing and transverse shear failure in the column<br />

member (observed in three out of ten tests) is shown. As<br />

a result of wood crushing and transverse shear failure no<br />

sudden load drops as seen in Figure 12 in either cycle<br />

can be seen. A load drop of approximately 20% of the<br />

recorded maximum load occurred in the positive cycle.<br />

After specimen disassembly it was found that this load<br />

drop was caused by the fracture of one tension screw in<br />

the top ZD-plate. The remaining screws on this side of<br />

the specimen were still functioning to carry loads and<br />

showed only little signs of high stresses with regard to<br />

screw bending and screw withdrawal. In all tests the<br />

failure of the connection initiated in the top ZD-plate and<br />

then progressed downward toward the column member.<br />

Figure 11: Typical Moment rotation plot derived from<br />

specimen Mc-10 with significant wood crushing and<br />

transverse shear failure at the column member in the<br />

positive and negative cycle.<br />

Figure 9: Bolt bending<br />

Figure 12: Typical Moment rotation plot derived from<br />

specimen Mc-4 with wood crushing at the column<br />

member in the positive cycle and tension fracture failure<br />

of screws with a related steep load drop in negative<br />

cycle.<br />

Figure 10: Bolt push-out


Beside a fracture failure of the screws in tension a<br />

withdrawal-push-out failure of the compression screws<br />

was observed mostly in the top ZD-plates (see Figure<br />

13). A significant visible failure on the ZD-plate itself<br />

was not found however slight indentations at the lid<br />

caused by the head of the compression screw were found<br />

throughout the entire test series. In addition, significant<br />

bending of the compression screws indicating high shear<br />

stresses at the interface between the ZD-plate and the<br />

wood member occurred. In general little signs of high<br />

stresses were observed at the bottom ZD-plate<br />

Figure 13: Observed withdrawal-push out failure (top left) and disassembled ZD-plate with compression screw bending<br />

and fractured tension screws after testing (top right). Screw withdrawal in column member (bottom left).Tension fracture<br />

of 12.5 mm bolt and steel plate yielding (bottom right).<br />

Beside the failure modes of the tension and compression<br />

screws in the beam member withdrawal failure of the<br />

screws driven into the column member also occurred.<br />

Along with the withdrawal of the screws tension splitting<br />

perpendicular to the grain at the location of the screws<br />

tip was observed. It is assumed that large tensile stresses<br />

were transferred through the screw shaft resulting in high<br />

stress concentrations at the screw tip. These stress<br />

concentrations finally cause wood splitting perpendicular<br />

to the grain. A further failure observed at the steel shoe<br />

was tension fracture of the 12.5 mm bolts. Accordingly<br />

the bottom steel plate separated itself from the top steel<br />

plate through significant yielding and screw withdrawal<br />

(see Figure 13).


Table 1: Summary of recorded test results<br />

Mc-1 Mc-2 Mc-3 Mc-4 Mc-5<br />

pos. neg. pos. neg. pos. neg. pos. neg. pos. neg.<br />

cycle cycle cycle cycle cycle cycle cycle cycle cycle cycle<br />

max M. [KNm] 69.34 -101.8 88.81 -86.07 79.20 -82.90 89.14 -85.53 108.4 -80.87<br />

rotation @ max M. [°] 2.84 -8.46 3.25 -2.67 3.61 -4.21 2.59 -2.51 2.99 -3.24<br />

failure M. [KNm] 55.47 -81.46 71.05 -68.86 63.36 -66.32 71.32 -68.43 86.73 -64.70<br />

rotation @ failure [°] 3.30 -4.34 3.90 -2.82 3.82 -5.18 3.46 -3.28 3.00 -3.67<br />

40% max M. [KNm] 27.74 -40.73 35.52 -34.43 31.68 -33.16 35.66 -34.21 43.36 -32.35<br />

rotation @ max M. [°] 1.27 -2.16 1.41 -1.47 1.28 -1.44 0.92 -1.08 0.91 -0.98<br />

yield M. [KNm] - - - - - -79.62 83.90 - 101.5 -75.65<br />

rotation @ yield M. [°] - - - - - -3.46 2.25 - 2.13 -2.29<br />

stiffness. [KNm/°] 21.90 18.87 30.52 33.85 24.75 22.97 38.87 35.05 47.75 33.01<br />

ductility [-] - - - - - 1.17 1.15 - 1.40 1.41<br />

Mc-6 Mc-7 Mc-8 Mc-9 Mc-10<br />

pos. neg. pos. neg. pos. neg. pos. neg. pos. neg.<br />

cycle cycle cycle cycle cycle cycle cycle cycle cycle cycle<br />

max M. [KNm] 107.8 -88.31 99.55 -88.41 95.22 -100.9 93.26 -93.98 102.5 -89.18<br />

rotation @ max M. [°] 3.60 2.81 3.55 2.19 3.12 2.87 3.46 4.26 3.14 2.76<br />

failure M. [KNm] 86.28 -70.65 79.64 -70.73 76.17 -80.79 74.61 -75.19 82.02 -71.34<br />

rotation @ failure [°] 3.55 -3.27 4.24 -2.68 3.33 -3.13 3.65 -4.92 3.36 -3.32<br />

40% max M. [KNm] 43.14 -35.32 39.82 -35.36 38.09 -40.39 37.30 -37.59 41.01 -35.67<br />

rotation @ max M. [°] 1.44 -1.14 2.01 -0.90 1.27 -1.05 1.40 -2.08 1.13 -1.05<br />

yield M. [KNm] 106.2 -81.31 - - 94.83 -99.52 - - 95.43 -86.82<br />

rotation @ yield M. [°] 3.05 -2.35 - - 3.12 -2.58 - - 2.71 -2.55<br />

stiffness. [KNm/°] 34.93 37.50 27.27 47.15 29.89 38.47 31.18 23.79 36.36 33.97<br />

ductility [-] 1.18 1.19 - - 1.00 1.11 - - 1.16 1.08<br />

Table 2: Summary statistics of tests results<br />

pos. cycle<br />

neg. cycle<br />

Average Stdev. COV Average Stdev. COV<br />

max M. [KNm] 93.33 12.38 0.13 -89.81 7.08 -0.08<br />

rotation @ max M. [°] 2.92 1.02 0.35 -0.62 4.17 -6.72<br />

failure M. [KNm] 74.66 9.90 0.13 -71.84 5.66 -0.08<br />

rotation @ failure M. [°] 3.56 0.36 0.10 -3.66 0.86 -0.24<br />

40% max M. [KNm] 37.33 4.95 0.13 -35.92 2.83 -0.08<br />

rotation @ max M. [°] 1.30 0.31 0.24 -1.33 0.45 -0.34<br />

yield M. [KNm] 96.62 9.68 0.10 -84.58 9.26 -0.11<br />

rotation @ yield M. [°] 2.64 0.52 0.20 -2.65 0.47 -0.18<br />

stiffness. [KNm/°] 32.34 7.50 0.23 32.46 8.42 0.26<br />

When looking at the average ultimate capacity values<br />

listed in Table 2 for the positive and negative cycle one<br />

can see the high performance of this assembly. The<br />

average ultimate moment resistances exceeded the<br />

design moment capacity of the 130 mm x 304 20f-E<br />

grade glulam member by a factor of 2 in the positive and<br />

a factor of 1.9 in the negative cycle. Considering the<br />

high stiffness of the connection with 32.34 KNm/° in the<br />

positive and 32.46 KNm/° in the negative cycle<br />

application of this connection in real structures seems


appropriate. As a result of eventual fracture of the STS<br />

the ductility of this connection was relatively low. This<br />

can be easily amended with changing the details of the<br />

steel hardware to force the failure into a more ductile<br />

mode by ensuring steel yielding can occur before screw<br />

fracture and withdrawal.<br />

4 CONCLUSIONS<br />

The research projected presented in this paper evaluated<br />

the performance of a moment resisting self-tapping<br />

screw assembly under reverse cyclic load. The applied<br />

tension and compression plates in combination with selftapping<br />

wood screws arranged at 30° to the wood grain<br />

of the beam member resulted in high moment resistance<br />

and very high connection stiffness. Failure of the main<br />

connecting members, the 10 mm x 240 mm ASSY VG<br />

screws, was promoted through the thick bottom steel<br />

plate and the large number of 12.5 mm bolts that were<br />

used as connector at the bottom. The ultimate moment<br />

resistance exceeded the bending moment design capacity<br />

by a factor of 2 in the positive direction and a factor of<br />

1.9 in the negative direction. Main failure modes<br />

observed in the beam member were tension fracture and<br />

withdrawal of screws. In the column member wood<br />

splitting perpendicular to the grain and compression/<br />

transverse shear failure occurred. At the steel shoe<br />

bottom plate significant yielding and tensile failure of<br />

bolts were observed in progressed cycles under heavy<br />

loads.<br />

Even though the ductility of this connection was<br />

relatively low, the high capacity of the tension and<br />

compression plates in combination with the STS allows<br />

one to weakening sections of the steel shoe and therefore<br />

promoting steel yielding instead of screw fracture.<br />

Forcing the steel parts to yield will eliminate brittle<br />

failure modes and increase ductility. In addition, the ease<br />

of assembly and the potential for pre-manufacturing<br />

instead of on site construction may broaden the field of<br />

application for STS connections in large structures.<br />

Creating timber connections that are capable of<br />

exceeding the capacity of the members they connect may<br />

significantly simplify the design of moment resisting<br />

self-taping screw assemblies in the future. This will<br />

form part of the on-going research and development<br />

activities at UBC on moment resisting connections.<br />

ACKNOWLEDGEMENT<br />

The cooperation received from Schraubenwerk Gaisbach<br />

Produktion (SWG) GmbH (www.swg-produktion.de) for<br />

the supply of the tension and compression plates (ZDplates)<br />

and the ASSY VG screws is appreciated.<br />

[2] Blass H.J.: Schmid M.: Self-tapping screws as<br />

reinforcement perpendicular to the grain in timber<br />

connections. Lehrstuhl fuer Ingenieurholzbau und<br />

Baukonstruktionen, University of Karlsruhe (TH)<br />

Germany, date unknown.<br />

[3] Bejtka I.: Verstaerkungen von Bauteilen aus Holz<br />

mit Vollgewindeschrauben. Lehrstuhl fuer<br />

Ingenieurholzbau und Baukonstruktionen,<br />

University of Karlsruhe Germany, 2005.<br />

[4] F. Lam., M. <strong>Gehloff</strong>., M. Closen.: Moment-resisting<br />

bolted timber connections. Proceedings of the<br />

Institution of Civil Engineers, Structures and<br />

buildings 163, pages 267-274, 2010.<br />

[5] M. <strong>Gehloff</strong>., M. Closen., F. Lam. Reduced edge<br />

distances in bolted timber moment connections with<br />

perpendicular to grain reinforcements. In 11 th World<br />

Conference on <strong>Timber</strong> Engineering, 2010.<br />

[6] M. Trautz, C. KOJ. Proceedings of the International<br />

Association for Shell and Spatial Structures (IASS)<br />

Symposium: Valencia, 2009. The RWTH Aachen<br />

University.<br />

[7] <strong>Gehloff</strong> M.: Pull-out Resistance of Self-Tapping<br />

Wood Screws with Continuous Thread. Department<br />

of Wood Science, The University of British<br />

Columbia Vancouver, Canada, 2011.<br />

[8] DIN (Deutsches Institut fuer Normung e.V.) DIN<br />

1052:2004-08: Entwurf, Berechnung und<br />

Bemessung von Holzbauwerken- Allgemeine<br />

Bemessungsregeln und Bemessungsregeln fuer den<br />

Hochbau. Beuth Verlag, Berlin, 2004.<br />

[9] DIBt Allgemeine Bauaufsichtliche Zulassung,<br />

Wuerth ASSY VG plus Vollgewindeschrauben als<br />

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[10] EC 5, EN 1995-1-1: (D), Eurocode 5: Bemessung<br />

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[11] Pruefbericht Nr. 106109: Versuche zur Ermittlung<br />

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Karlsruher Institut fuer Technology, Versuchsanstalt<br />

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[12] H. Krawinkler, F. Ibarra, L. A. Ayoub, R. Medina.<br />

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REFERENCES<br />

[1] Sjoedin J.: Steel-to-<strong>Timber</strong> Dowel Joints- Influence<br />

of Moisture Induced Stresses. School of Technology<br />

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