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Design. Compare. Choose. — design anchor solutions, compare available products and manufacturers, and select the right option based on engineering requirements, performance, and cost.

Temperature ranges

The temperature range describes the service temperatures the bonded anchor is assessed for in its ETA: the short-term value covers brief peaks (e.g. diurnal cycles), the long-term value the sustained base-material temperature. The characteristic bond resistance τRk declared by the ETA depends on the selected range.

Pick the smallest range that envelopes both temperatures expected at the fastening over the working life — a member permanently warmer than the long-term cap needs the next range even if the short-term maximum is not exceeded. A higher range generally means lower declared bond values.

Stand-off installation types

A stand-off exists when the base plate does not bear directly on the concrete — the gap eb is the “Base plate stand-off” below. The installation type decides how the anchors carry SHEAR (EN 1992-4 6.2.2.3 / 7.2.2.3.2) and how the anchor forces are distributed:

TypeImageBehaviour
No stand-off Plate bears on the concrete; shear is verified without a lever arm; rigid-plate force distribution.
Without clamping e Plate on levelling nuts, free to rotate: rod bending over the lever arm la = eb + t/2 + 0.5d with αM = 1. No bearing — anchors also take the compression (linear force distribution).
With clamping Nut and washer clamp the rod at the concrete surface: αM = 2 and the restraint removes the 0.5d depth (la = eb + t/2). Still no bearing under the plate.
With grout Gap packed with mortar: bearing exists (rigid-plate distribution). A pad thicker than 0.5d keeps the rod-bending check (αM = 2); a pad ≤ 0.5d waives it (EN 1992-4 6.2.2.3).

The lever-arm steel check usually governs stand-off designs — an unfilled gap of even a few bolt diameters can cut the shear capacity by an order of magnitude.

Dense existing reinforcement (ψre,N)

Closely spaced surface reinforcement in the base member (spacing < 150 mm, or < 100 mm for Ø ≤ 10 mm) can split off a concrete shell between the bars and the surface. For shallow embedments (hef < 100 mm) the shell-spalling factor ψre,N = 0.5 + hef/200 ≤ 1.0 then reduces the concrete cone, combined pull-out, splitting and pry-out resistances (EN 1992-4 7.2.1.4(5)).

Leave unticked when there is no reinforcement, or its spacing is ≥ 150 mm (any diameter) or ≥ 100 mm (Ø ≤ 10 mm) in both directions. At hef ≥ 100 mm the factor is 1.0 either way.

Crack width limitation (EN 1992-4 7.2.1.7(2)b)

Tick when the member's reinforcement is designed to resist the splitting forces and to limit the crack width to wk ≤ 0.3 mm. The splitting failure verification may then be omitted.

The declaration acts only together with cracked concrete — the clause requires the concrete cone and pull-out checks to assume the cracked state.

Edge reinforcement (ψre,V)

Edge reinforcement (straight bars per Figure 7.10) combined with closely spaced stirrups or a wire mesh (spacing a ≤ 100 mm and a ≤ 2·c1) raises the concrete edge resistance by ψre,V = 1.4 in cracked concrete (EN 1992-4 7.2.2.5(13)).

In uncracked concrete the benefit is already contained in the base value — the factor stays 1.0 and the tick has no effect.

EN 1992-4 Figure 7.10 a

EN 1992-4, Figure 7.10 a — surface reinforcement to take up shear forces

Tension supplementary reinforcement (EN 1992-4 7.2.1.9)

Stirrups or loops around each fastener, designed to carry the tension load across the concrete break-out cone. When active with a valid anchorage length l1, the concrete cone verification is replaced by two checks: steel of the legs (Eq. 7.31) and their anchorage inside the assumed cone (Eq. 7.32).

Detailing per 7.2.1.2(2): ribbed bars ≤ 16 mm around every fastener, only legs within 0.75·hef effective, l1 ≥ 4Ø for hooks/bends/loops or 10Ø for straight legs. Relying on supplementary reinforcement also reduces pry-out by the factor 0.75 (Eq. 7.39) and, when only one direction is reinforced, switches the concrete N–V interaction to Formula (7.57).

EN 1992-4 Figure 7.2 a

EN 1992-4, Figure 7.2 a — supplementary reinforcement (1: stirrups, 2: surface reinforcement) to take up tension loads

Shear supplementary reinforcement (EN 1992-4 7.2.2.6)

Surface reinforcement (Fig. 7.10 a) or stirrups/loops in contact with the fastener (Fig. 7.10 b, c) that carry the shear towards the edge. The concrete edge verification of the reinforced direction is then replaced: the reinforcement is designed for NEd,re = VEd·(1 + es/z), Formula (6.6).

The steel check (7.51) uses k10 = 1.0 for surface reinforcement and 0.5 for loops; the surface form additionally needs the anchorage length l1 inside the edge break-out body (7.52/7.53). Reliance reduces pry-out by 0.75 and, with reinforcement in one direction only, the interaction uses Formula (7.57) with k11 = 2/3.

EN 1992-4 Figure 7.10 b, c

EN 1992-4, Figure 7.10 b, c — stirrups / loops in contact with the fastener

Sustained-load ratio αsus (EN 1992-4 7.2.1.6)

αsus is the sustained fraction of the tension load: αsus = NEd,sus/NEd, where NEd,sus includes permanent actions and the permanent part of variable actions (dead load, prestress, long-term settlement effects). Bonded anchors creep under sustained tension, so the bond resistance is reduced by ψsus = ψ0sus + 1 − αsus ≤ 1.0 (Formula 7.14b), applied inside the combined pull-out–cone check and its pry-out leg.

ψ0sus comes from the product's ETA and depends on the temperature range and working life (typically 0.6–0.99). With αsus ≤ 1 − ψ0sus the factor stays 1.0 — a fully short-term load loses nothing; a fully sustained load (αsus = 1) reduces the bond to ψ0sus·τRk. Steel and concrete-cone modes are not affected.

Interface shear check (EN 1992-1-1 6.2.5)

The joint between existing and new concrete is a cold joint: the longitudinal shear acting across it must be transferred by adhesion, friction and the reinforcement crossing the interface. “no” omits this verification — for joints verified elsewhere or not loaded in shear.

On the end-anchorage route a shear-loaded joint must declare its transfer path: pick a verification method here, or “transferred externally” when a shear key / dowels carry it (recorded in the result as your declaration). With shear present and “no” selected, the result is marked failed until the path is declared.

EN 1992-1-1 6.2.2/6.2.3 is the strut-and-tie route for members dominated by bending: the concrete shear resistance VRd,c (6.2a/b), reduced by the roughness knock-down c/0.5. EN 1992-1-1 6.2.5 checks vRdi = c·fctd + μ·σn + ρ·fyd·(μ·sin α + cos α) directly at the interface — for shear/compression-dominated joints.

The joint roughness supplies the coefficient pair c / μ per 6.2.5(2): very smooth 0.025/0.5, smooth 0.20/0.6, rough (≥ 3 mm profile) 0.40/0.7, indented 0.50/0.9 — it is used only by this check.

Transverse pressure ptr (TR 069 Eq. 4.13)

Stress acting across the drilled bars in the existing member — bearing pressure from loads above the anchorage (compression, −) or restraint stresses pulling the zone apart (tension, +). Through Ωp,tr (Eq. 4.11a) it scales the bond-splitting resistance: transverse tension opens the splitting cracks and cuts the bond by up to 30 % at ptr = fctm; transverse compression clamps the bars and raises it.

0 (the default) means no effect. Only the bond-splitting verification is affected — steel and concrete cone are not. Enter a negative (clamping) value only for a pressure that is reliably permanent.

Compression-zone overrides (ψM,N, TR 069 Eq. 4.9)

A bending moment presses the section's compression resultant onto the concrete beside the anchorage, clamping the potential break-out cone. The cone resistance grows by ψM,N = 2 − z/(1.5·lb) ≥ 1.0 — the closer the compression sits to the bars (small z), the larger the benefit, up to ×2.

Blank fields (the default) derive the lever arm z and the ratio |CEd|/NEd from the interface cross-section analysis. Fill them only to impose values from your own frame analysis. The benefit applies only when |CEd|/NEd ≥ 0.8, z is known and no edge lies closer than 1.5·lb — otherwise ψM,N = 1.0.

End-anchorage design methods

Pick the method by the load situation at the interface:

MethodLoad situation at the interfaceVerification
EOTA TR 069Bending and shear, with compression or tension (uni- or biaxial); continuous joints onlyAnchorage length with the product's bond-splitting strength (ETA) plus the concrete break-out check
EN 1992-1-1Compression and/or shear (no bending moment)Anchorage length per EN 1992-1-1 8.4.4
EN 1992-1-1Bending and shear (uniaxial), with or without compression — e.g. an L-shaped frame cornerStrut-and-tie model to equilibrate the moment, anchorage per 8.4.4 (not implemented yet — the result is marked out of scope)

EOTA TR 069 is valid only in continuous joints: a beam-to-column frame corner (L-joint) must be designed with the EN 1992-1-1 strut-and-tie method.

Joint roughness (EN 1992-1-1 6.2.5(2))

Classifies the surface of the cold joint between the existing and the new concrete. It sets the adhesion coefficient c and the friction coefficient μ of the interface-shear verification; the 6.2.2/6.2.3 route applies the same c as its c/0.5 knock-down.

ClassSurfacecμ
Very smoothcast against steel, plastic or smooth wooden moulds0.0250.5
Smoothslipformed or extruded, or free surface left after vibration0.200.6
Rough≥ 3 mm roughness at ~40 mm spacing (raking, exposed aggregate)0.400.7
Indentedindentations per EN 1992-1-1 Figure 6.90.500.9

Roughening the joint (raking, high-pressure water jetting, exposed aggregate) is the cheapest way to raise the interface capacity — a very smooth formwork joint carries almost no adhesion.

EN 1992-1-1 Figure 6.9

EN 1992-1-1, Figure 6.9 — indented construction joint

Shear reinforcement in the new member (EN 1992-1-1 6.2)

For a beam or column joint checked with method 6.2.2, the shear resistance depends on whether the NEW member carries shear reinforcement (links / stirrups) across the joint region:

SelectionModel
yesStrut-and-tie per 6.2.3: VRd = max(VRd,c, VRd,max) with the chord lever arm between the outer bar layers; the joint roughness factor c/0.5 applies.
noMember without shear reinforcement per 6.2.2 eq. (6.2): only VRd,c with the tensioned connection bars as longitudinal reinforcement — usually MUCH lower.

Select no when the new member has no links crossing the joint — assuming links that are not there overestimates the shear capacity by an order of magnitude.

Tension-chord shift ΔFtd (EN 1992-1-1 6.2.3 / 9.2.1.3)

Shear across the section shifts the tension line: the tension chord carries an additional longitudinal force ΔFtd = VEd·cot θ (cot θ = 1.0). For a discrete rebar connection the full shift applies — not the 0.5·V·cot θ of a distributed beam web.

The shift is split per reinforcement layer: each of the n layers carries ΔF/n shared over its bars, raising their steel stress σsd and with it the required lap or anchorage length. The transverse shear transfer across the joint still needs its own path — a roughened surface, dowels, or the interface-shear check.

Most unfavourable tolerance (EN 1992-1-1 8.7.2)

A drilled bar cannot be guaranteed to sit directly beside the existing bar it laps onto. This option designs for the worst permitted position: a non-contact splice with a clear distance e = bar spacing / 2 (columns: max(sx, sy)/2).

Per EN 1992-1-1 8.7.2(3), a lap with e beyond 4Ø (max 50 mm) is lengthened by the excess: l0,e = e − min(4Ø, 50 mm), added to the lap length l0 and the installation length lv. Untick only when the drill position is controlled on site and the actual spacing is entered.

Design actions — static and quasi-static loading

Enter design values at the ultimate limit state (ULS) — actions already factored and combined to EN 1990. The verification compares them directly against the design resistances; no further partial factor is applied to what you type here.

The methods used here — EN 1992-4 (main body), EOTA TR 069 and EOTA TR 023 / EN 1992-1-1 — cover predominantly static actions, i.e. static and quasi-static loading: self-weight, imposed and wind loads, earth and water pressure, temperature and shrinkage effects, and slowly applied or rarely repeated variable actions.

Not covered by this calculation: seismic actions (EN 1992-4 Annex C, performance categories C1/C2), fatigue (Annex B), and impact or shock loading. Each of those needs the product to be assessed for that action in its ETA and a design check beyond the scope of this tool. Use these results for predominantly static design situations only.

Sign convention: N is positive in tension and negative in compression; shear and moment components are taken about the axes shown on the 3D model.

Transverse reinforcement on the lap (α3, EN 1992-1-1 8.7.4)

Stirrups along the lap confine the concrete and take up the transverse tension forces of the splice; the lap length may then be reduced by α3 = 1 − K·λ ≥ 0.7, with λ = (ΣAst − ΣAst,min)/As counted over the stirrups within the lap zone and K set by the stirrup-leg position (Fig. 8.4).

“yes” opens the stirrup fields: Ø and spacing give the countable ΣAst over the assumed lap length, the cover sets where the first stirrup sits in the 3D model. “no” takes no confinement credit — α3 = 1.0 — which is always conservative.

EN 1992-1-1 Figure 8.4

EN 1992-1-1, Figure 8.4 — values of K for beams and slabs

Transverse reinforcement — confinement Ktr (TR 069 Eq. 4.12)

Ktr = (nt·Ast)/(nb·Ø·sb) ≤ 0.05 (Eq. 4.12, per fib Model Code 2010): nt — number of legs of confining reinforcement crossing a potential splitting surface; Ast — cross-sectional area of one stirrup leg; nb — number of anchored bars in that splitting surface; sb — spacing of the confining reinforcement. The term km·Ktr is added inside the bond-splitting resistance, Eq. (4.11a), and stays capped by the ETA bond limit (4.11b/c).

kmEffectiveness of the links (TR 069 / Figure 4.2, fib Bulletin 72)
12rebars confined inside a bend of links passing round the bar by at least 90° (ai ≤ 125 mm or ai ≤ 5Ø)
6the rebar is more than 125 mm and more than 5Ø from the nearest vertical leg of a link crossing the splitting plane approximately perpendicularly
0a splitting crack would not intersect the transverse reinforcement — links positioned inside the bars, or the clear bar spacing is less than 4 times the bottom cover (cs < 4cy)

Count only links of the EXISTING member around the anchorage — not new-member stirrups. “no” sets Ktr = 0 (always conservative). Independent of “Dense existing reinforcement”, which reduces the concrete cone (ψre,N) for shallow embedments.

EOTA TR 069 Figure 4.2

EOTA TR 069, Figure 4.2 — reduced effectiveness of links (fib Bulletin 72)

Bond condition (EN 1992-1-1 8.4.2)

The design bond strength fbd = 2.25·η₁·η₂·fctd depends on the bond-condition coefficient η₁: 1.0 in “good” conditions, 0.7 otherwise — poor bond lengthens anchorages and laps by roughly 40 %.

Good conditions per EN 1992-1-1 Figure 8.2: all bars inclined 45–90° to the horizontal, and horizontal bars in members ≤ 250 mm deep, in the bottom 250 mm, or at least 300 mm below the top surface. Anything else — notably top bars of deep members — is “poor”. The selection feeds fbd of both the drilled bar and the existing cast-in bar.

EN 1992-1-1 Figure 8.2

EN 1992-1-1, Figure 8.2 — description of bond conditions