[0001] The present invention relates to a tile holder for a combustor of a gas turbine.
[0002] As known, in gas turbine combustors acoustic dampers are used for the purpose of
mitigating the acoustic pulsations that may occur during operation in specific frequency
ranges. Acoustic dampers attenuate acoustic oscillations in respective frequency bands
and, when appropriately tuned, may prevent noxious vibrations to the benefit of efficiency,
performance and structural integrity. In order to maximize the beneficial effect,
size and location of the acoustic dampers need to be accurately selected and meet
several requirements, e.g. in relation to acoustic, thermal and mechanical performance,
feasibility and gas turbine efficiency.
[0003] Coupling acoustic dampers to the combustion chambers of combustors, however, is not
a simple task, because combustion chambers must be internally provided with a thermoinsulating
coating or heat-shield, due to the high temperatures reached during the machine operation.
The heat-shield generally comprises a plurality of tiles made of special metallic
alloys or of refractory material and arranged in contiguous rows on the inner surface
of the shell of the combustion chamber, so as to define a substantially continuous
surface. Providing access to the combustion chamber for acoustic coupling would require
modifying the tiles, in other words either making special refractory tiles with access
holes or drilling holes in metallic tiles. This would in any case incur additional
costs and may also put the mechanical resistance of the tiles at risk. Moreover, tile
holders, which are used to retain the tiles against the shell of the combustion chamber,
limit the space available for coupling acoustic dampers and the positioning thereof
is made difficult if possible at all.
[0005] The object of the present invention is therefore to provide a tile holder for a combustor
of a gas turbine, which allows to overcome or at least reduce the limitations described
above.
[0006] According to the present invention, there is provided a tile holder for a combustor
of a gas turbine, comprising:
a connector having a tubular body extending along a first axis and a retaining system,
configured to secure the tubular body in a seat through a wall and to retain a tile
against the wall;
an acoustic damper having a damping volume and a neck at least in part extending along
a second axis;
wherein the neck is acoustically coupled to the outside through the tubular body and
the first axis is transverse to the second axis.
[0007] The tile holder therefore provides also the functions of mechanical supporting and
acoustic coupling for an acoustic damper. Acoustic dampers can thus be easily fitted
to the combustor and acoustically coupled to the combustion chamber and there is no
need to modify the tiles. All tiles having a through seat for receiving a tile holder,
no matter whether metallic tiles or refractory tiles, can be equally used for the
purpose of supporting and acoustically coupling acoustic dampers.
[0008] According to an aspect of the present invention, the retaining system comprises a
retaining member at a tile-coupling end of the tubular body, the retaining member
projecting radially outward from the tubular body.
[0009] The inner end of the tile holder, that faces the inside of the combustion chamber,
is configured to easily engage and firmly retain a respective tile.
[0010] According to an aspect of the present invention, the retaining member comprises a
retaining ring removably coupled to the tile-coupling end of the tubular body.
[0011] Removable connection (e.g. threaded connection) simplifies assembling and disassembling
of the tile holder and acoustic damper, that is particularly appreciated in maintenance
operation for replacement of any of the connector, acoustic damper and tile as required.
[0012] According to an aspect of the present invention, the retaining system comprises a
threaded portion at a wall-coupling end of the tubular body.
[0013] The threaded portion provides for direct coupling the shell of the combustion chamber,
which is usually provided with threaded through seats for receiving conventional tile
holders.
[0014] According to an aspect of the present invention, the retaining system comprises an
externally threaded bushing fitted onto the wall-coupling end of the tubular body.
[0015] Parts of the tile holder can be easily mounted and removed. For example, the tubular
body may be extracted and replaced without removing the threaded bushing, which may
remain permanently connected to the shell because of high operating temperatures.
[0016] According to an aspect of the present invention, the neck comprises a securing mechanism
configured to secure the neck to the wall.
[0017] The securing mechanism helps fastening the neck directly and independently to an
outer face of the shell of the combustion chamber. Other parts of the tile holder,
such as the threaded portion of the retaining system, may be removed (e.g. for the
purpose of replacing the tile) without intervening on the acoustic damper.
[0018] According to an aspect of the present invention, the securing mechanism comprises
mounting plates, integral with the neck and provided with mounting holes, and screws
through the mounting holes for connecting to seats in the wall.
[0019] According to an aspect of the present invention, the screws are parallel to the first
axis of the tubular body or the screws are parallel to a portion of the neck at an
interface with the tubular body.
[0020] The screws can be easily tightened into respective receiving threaded holes in the
outer face of the shell of the combustion chamber. The orientation of the screws may
be conveniently selected as desired depending on the freedom to make the receiving
holes, namely while manufacturing a new machine or during retrofitting operations.
[0021] According to an aspect of the present invention, the neck of the acoustic damper
comprises a terminal duct, having the damping volume at one end, and an intermediate
duct, between the tubular body and the terminal duct.
[0022] Modular construction of the acoustic damper increases flexibility of use and ease
of mount.
[0023] According to an aspect of the present invention, the intermediate duct is coaxial
to the terminal duct.
[0024] According to an aspect of the present invention, the intermediate duct extends along
a third axis which is transverse to the first axis and to the second axis.
[0025] Accordingly, the configuration of the acoustic damper can be flexibly selected to
meet both acoustic requirements and space limitations.
[0026] According to an aspect of the present invention, the terminal duct and the intermediate
duct comprise respective coupling flanges for releasable mutual connection.
[0027] The coupling through flanges can be easily released for removing and replacing the
acoustic damper. Maintenance and retrofit are therefore made simpler.
[0028] According to an aspect of the present invention, the tubular body has a rounded edge
coupled to the neck, whereby a smooth transition is defined between the tubular body
and the neck.
[0029] The smooth transition is beneficial for the properties of the acoustic damper.
[0030] According to an aspect of the present invention, a combustor of a gas turbine comprises
a combustion chamber, having a shell defined by a wall and a heat-shield on an inner
surface of the wall, wherein the heat-shield comprises a plurality of tiles and at
least one damper connection tile is retained against the wall by a tile holder according
to any one of the preceding claims.
[0031] According to an aspect of the present invention, the wall has a through seat and
the connector of the tile holder is fitted in the through seat.
[0032] According to an aspect of the present invention, the damper connection tile has a
rim that delimits at least a portion of a retaining seat and the connector engages
the rim to retain the damper connection tile against the wall.
[0033] The present invention will now be described with reference to the accompanying drawings,
which illustrate some examples of non-limiting embodiments, wherein:
- Figure 1 is a side view, cut along a vertical axial plane, of a combustor of a gas
turbine, with parts removed for clarity;
- Figure 2 is an enlarged side view, cut along a longitudinal axial plane, of a tile
holder in accordance with an embodiment of the present invention incorporated in the
combustor of figure 1;
- Figure 3 is an enlarged view of a detail of figure 2;
- Figure 4 is a front view of the tile holder of Figure 2;
- Figure 5 is a side view of a tile holder in accordance with another embodiment of
the present invention;
- Figure 6 is a side view of a tile holder in accordance with another embodiment of
the present invention; and
- Figure 7 is a side view, cut along an axial plane, of a tile holder in accordance
with another embodiment of the present invention.
[0034] Figures 1 illustrates a combustor 1 of a gas turbine (with parts removed for the
sake of clarity). The combustor 1 comprises an annular combustion chamber 2, extending
around an axis A and having a shell defined by an annular wall 3 and a heat-shield
5 on an inner surface of the annular wall 3. The arrangement herein described is given
purely by way of example and is not to be considered limiting, however. In particular,
the combustion chamber may be of any type, such as of the silo or can or cannular
type.
[0035] The heat-shield 5 comprises a plurality of first thermoinsulating tiles 7 of a metallic
alloy and a plurality of second thermoinsulating tiles 8 of refractory material, all
arranged in adjacent circumferential rows, around the axis A of the combustion chamber
2. In one embodiment, the thermoinsulating tiles 7, 8 may be of generally quadrangular
shape. Also other shapes are available, however.
[0036] At least one of the first thermoinsulating tiles 7, selected for the purpose of coupling
an acoustic damper, is fastened to the annular wall 3 by a tile holder 10 in accordance
with an embodiment of the present invention. The tile holder 10 comprises a connector
11 and an acoustic damper 12 coupled to the inside of the combustor chamber 2 through
the connector 11 as described hereinafter. The other first thermoinsulating tiles
7 may be supported by further tile holders 10 or by conventional tile holders, as
desired for the purpose of coupling acoustic dampers to the combustion chamber 2.
[0037] The second thermoinsulating tiles 8 are provided with spring holders 13, which engage
circumferential guides 14, which are formed on the inner face of the wall 3 and extend
around the axis A.
[0038] As already mentioned, the tile holder 10 comprises a connector 11 and an acoustic
damper 12 coupled to the inside of the combustor chamber 2 through the connector 11.
[0039] As illustrated in figures 2 to 4, the connector 11 comprises a tubular body 15, which
extends along a connector axis X1, and a retaining system 17, configured to secure
the tubular body 15 in a threaded through seat 18 in the annular wall 3 and to retain
the respective first thermoinsulating tile 7 against the annular wall 3. The tubular
body may have any suitable cross-section, such as circular, elliptical or polygonal
cross-section and the present disclosure is not limited to a specific example.
[0040] The retaining system 17 comprises a retaining member 20 at a first end of the tubular
body 15 coupled to the first thermoinsulating tile 7. Specifically, the first thermoinsulating
tile 7 has a through retaining seat 21 delimited by a rim 22. In one embodiment, the
retaining seat 21 is provided centrally in the first thermoinsulating tile 7. In other
embodiments not shown, however, the retaining seat may be provided between two or
more first thermoinsulating tiles. In this case, each first thermoinsulating tile
has a rim that delimits a portion of the through retaining seat. The retaining member
20 projects radially outward from the tubular body 15 and engages the rim 22 to retain
the first thermoinsulating tile 7 against the annular wall 3. In one embodiment, the
retaining member 20 comprises a retaining ring removably coupled to the first end
of the tubular body 15, e.g. by a threaded coupling.
[0041] The retaining system 17 comprises a threaded portion 23 at a second end of the tubular
body 15 coupled to the annular wall 3. In one embodiment, the threaded portion 23
is defined on an outer surface of an externally threaded bushing 25 fitted onto the
second end of the tubular body 15. The bushing 25 is inserted into the threaded through
seat 18 in the annular wall 3 of the combustion chamber 2 to secure the tile holder
10.
[0042] The acoustic damper 12 has a damping volume 30 and a neck 31 that extends at least
in part along a neck axis X2 and is acoustically coupled to the outside of the acoustic
damper 12 through the tubular body 15 of the connector 11. Here, the outside of the
acoustic damper 12 is the inside of the combustion chamber 2.
[0043] The size and shape of the damping volume 30, and the length, the diameter and cross
section of the neck 31 are selected to obtain damping effect in a frequency band as
desired in connection with operation of the combustor 1. In particular, the neck 31
may have any suitable cross-section and the diameter or cross dimension may be either
constant or variable along the neck axis X2. The tubular body 15 has also the function
of extension of the neck 31, so an equivalent neck length that may be considered,
that includes also the length of the tubular body 15.
[0044] The connector axis X1 and the neck axis X2 are transverse to the one another, so
a duct defined by the tubular body 15 and the neck 31 and connecting the combustion
chamber 2 and the damper volume 30 forms a bend 33 at an interface of the neck 31
and the connector 11. The angle between the connector axis X1 and the neck axis X2
may be selected to comply with space occupation requirements. In one embodiment, the
neck 31 is arranged substantially radially with respect to axis A.
[0045] The neck 31 of the acoustic damper 12 comprises a terminal duct 31a, at one end of
which the damping volume 30 is located, and an intermediate duct 31b, between the
tubular body 15 and the terminal duct 31a. In one embodiment, the intermediate duct
31b is coaxial to the terminal duct 31a. The terminal duct 31a and the intermediate
duct 31b comprise respective coupling flanges 31c, 31d for releasable mutual connection.
[0046] The neck 31 is also provided with a securing mechanism 35 configured to secure the
neck 31 to the annular wall 3 of the combustion chamber 2. In one embodiment, the
securing mechanism 35 comprises mounting plates 36, integral with the intermediate
duct 31b of the neck 31 and having mounting holes 37, and screws 38 through the mounting
holes 37. The screws 37 are coupled to respective threaded seats in the outer face
of the annular wall 3. In the embodiment of figure 2 and 3, the screws 37 are parallel
to the neck axis X2 in a portion of the neck 31 at an interface with the tubular body
15. At the interface, the tubular body 15 has a rounded edge 15a coupled to the neck
31, whereby a smooth transition is defined between the tubular body 15 and the neck
31. A belleville washer 39 is arranged between the rounded edge 15a of the tubular
body 15 and the threaded bushing 25. When the screws 37 are tightened to the annular
wall 3, an interface edge of the intermediate duct 31b of the neck 31 is pressed against
the tubular body 15 and the bushing 25 and seals the junction between the connector
11 and the acoustic damper 12.
[0047] In another embodiment of the invention, illustrated in figure 5, the neck 31 of the
acoustic damper 12 is provided with a securing mechanism, here indicated by 135, which
is configured to secure the neck 31 to the annular wall 3 of the combustion chamber
2 and comprises mounting plates 136, integral with the neck 31 and having mounting
holes 137, and screws 138 through the mounting holes 137. The screws 138 are coupled
to respective threaded seats in the outer face of the annular wall 3. In the embodiment
of figure 5, the screws 138 are parallel to the connector axis X1.
[0048] Figure 6 shows another embodiment of the invention. Here, the acoustic damper 12
has a neck 231 with a terminal portion 231a which extend along the neck axis X2 and
an intermediate duct 231b that extends along an intermediate axis X3, which is transverse
both to the connector axis X1 and to the axis. A securing mechanism 235 with screws
238 are parallel to the connector axis X1.
[0049] In the embodiment of figure 7, in combustor 300 of a gas turbine a tile holder 310
comprises a connector 311 and an acoustic damper 312 as described. The tile holder
310 is coupled to a thermoinsulating tiles 308 of refractory material, which has a
through retaining seat 321. Second thermoinsulating tiles 8 with a central hole are
normally present in annular combustion chamber of gas turbines as closure tiles. While
the other second thermoinsulating tiles 308 are slidably inserted along circumferential
guides (as circumferential guides 14 of figure 1), the closure tiles are inserted
last and need to be secured to the annular wall 3 by tile holders. For this reason
such tiles are provided with through holes.
[0050] Finally, it is evident that described modifications and variations can be made to
the tile holder described, without departing from the scope of the present invention,
as defined in the appended claims.
1. A tile holder for a combustor of a gas turbine, comprising:
a connector (11; 311) having a tubular body (15) extending along a first axis (X1)
and a retaining system (17), configured to secure the tubular body (15) in a seat
(18) through a wall (3) and to retain a tile (7; 308) against the wall (3);
an acoustic damper (12; 312) having a damping volume (30) and a neck (31) at least
in part extending along a second axis (X2);
characterized in that the neck (31) is acoustically coupled to the outside through the tubular body (15)
and the first axis (X1) is transverse to the second axis (X2).
2. The tile holder (7; 308) according to claim 1, wherein the retaining system (17) comprises
a retaining member (20) at a tile-coupling end of the tubular body (15), the retaining
member (20) projecting radially outward from the tubular body (15).
3. The tile holder (7; 308) according to claim 2, wherein the retaining member (20) comprises
a retaining ring removably coupled to the tile-coupling end of the tubular body (15).
4. The tile holder (7; 308) according to any one of the preceding claims, wherein the
retaining system (17) comprises a threaded portion (23) at a wall-coupling end of
the tubular body (15).
5. The tile holder (7; 308) according to claim 4, wherein the retaining system (17) comprises
an externally threaded bushing (25) fitted onto the wall-coupling end of the tubular
body (15).
6. The tile holder (7; 308) according to any one of the preceding claims, wherein the
neck (31) comprises a securing mechanism (35) configured to secure the neck (31) to
the wall (3).
7. The tile holder (7; 308) according to claim 6, wherein the securing mechanism (35)
comprises mounting plates (36), integral with the neck (31) and provided with mounting
holes (37), and screws (38) through the mounting holes (37) for connecting to threaded
seats in the wall (3).
8. The tile holder (7; 308) according to claim 7, wherein the screws (38) are parallel
to the first axis (X1) of the tubular body (15) or the screws (38) are parallel to
a portion of the neck (31) at an interface with the tubular body (15).
9. The tile holder (7; 308) according to any one of the preceding claims, wherein the
neck (31) of the acoustic damper (12; 312) comprises a terminal duct (31a), having
the damping volume (30) at one end, and an intermediate duct (31b), between the tubular
body (15) and the terminal duct (31a).
10. The tile holder (7; 308) according to claim 9, wherein the intermediate duct (31b)
is coaxial to the terminal duct (31a).
11. The tile holder (7; 308) according to claim 10, wherein the intermediate duct (31b)
extends along a third axis (X3) which is transverse to the first axis (X1) and to
the second axis (X2).
12. The tile holder according to any one of claims 9 to 11, wherein the terminal duct
(31a) and the intermediate duct (31b) comprise respective coupling flanges (31c, 31d)
for releasable mutual connection.
13. The tile holder according to any one of claims 9 to 12, wherein the tubular body (15)
has a rounded edge (15a) coupled to the neck (31), whereby a smooth transition is
defined between the tubular body (15) and the neck (31).
14. A combustor of a gas turbine comprising a combustion chamber (2), having a shell defined
by a wall (3) and a heat-shield (5) on an inner surface of the wall (3), wherein the
heat-shield (5) comprises a plurality of tiles and at least one damper connection
tile (7; 308) is retained against the wall (3) by a tile holder (10) according to
any one of the preceding claims.
15. The combustor according to claim 14, wherein the wall (3) has a through seat (18)
and the connector (11; 311) of the tile holder (10) is fitted in the through seat
(18).
16. The combustor according to claim 14 or 15, wherein the damper connection tile (7;
308) has a rim (22) that delimits at least a portion of a through seat (18) and the
connector (11; 311) engages the rim (22) to retain the damper connection tile (7;
308) against the wall (3).
1. Plattenhalter für einen Brenner einer Gasturbine, der Folgendes umfasst:
ein Verbindungsstück (11; 311), das einen röhrenförmigen Körper (15), der sich entlang
einer ersten Achse (X1) erstreckt, und ein Haltesystem (17), das konfiguriert ist,
den röhrenförmigen Körper (15) in einer durch eine Wand (3) verlaufenden Aufnahme
(18) zu befestigen und eine Platte (7; 308) gegen die Wand (3) zu halten, aufweist;
und
einen Schalldämpfer (12; 312), der ein Dämpfungsvolumen (30) und einen Hals (31) aufweist,
der sich zumindest teilweise entlang einer zweiten Achse (X2) erstreckt;
dadurch gekennzeichnet, dass der Hals (31) durch den röhrenförmigen Körper (15) mit der Außenseite akustisch gekoppelt
ist und die erste Achse (X1) quer zu der zweiten Achse (X2) ist.
2. Plattenhalter (7; 308) nach Anspruch 1, wobei das Haltesystem (17) an einem mit der
Platte koppelnden Ende des röhrenförmigen Körpers (15) ein Halteelement (20) umfasst,
wobei das Halteelement (20) von dem röhrenförmigen Körper (15) radial nach außen vorsteht.
3. Plattenhalter (7; 308) nach Anspruch 2, wobei das Halteelement (20) einen Haltering
umfasst, der an das mit der Platte koppelnde Ende des röhrenförmigen Körpers (15)
lösbar gekoppelt ist.
4. Plattenhalter (7; 308) nach einem der vorhergehenden Ansprüche, wobei das Haltesystem
(17) an einem mit der Platte koppelnden Ende des röhrenförmigen Körpers (15) einen
mit einem Gewinde versehenen Abschnitt (23) aufweist.
5. Plattenhalter (7; 308) nach Anspruch 4, wobei das Haltesystem (17) eine mit einem
Außengewinde versehene Buchse (25) umfasst, die an dem mit der Platte koppelnden Ende
des röhrenförmigen Körpers (15) angebracht ist.
6. Plattenhalter (7; 308) nach einem der vorhergehenden Ansprüche, wobei der Hals (31)
einen Befestigungsmechanismus (35) umfasst, der konfiguriert ist, den Hals (31) an
der Wand (3) zu befestigen.
7. Plattenhalter (7; 308) nach Anspruch 6, wobei der Befestigungsmechanismus (35) Montageplatten
(36), die mit dem Hals (31) einteilig ausgebildet sind und mit Montagelöchern (37)
versehen sind, und Schrauben (38) durch die Montagelöcher (37) umfasst, um sie mit
den mit Gewinde versehenen Aufnahmen in der Wand (3) zu verbinden.
8. Plattenhalter (7; 308) nach Anspruch 7, wobei die Schrauben (38) zu der ersten Achse
(X1) des röhrenförmigen Körpers (15) parallel sind oder die Schrauben (38) an einer
Grenzfläche mit dem röhrenförmigen Körper (15) zu einem Abschnitt des Halses (31)
parallel sind.
9. Plattenhalter (7; 308) nach einem der vorhergehenden Ansprüche, wobei der Hals (31)
des Schalldämpfers (12; 312) einen Anschlusskanal (31a), an dessen einem Ende sich
das Dämpfungsvolumen (30) befindet, und einen Zwischenkanal (31b) zwischen dem röhrenförmigen
Körper (15) und dem Anschlusskanal (31a) umfasst.
10. Plattenhalter (7; 308) nach Anspruch 9, wobei der Zwischenkanal (31b) koaxial zu dem
Anschlusskanal (31a) ist.
11. Plattenhalter (7; 308) nach Anspruch 10, wobei sich der Zwischenkanal (31b) entlang
einer dritten Achse (X3) erstreckt, die quer zu der ersten Achse (X1) und zu der zweiten
Achse (X2) ist.
12. Plattenhalter (7; 308) nach einem der Ansprüche 9 bis 11, wobei der Anschlusskanal
(31a) und der Zwischenkanal (31b) zur lösbaren gegenseitigen Verbindung jeweils Kopplungsflansche
(31c, 31d) aufweisen.
13. Plattenhalter (7; 308) nach einem der Ansprüche 9 bis 12, wobei der röhrenförmige
Körper (15) eine abgerundete Kante (15a) aufweist, die mit dem Hals (31) verbunden
ist, wobei zwischen dem röhrenförmigen Körper (15) und dem Hals (31) ein glatter Übergang
definiert ist.
14. Brenner einer Gasturbine, der eine Brennkammer (2) umfasst, die eine Hülle, die durch
eine Wand (3) definiert ist, und einen Hitzeschild (5) auf einer Innenfläche der Wand
(3) aufweist, wobei der Hitzeschild (5) mehrere Platten umfasst und mindestens eine
Dämpferverbindungsplatte (7; 308) durch einen Plattenhalter (10) nach einem der vorhergehenden
Ansprüche gegen die Wand (3) gehalten wird.
15. Brenner nach Anspruch 14, wobei die Wand (3) eine Durchgangsaufnahme (18) aufweist
und das Verbindungsstück (11; 311) des Plattenhalters (10) in der Durchgangsaufnahme
(18) angebracht ist.
16. Brenner nach Anspruch 14 oder 15, wobei die Dämpferverbindungsplatte (7; 308) einen
Kranz (22) aufweist, der zumindest einen Teil einer Durchgangsaufnahme (18) begrenzt,
und das Verbindungsstück (11; 311) mit dem Kranz (22) in Eingriff ist, um die Dämpferverbindungsplatte
(7; 308) gegen die Wand (3) zu halten.
1. Support de tuile pour le brûleur d'une turbine à gaz comprenant :
un connecteur (11 ; 311) avec un corps tubulaire (15) se prolongeant le long d'un
premier axe (X1) et un système de retenue (17), configuré pour fixer le corps tubulaire
(15) dans une assise (18) à travers une paroi (3) et pour maintenir une tuile (7 ;
308) contre la paroi (3) ;
un absorbeur acoustique (12 ; 312) avec un volume d'absorption (30) et une couronne
(31) se prolongeant au moins en partie le long d'un second axe (X2) ;
caractérisé par le fait que la couronne (31) est reliée acoustiquement sur l'extérieur à travers le corps tubulaire
(15) et le premier axe (X1) est transversal par rapport au second axe (X2).
2. Support de tuile (7 ; 308) selon la revendication 1, dans lequel le système de retenue
(17) comprend un élément de retenue (20) à une extrémité de couplage de tuile du corps
tubulaire (15), l'élément de retenue (20) se projetant de façon radiale vers l'extérieur
du corps tubulaire (15).
3. Support de tuile (7 ; 308) selon la revendication 2, dans lequel l'élément de retenue
(20) comprend une bague de retenue couplée, de façon amovible, à l'extrémité de couplage
de tuile du corps tubulaire (15).
4. Support de tuile (7 ; 308) selon l'une quelconque des revendications précédentes,
dans lequel le système de retenue (17) comprend une partie filetée (23) sur une extrémité
de couplage de paroi du corps tubulaire (15).
5. Support de tuile (7 ; 308) selon la revendication 4, dans lequel le système de retenue
(17) comprend une bague (25) filetée à l'extérieur installée sur l'extrémité de couplage
de paroi du corps tubulaire (15).
6. Support de tuile (7 ; 308) selon l'une quelconque des revendications précédentes,
dans lequel la couronne (31) comprend un mécanisme de fixation (35) configuré pour
fixer la couronne (31) sur la paroi (3).
7. Support de tuile (7 ; 308) selon la revendication 6, dans lequel le mécanisme de fixation
(35) comprend des plaques de montage (36), faisant partie intégrante de la couronne
(31) et dotées d'orifices de montage (37), et de vis (38) à travers les orifices de
montage (37) pour la connexion à des sièges filetés dans la paroi (3).
8. Support de tuile (7 ; 308) selon la revendication 7, dans lequel les vis (38) sont
parallèles au premier axe (X1) du corps tubulaire (15) ou les vis (38) sont parallèles
à une partie de la couronne (31) sur une interface avec le corps tubulaire (15).
9. Support de tuile (7 ; 308) selon l'une quelconque des revendications précédentes,
dans lequel la couronne (31) de l'absorbeur acoustique (12 ; 312) est constituée d'un
conduit terminal (31a), ayant le volume d'absorption (30) sur une extrémité, et un
conduit intermédiaire (31b), entre le corps tubulaire (15) et le conduit terminal
(31a).
10. Support de tuile (7 ; 308) selon la revendication 9, dans lequel le conduit intermédiaire
(31b) est coaxial au conduit terminal (31a).
11. Support de tuile (7 ; 308) selon la revendication 10, dans lequel le conduit intermédiaire
(31b) se prolonge le long d'un troisième axe (X3) qui est transversal par rapport
au premier axe (X1) et au second axe (X2).
12. Support de tuile (7 ; 308) selon l'une quelconque des revendications 9 à 11, dans
lequel le conduit terminal (31a) et le conduit intermédiaire (31b) comprennent des
brides d'accouplement respectives (31c, 31d) pour la connexion mutuelle séparable.
13. Support de tuile (7 ; 308) selon l'une quelconque des revendications 9 à 12, dans
lequel le corps tubulaire (15) comprend un bord arrondi (15a) couplé à la couronne
(31), par lequel une transition lisse est définie entre le corps tubulaire (15) et
la couronne (31).
14. Brûleur de turbine à gaz comprenant une chambre de combustion (2), ayant une coque
définie par une paroi (3) et un bouclier thermique (5) sur une surface interne de
la paroi (3), dans lequel le bouclier thermique (5) comprend plusieurs tuiles et au
moins une tuile de connexion d'absorbeur (7 ; 308) est maintenue contre la paroi (3)
par un support de tuile (10) selon l'une quelconque des revendications précédentes.
15. Brûleur selon la revendication 14, dans lequel la paroi (3) comprend une assise traversante
(18) et le connecteur (11 ; 311) du support de tuile (10) est fixé dans l'assise traversante
(18).
16. Brûleur selon la revendication 14 ou 15, dans lequel la tuile de connexion d'absorbeur
(7 ; 308) présente un bord (22) qui délimite au moins une partie d'une assise traversante
(18) et dans lequel le connecteur (11 ; 311) s'engage dans le bord (22) pour maintenir
la tuile de connexion d'absorbeur (7 ; 308) contre la paroi (3).