[0001] The present invention relates to a heat-recovery boiler provided with a divergent
duct between the outlet of a turbine and the inlet of a boiler.
[0002] Boilers of the above type utilize the heat of the exhaust gases from the gas turbine,
which are conveyed to the heat-recovery boiler by means of a so-called divergent duct.
[0003] Current heat-recovery boilers known from the state of the art are approximately 16
to 20 m high.
[0004] A so-called divergent duct, which may be 15 to 20 m long, is provided between the
outlet duct of the gas turbine, having a diameter of approximately 5 to 6 meters,
and the heat-recovery boiler.
[0005] It is easily understandable that the hot exhaust gases exiting from the outlet of
the feeder turbine towards the inlet of the heat-recovery boiler should not undergo
excessive load losses, which instead occur inside conventional divergent ducts.
[0006] Attempts to improve the situation have been made by using relatively long divergent
ducts formed substantially by walls which tun from the outlet of the turbine to the
inlet of the heat-recovery boiler.
[0007] These considerably large ducts, however, entail the drawback that they are relatively
heavy, owing to the amount of construction material used; moreover, conventional solutions
do not allow to effectively decrease the generation of unwanted vortices.
[0008] In order to obviate these drawbacks, it has been suggested to install, inside the
divergent duct, grids of pipes for deflecting the stream of hot gases.
[0009] These flow deflectors allowed to even out, to a certain extent, the stream of hot
gases, also partially reducing the formation of unwanted vortices, but high load losses
in the gas stream were inevitable and removed pressure which was useful for the effective
heat exchange of the heat-recovery boiler.
[0010] Accordingly, the aim of the invention is to obviate the drawbacks of the prior art
and to provide a new divergent duct having much smaller dimensions which lead to a
considerable saving in construction material; an object of the invention is also to
provide a divergent duct in which it is possible to provide, between the outlet of
the gas turbine and the inlet of the heat-recovery boiler, a current which has no
flow recirculations and in which load losses are reduced to an acceptable minimum.
[0011] According to the invention, this aim is achieved in that the covering wall of the
divergent duct that runs from the top of the boiler to the top of the outlet of the
gas turbine has an inclination which forms an angle (α) greater than 45° and up to
75° with respect to the horizontal plane, and that the inclined wall of the divergent
duct is connected to the top of the outlet of the gas turbine through a wall which
is shaped like an arc. Preferably, inside the divergent duct, in the region adjacent
to the arc-shaped wall, aerodynamic profiles for conveying the gas stream are provided
which are arranged in succession and in adjacent rows.
[0012] Preferably, the angle (α) assumes a value between 62° and 65°.
[0013] When the plant requires a reheating system, it is advantageous to install burners
which can be orientated and adapted with respect to the direction of flow of the hot
gas stream inside the divergent duct and downstream of the aerodynamic profiles that
are optionally present.
[0014] Advantageously, the aerodynamic conveyance profiles have an arc-like configuration
on their leading edge, and the part of the metal plates directed towards the inlet
of the heat-recovery boiler is formed by converging conduction plates which cover
an angle (γ) of approximately 20°.
[0015] Preferably, the bottom wall of the divergent duct is inclined with respect to the
horizontal plane.
[0016] Advantageously, the metal plates of the aerodynamic profile have a concave/convex
shape in order to efficiently open out the stream of hot gases directed towards the
boiler.
[0017] Further characteristics of the invention will become apparent from the dependent
claims.
[0018] With a divergent duct of this kind a considerable saving in construction material
is achieved, the structure of the divergent duct is considerably shorter and the flow
profile of the hot gases is uniform over the entire inlet front of the heat-recovery
boiler.
[0019] The device according to the present invention is now described in greater detail
and illustrated by means of an embodiment given only by way of example in the accompanying
drawings, wherein:
Figure 1 is a schematic view of the divergent duct conceived according to the invention
and arranged between the outlet of a gas turbine and the inlet of a heat-recovery
boiler;
Figure 2 is a schematic sectional view of an aerodynamic conveyance profile according
to the present invention;
Figure 3 is a sectional view of an aerodynamic conveyance profile having a concave/convex
profile; and
Figure 4 is a schematic view of the flow lines of the hot gases inside the divergent
duct according to the present invention.
[0020] As shown in Figure 1, the outlet of a gas turbine is connected to the inlet 2 of
a heat-recovery boiler, by using for this purpose a divergent duct, generally designated
by the reference numeral 3.
[0021] The divergent duct 3 is advantageously provided by means of a frame-like structure.
[0022] Vertical side walls, designated by the reference numerals 4 and 5, form, together
with a bottom wall 6 and a covering wall 7, the internal space 9 of the divergent
duct.
[0023] The hot gases are fed from the outlet 1 of the turbine in the direction indicated
by the arrow 102 in order to enter the heat-recovery boiler 2 in the direction indicated
by the arrow 110.
[0024] The bottom wall 6 is inclined with respect to the horizontal plane by an angle (β)
of approximately 15° in order to join with the inlet of the heat-recovery boiler.
[0025] The covering wall 7 has an angle (α) which is greater than 45° and up to 75°, preferably
approximately 62-65° with respect to the horizontal plane 100.
[0026] A portion 8 made of metal plate and having an arc-like shape is provided between
the outlet 1 and the inclined covering wall 7.
[0027] Tests have shown that advantageously the radius of curvature R of the arc-shaped
wall 8 corresponds to a value of 0.5-0.8 times the vertical dimension of the inlet
of the divergent duct.
[0028] The internal internal space 9 of the divergent duct 3 accommodates, proximate to
the region formed by the arc-shaped plate 8, a plurality of aerodynamic conveyance
profiles designated by the reference numeral 10.
[0029] Advantageously, the aerodynamic conveyance profiles 10 that run through the internal
space 9 are arranged along arc-shaped segments having the same center 101 as the radius
of curvature that forms the profile of the arc-shaped plate 8.
[0030] The aerodynamic profiles 10 are arranged in groups and sequentially along arc-like
paths 103, 104, 105 and 106 whose radii increase from the center 101 in order to uniformly
diffuse the stream of hot gases in the divergent duct.
[0031] Advantageously, the aerodynamic conveyance profiles 10, which run lengthwise along
the internal space 9, are supported by the walls 4 and 5 so as to allow an angular
adjustment, allowing to adapt the angle of attack of the profile with respect to the
stream, so as to achieve the different degrees of deflection of the hot fumes in the
entire divergent duct.
[0032] Downstream of the aerodynamic profiles 10, inside the internal space 9, reheaters
20, 21, 22 and 23 are provided and, according to the invention, these burners can
be adjusted angularly in an operating position, so that their flame is aligned with
the lines of flow of the hot gas stream, as defined by the conveyance profiles 10.
[0033] In this manner, the burner 20 is arranged so that its centerline axis is at approximately
57° with respect to the horizontal plane, while the axis of the burner 21 is arranged
at 45° with respect to the horizontal plane and the axis of the burner 22 is arranged
at 31° with respect to the horizontal plane.
[0034] As shown in Figure 2, the conveyance profiles 10 are composed of a tube 30 having
a circular cross-section, the rounded part 31 whereof is directed towards the incoming
gas stream, designated by the reference numeral 102.
[0035] The remaining part of the tube 30 is covered by two conduction plates 32 and 33,
the free ends whereof are joined at the point 34. The plates 32 and 33 are sized so
as to cover an angle (γ) of approximately 20°.
[0036] For some conveyance profiles 10, it is more advantageous to adopt a concave/convex
shape for the edges 200, 201, so as to accordingly achieve a greater stream deflection
capability for an equal angle of attack and a lower pressure loss due to wake eddies.
1. A heat-recovery boiler provided with a divergent duct which runs from the outlet of
a turbine to the inlet of a boiler, characterized in that the covering wall (7) of
the divergent duct (3), which runs from the top of the boiler (2) to the top of the
outlet of the gas turbine (1), is inclined at an angle (α) which is greater than 45°
and up to 75° with respect to the horizontal plane (100), and in that the inclined
wall (7) of the divergent duct (3) is connected to the top of the outlet (1) of the
gas turbine by means of an arc-shaped wall (8).
2. A heat-recovery boiler according to claim 1, characterized in that on the inside (9)
of the divergent duct (3), in the region lying adjacent to the arc-shaped wall (8),
aerodynamic gas stream conveyance profiles (10) are provided which are arranged in
succession and in adjacent rows (103, 104, 105, 106).
3. A heat-recovery boiler according to one or more of the preceding claims, characterized
in that the angle (α) is between 62° and 65°.
4. A heat-recovery boiler according to one or more of the preceding claims, characterized
in that on the inside (9) of the divergent duct (3) and downstream of the sets of
aerodynamic conveyance profiles (10) a plurality of burners (20, 21, 22, 23) is provided,
and in that the burners (20, 21, 22, 23) are provided so that their angular position
can be adjusted.
5. A heat-recovery boiler according to one or more of the preceding claims, characterized
in that the aerodynamic conveyance profiles (10) have an arc-like shape (30, 31),
on the edge (102) first affected by the hot gas stream, and in that the wall of the
plates (10) that is directed towards the inlet (110) of the heat-recovery boiler (2)
is formed by converging conduction plates (32, 33) covering an angle (γ) of approximately
20°.
6. A heat-recovery boiler according to one or more of the preceding claims, characterized
in that the conveyance profiles (10) have a concave/convex shape for their edges (200,
201).
7. A heat-recovery boiler according to one or more of the preceding claims, characterized
in that the radius of curvature (R) of the arc-shaped wall (8) corresponds to a radius
which is 0.5-0.8 times the height of the inlet of the divergent duct (3).
8. A heat-recovery boiler according to one or more of the preceding claims, characterized
in that the aerodynamic conveyance profiles (10) are arranged along arc-shaped segments
(103, 104, 105, 106) which have a single center (101) for their radius of curvature
(R) and in that the different paths (103, 104, 105, 106) have progressively greater
curvature radii.
9. A heat-recovery boiler according to one or more of the preceding claims, characterized
in that the conveyance profiles (10) cross the internal space (9) of the divergent
duct (3) along its width and in that the aerodynamic profiles (10) are supported by
the walls (4, 5) so as to allow angular adjustment and orientation.
10. A heat-recovery boiler according to one or more of the preceding claims, characterized
in that the aerodynamic conveyance profiles (10) are composed of a tube (30) having
a circular cross-section and the round part (31) whereof is directed towards the incoming
gas stream (102), and in that the remaining part of the tube (30) is covered by two
conducting plates (32, 33), whose free ends are joined and cover an angle (γ).