[0001] The present invention concerns a concreting jet spray apparatus comprising a concrete
mix container having a propelling flight for moving the concrete mix and a jet nozzle
assembly at the exit end of the flight assembly with a compressed air jet nozzle inside
the jet assembly.
[0002] The compressed air channel leading to the compressed air jet nozzle assembly is conventionally
adapted to pass through the center of the shaft of the concrete mix propelling flight
(Fig. 1). Disclosed in German patent application publications 2 056 145 and 2 103
448 is an alternative embodiment in which compressed air is routed from an annular
slot of the nozzle assembly to the jet-forming nozzle.
[0003] The present invention aims to achieve a novel type of a concreting jet spray apparatus,
which offers significant advantages in comparison with conventional techniques. The
concreting jet spray apparatus is characterized by having the jet nozzle assembly
mounted to the head of the concrete mix-propelling flight assembly so that the jet
nozzle is adapted perpendicularly to the flight axis. Thus, one or several compressed
air nozzles can be adapted to the jet nozzle head assembly in a desired manner. The
need for routing compressed air via ducts is avoided allowing the flight to be rotated
with a solid shaft.
[0004] An embodiment of the invention is characterized by having the compressed-air jet
nozzle comprised of a pipe placed within the rear section of the nozzle head assembly
and perpendicularly to the flight axis. This kind of a compressed-air jet nozzle is
simple in construction, cost-effective in manufacturing and, when required, quickly
replaceable with different types of jet nozzles.
[0005] Another embodiment of the invention is characterized by having the nozzle assembly
pivotally mounted to the end of the flight assembly to be rotatable about the axis
of the flight. Thus, the nozzle assembly can easily be directed to a desired point
if spraying is desired to be performed obliquely from above or from below.
[0006] A further embodiment of the invention is characterized by having the jet nozzle assembly
rotatably mounted with the help of a ball-socket joint to the head of the flight assembly
so that the nozzle direction is freely adjustable to any direction. In this way the
jet can be directed in desired directions, and furthermore, if the flight assembly
is provided with two auger flights with individual head assemblies, significant improvements
will be achieved in comparison with all prior art concreting jet constructions.
[0007] In the following, the invention will be examined in more detail by means of an exemplifying
embodiment with reference to the attached drawings, in which
Fig. 1 shows a conventional concreting jet spray apparatus in a cross-sectional view.
Fig. 2 shows a concreting jet spray apparatus in accordance with the invention in
a top view.
Fig. 3 shows a section of Fig. 3 along line III-III of the apparatus.
Fig. 4 shows the jet nozzle assembly of the apparatus in an enlarged view.
Fig. 5 shows the jet nozzle assembly in a partially sectioned end view.
Fig. 6 shows another embodiment of the concreting jet spray apparatus having two concrete
mix-propelling flights and two jet nozzle assemblies.
Fig. 7 shows a concreting jet spray apparatus in accordance with the invention inclined
from the vertical axis.
[0008] The concreting jet comprises a concrete mix container 1 with a concrete mix-transferring
flight 2 below the container, and a jet nozzle assembly 3 mounted to the end of the
flight assembly, having a compressed-air nozzle 4 inside the nozzle assembly. The
nozzle assembly 3 is mounted to the head of the flight 2 assembly so that the nozzle
section is perpendicular to the flight axis. The compressed-air nozzle 4 is comprised
of a tube 5, mounted to the rear section of the nozzle assembly 3, so that the tube
also is aligned perpendicular to the flight. Fig. 5 illustrates the method of mounting
the nozzle assembly 3 rotatably to the end section of the flight assembly as indicated
by arrow 6. The angle of rotation may be up to 180°. Figs. 6 and 7 illustrate a concreting
jet spray apparatus with dual spray assemblies, in which an inclination α of the apparatus
allows the elevations of the spray assemblies to be displaced by height x, whereby
the spraying operation is speeded up. The number of compressed-air nozzles can be
freely selected so that the embodiment shown in Fig. 5 has, for instance, three nozzles.
The concrete mix container 1 also has a fill blade 7, which shears and propels the
concrete mix, which now may have a very high stiffness, toward the flight 2. By virtue
of the invention, the design of the nozzle section can be varied to a large extent
allowing minimization of the flow resistance to the concrete mix and use of extremely
stiff and coarse-aggregate mixes.
[0009] The nozzle assembly 3 may, of course, be provided with two nozzles adapted horizontally
or vertically adjacent. In this arrangement, the nozzle assembly will correspondingly
contain two compressed-air nozzles 4, or groups of nozzles, respectively.
1. A concreting jet apparatus comprising a concrete mix container (1) having a concrete
mix-propelling flight (2) mounted below the container, and a jet nozzle assembly (3)
adapted to the end section of the flight assembly, having a compressed air jet nozzle
(4) mounted inside the assembly, characterized in that the jet nozzle assembly (3) is mounted to the end section of the flight (2)
assembly so that the jet nozzle assembly is perpendicular to the axis of the flight.
2. A concreting jet spray apparatus as claimed in claim 1, characterized in that the compressed-air jet nozzle (4) is comprised of a tube (5) mounted inside
the rear section of the jet nozzle assembly (3) so that the tube also is aligned perpendicular
to the axis of the flight.
3. A concreting jet spray apparatus as claimed in claim 1 or 2, characterized in that the jet nozzle assembly (3) is mounted rotatably to the end section of the
flight (2) assembly so as to be pivotable about the flight axis.
4. A concreting jet spray apparatus as claimed in any of claims 1...3, characterized in that the jet nozzle assembly (3) is mounted rotatably with the help of a ball-socket
joint to the head of the flight (2) assembly so that the nozzle direction is freely
adjustable in any direction.