[0001] This invention relates to anchorages for stressed reinforcing tendons for structures,
for example, concrete or metal structures having internal or external stressed tendons
and other engineering structures having stays constituted by stressed reinforcing
tendons. The invention also relates to a reinforced structure including a reinforcing
tendon and at least one anchorage therefore.
[0002] A reinforcing tendon in a reinforced structure, e.g. a concrete structure, comprises
one or more tensioned elements usually of steel and nowadays usually in the form of
strand, i.e. a multifilament steel wire. The element or elements are anchored after
stressing at each end in an anchorage. At at least one end, there is a "live" anchorage
at which a jack has been applied to tension the element or elements and at which the
tensioned elements are anchored by means of an anchoring device, for example a split
conical wedge lodged in a conical seat in an anchoring body, e.g. a plate. The anchoring
plate bears on the reinforced structure directly or indirectly. Adjacent the anchoring
plate, the element or elements may be located within a rigid tube or trumpet, and
throughout their length in the reinforced structure, or when extending through the
air in the case of an external tendon, they are usually encased in a sheath.
[0003] Recently there has developed a practice of filling the rigid tube or trumpet adjacent
the anchoring body with epoxy resin, which hardens in situ to provide a rigid bond
between the element or elements and the tube or trumpet. The epoxy when hardened transfers
some of the load of the elements to the structure, thus relieving the anchoring wedges
of some of the applied load. This relief is particularly valuable when the load is
subject to cyclical variation, e.g. in a bridge. In GB-A-2,095,302, there is described
a method in which a curable low viscosity epoxy material is introduced into the trumpet
at the anchorage first, and aggregate particles are added later to act as filler.
GB-A-2,148,351 describes further processes of filling, including passing the epoxy
upwardly through a tube passing through the anchoring plate into the trumpet, where
the epoxy fills the space around the stressed elements. It is mentioned that the liquid
epoxy may run back through the bores housing the elements and the conical wedges.
To prevent escape of epoxy in this manner a rubber sheet is fixed to the outside of
the anchoring plate.
[0004] US-A-4,619,088 describes injection of epoxy through the bores housing the conical
wedges which grip the stressed elements, in order that the grouting material, e.g.
epoxy, shall enter a tube closely surrounding the stressed element, in order to anchor
the element to the tube. This tube acts as a secondary member for transferring stress
from the stressed element to the anchoring plate. This tube may extend through the
plate as far as the outer end of the anchoring plate, in which case the anchoring
wedge is located in the tube. Alternatively, the tube has its end close to the narrow
end of the conical wedge in the bore in the anchoring plate.
[0005] The present invention seeks to provide improved load transfer from the stressed element
to the anchoring body, in the case where the stressed element is anchored in the anchoring
body by means of a split conical wedge, and using a hardenable fluid material such
as epoxy resin.
[0006] According to the invention there is provided an anchorage for a stressed reinforcing
tendon having an anchoring body and at least one stressed element of said tendon extending
through a bore in said anchoring body and anchored in said bore by a split conical
wedge in a conical portion of said bore, said bore being substantially entirely filled
by hardened filling material providing a direct bond between the stressed element
in the bore and the wall of the bore, the extent of said filling material being substantially
confined to the bore. Thus the filling material at most projects only slightly from
the bore, at least at the inner end of the bore.
[0007] In the invention, the stressed element in the bore is directly bonded to the anchoring
body by the filling material in the bore, which provides good load transfer between
the stressed element and the anchoring body. Thus the filling material bridges the
gap between the strand and the wall of the bore. Furthermore, the gaps in the split
conical wedge in the bore are entirely filled with the filling material. Preferably
the wedge is toothed at its surface which grips the stressed element, and the filling
material fills the gaps between the teeth and the stressed element, thereby improving
the engagement between the stressed element and the wedge.
[0008] Preferably the bore has a length of at least 8 centimetres, more preferably at least
10 centimetres. Preferably at least 50% of the length of the bore is not occupied
by the conical wedge.
[0009] The invention is particularly applicable to the case where the element is a strand.
[0010] The invention also provides a method of making an anchorage as described above, in
which the hardenable filling material is injected into the bore from outside the bore
at the outside face of the anchoring body and has a viscosity such that it does not
flow freely and substantially entirely fills the bore when injected substantially
without flowing out of the other end of the bore, or at least not to more than a small
extent. Suitably a thixotropic hardenable material is used. The hardenable material
at the time of injection preferably has a "non-sag" thickness (determined according
to ASTM D2730) in the range 10 mm to 40 mm at 15°C.
[0011] The invention is particularly applicable to an anchoring body having a plurality
of bores each housing a stressed element and a conical wedge therefore. In this case
preferably the hardenable material is injected into each bore individually.
[0012] An embodiment of the invention is illustrated by way of non-limitative example in
the accompanying drawing, in which
Fig. 1 is a sectional view of part of an anchorage of the invention during the injection
operation,
Fig. 2 is a sectional view corresponding to Fig. 1 showing the filled bore after injection
and hardening of the filling material, and
Fig. 3 is a sectional view of completed anchorage.
[0013] Fig. 1 shows part of an anchoring plate 1 having a plurality of bores 2, of which
only one is shown in the drawing, each bore housing a stressed steel strand 3 which
is anchored in a frusto-conical portion 4 of the bore by a split conical wedge 5 of
conventional type. Typically the wedge 5 is in three parts, being split along axial
planes. It has teeth (not shown) at its inner surfaces which engage the strand 3.
Anchoring plates of this general kind, and the split conical wedges, are well-known
in this art. Likewise, the application of the present anchorage in a stressed reinforcing
tendon in a concrete structure will be apparent to one skilled in the art without
further description.
[0014] As seen in Fig. 1, the bore 2 of the plate has a length of about 10 cm, of which
about 4 cm are occupied by the wedge 5. In the cylindrical portion 6 of the bore,
where the stressed portion of the strand 3 extends there is a widening at a shoulder
7 at the region not occupied by the wedge 5.
[0015] The vacant spaces of the bore 2 are entirely filled with a hardened filling material
8, such as an epoxy resin. This is injected in liquid state prior to hardening by
applying a covering head 9 to the outside face 10 of the anchoring body 1 with a seal
11 to the face 10 around the opening of the bore 2 and an O-ring 12 sealing to the
projecting end of the strand 3. There is thus left a hollow space 13 at the mouth
of the bore 2, into which hardenable filling material is injected via a passage 14
in the cover 9. Two suitable hardenable materials are mentioned below.
[0016] The hardenable material is injected via the passage 14 and has a viscosity such that
it flows under the injection pressure but does not flow freely. It therefore fills
the space 13 and the whole of the bore 2, including the spaces between the split portions
of the wedge 5 and between the teeth of the wedge 5 and the gripped surface of the
strand 3, and also fills all the space around the strand 3 at the the portion of the
bore not occupied by the wedge 5, finally to emerge at the inner end of the bore to
form a small head 15 around the strand. Preferably this head 15 is as small as possible.
Suitably it projects not more than 2 cm from the end of the core 5.
[0017] After removal of the cover 9 and the seals 11,12, the filling material is allowed
to self-harden (cure) or is hardened for example by heat. There is thus produced the
anchored strand 3 shown in Fig. 2 embedded in a rigid body of hardened filling material
8 which completely fills the bore 2 and provides load transfer between the strand
3 and the anchoring body 1, thus relieving the wedge 5 of a part of the load. The
material 8 also fills the gaps between the teeth of the wedge 5 and the gripped surface
of the strand 3, improving the engagement between the strand and the wedge. As can
be seen, only small portions of the material 8 project from the ends of the bore 2.
[0018] The presence of the step 7 is to allow the strand 3 to have a deflection where it
emerges from the wedge 5 as is often necessary where a plurality of strands are anchored
in a single plate.
[0019] The effect of the rigid body of filling material 8 is to dampen the force applied
by the strand 3 to the wedge 5, so that the wedge absorbs the dead load while the
live load (dynamic load) applied to the strand is mainly or entirely transferred directly
to the anchoring plate by the filling material 8, so that little or no live load is
applied to the wedge. The hardened material 8 in this way improves the fatigue performance
of the anchorage. A stay having an anchorage of the present type has been subjected
satisfactorily to tests of 2 million loading cycles. The tension of the strand 3 is
taken wholly by the plate 1.
[0020] Suitable hardenable materials for injection in the process of the invention are Concresive
(Regd. Trade Name) 1411 and 1428 supplied by Ceilcote GmbH (Biebesheim, Germany).
These have non-sag thicknesses at 15°C of 25 mm (1411) and 20 mm (1428).
[0021] Fig. 3 shows the completed anchorage in section. The anchoring plate 1 bears upon
a support ring 16 embedded in a concrete structure 17 which has a passage 18 bounded
by a tube 19. The plate 1 is shown with three of the bores 2 each receiving a tensioned
strand 3. In practice there are usually a larger number of such bores 2 and strands
3. The strands 3 extend through the passage 18 within a sheath 20, and converge towards
each other. As shown in more detail in Figs. 1 and 2, the strands 3 are anchored in
the anchoring plate by the combination of the split conical wedges 5 and the hardened
filler material 8.
1. An anchorage for a stressed reinforcing tendon having an anchoring body (1) and
at least one stressed element (3) of said tendon extending through a bore (2) in said
anchoring body and anchored in said bore by a split conical wedge (5) in a conical
portion of said bore, said bore being substantially entirely filled by hardened filling
material (8) providing a direct bond between the stressed element (3) in the bore
and the wall of the bore, the extent of said filling material (8) being substantially
confined to the bore.
2. An anchorage according to claim 1 wherein gaps in the- split conical wedge (5)
in the bore are entirely filled with the filling material.
3. An anchorage according to claim 2 wherein said wedge (5) is toothed at its surface
which grips the stressed element, and the filling material fills the gaps between
the teeth and the stressed element.
4. An anchorage according to any one of claims 1 to 3 wherein said bore (2) has a
length of at least 8 centimetres.
5. An anchorage according to any one of claims 1 to 4 wherein said split conical wedge
(5) occupies less than half the length of said bore (2).
6. An anchorage according to claim 1 wherein said stressed element (3) is a metal
strand.
7. A method of making an anchorage for a stressed reinforcing tendon comprising the
steps of
(i) providing an anchoring body (1) having a bore (2) extending it through it and
at least partly bounded by a frusto-conical surface,
(ii) locating a portion of an elongate element (3) of said tendon in said bore, stressing
said element and anchoring it in the bore by means of a split conical wedge (5) engaging
said frusto-conical surface,
(iii) injecting hardenable filling material (8) into said bore at one end thereof
so as entirely to fill the bore, said hardenable filling material having a viscosity
such that it does not flow freely, whereby it does not substantially flow out of the
other end of said bore,
(iv) effecting hardening of said hardenable filling material (8) in said bore, said
hardenable filling material being selected so that after hardening it is capable of
transferring load in said elongate element directly to Said anchoring body.
8. A method according to claim 7 wherein said hardenable filling material (8) when
injected has a no-sag thickness in the range 10 to 40 mm at 15°C.