U.S. patent application number 10/837007 was filed with the patent office on 2005-11-03 for hot gas seal.
Invention is credited to Dahlke, Stefan, Eng, Jesse, Glessner, John Carl, Hofmann, Daniel, Liebe, Roland, Tamaddoni-Jahromi, Kenneth Michael.
Application Number | 20050242526 10/837007 |
Document ID | / |
Family ID | 35186274 |
Filed Date | 2005-11-03 |
United States Patent
Application |
20050242526 |
Kind Code |
A1 |
Dahlke, Stefan ; et
al. |
November 3, 2005 |
Hot gas seal
Abstract
An inventive hot gas seal comprises a sealing body and means for
allowing a cooling fluid, preferably cooling air, to flow through
the interior of the sealing body. Such a hot gas seal can be
effectively cooled by guiding a cooling fluid through the interior
of the sealing body.
Inventors: |
Dahlke, Stefan; (Bechen,
DE) ; Eng, Jesse; (Jupiter, FL) ; Glessner,
John Carl; (Oviedo, FL) ; Hofmann, Daniel;
(Orlando, FL) ; Liebe, Roland; (Monheim, DE)
; Tamaddoni-Jahromi, Kenneth Michael; (Orlando,
FL) |
Correspondence
Address: |
Siemens Corporation
Intellectual Property Department
170 Wood Avenue South
Iselin
NJ
08830
US
|
Family ID: |
35186274 |
Appl. No.: |
10/837007 |
Filed: |
April 30, 2004 |
Current U.S.
Class: |
277/605 |
Current CPC
Class: |
F23M 5/00 20130101; F01D
25/12 20130101; F23R 2900/00012 20130101; F23R 3/002 20130101; F01D
11/005 20130101; F16J 15/064 20130101; F23M 2900/05005 20130101;
F05D 2300/21 20130101; F05D 2260/20 20130101; F05D 2300/612
20130101 |
Class at
Publication: |
277/605 |
International
Class: |
F01D 005/14 |
Claims
What is claimed is:
1. A hot gas seal comprising a sealing body and means for allowing
a cooling fluid to flow through the interior of the sealing
body.
2. The hot gas seal claimed in claim 1, in which at least one
cooling channel extending through the interior of the sealing body
is formed as said means for allowing a cooling fluid to flow
through the interior of the sealing body.
3. A hot gas seal which comprises a sealing body, the sealing body
being shaped in a tube like manner such that it comprises a
generally circumferential portion and an interior space surrounded
by the circumferential portion which defines a cooling channel for
allowing a cooling fluid to flow through the interior of the tube
like shaped sealing body.
4. The hot gas seal as claimed in claim 1, in which the sealing
body is made from a porous material the pores of which are
interconnected so that they form said means for allowing a cooling
fluid to flow through the interior of the sealing body.
5. The hot gas seal as claimed in claim 4, in which the porous
material is an elastic material.
6. The hot gas seal as claimed in claim 5, in which the elastic
material is a ceramic material.
7. The hot gas seal as claimed in claim 5, in which the elastic
material is a metal foam.
8. The hot gas seal as claimed in claim 5, in which the elastic
porous material is a polymer material.
9. A hot gas seal assembly comprising a hot gas seal which
comprises a sealing body in which at least one cooling channel
extending through the interior of the sealing body is formed as a
means for allowing a cooling fluid to flow through the interior of
the sealing body and which further comprises means arranged outside
of the hot gas seal for channeling a cooling fluid flow at least
partly through the cooling channel of the hot gas seal.
10. The hot gas seal assembly claimed in claim 9, in which the
means for channeling the cooling fluid through the cooling channel
are designed such that a high static pressure is built up in front
of them which channels the cooling fluid at least partly through
the cooling channel.
11. The hot gas seal assembly claimed in claim 10, in which a
fixing bolt for fixing a heat shield element is used for building
up said high static pressure.
12. The hot gas seal assembly claimed in claim 9, comprising a
means arranged outside of the hot gas seal for guiding the cooling
fluid which has flown through the cooling channel back into the
cooling fluid flow.
13. The hot gas seal assembly claimed in claim 12, in which the
mans for guiding the cooling fluid back into the cooling fluid flow
are designed such that a high static pressure is built up in front
of them which guides the cooling fluid back into the cooling fluid
flow.
14. The hot gas seal assembly claimed in claim 13, in which a
fixing bolt for fixing a heat shield element is used for building
up said high static pressure.
Description
FIELD OF THE INVENTION
[0001] The present invention relates to a hot gas seal and a hot
gas seal assembly.
BACKGROUND OF INVENTION
[0002] Walls of high temperature gas reactors, e.g. the walls of
turbine combustion chambers, need to be shielded by a suitable
thermal shield against attack of the hot gas. The thermal shielding
can be achieved by providing a hot gas resistant liner, which
usually comprises a number of shield elements covering the wall to
be shielded. The heat shield elements can e.g. be implemented in
form of ceramic heat shield elements (CHS elements) or in form of
suitable metallic heat shield elements. To allow for thermal
expansion when being exposed to the hot gas, the heat shield
elements are arranged such that gaps are left between neighboring
heat shield elements. In order to prevent hot gas from passing
through these gaps from the hot gas side of a heat shield, e.g. to
a carrier structure to which the heat shield elements are fixed,
gaps would need purging with air to avoid over-heating. This air is
costly leakage.
[0003] In EP 1 302 723 A1 it is proposed to seal gaps between heat
shield elements with sealing elements to prevent hot gas from
passing the gaps. This sealing elements my be cooled.
SUMMARY OF THE INVENTION
[0004] It is an object of the present invention to provide a hot
gas seal and a hot gas seal assembly by which the cooling of the
hot gas seal can be improved.
[0005] The first object is solved by a hot gas seal as claimed in
claim 1, the second object is solved by a hot gas seal assembly as
claimed in claim 11.
[0006] An inventive hot gas seal comprises a sealing body and means
for allowing a cooling fluid, preferably cooling air, to flow
through the interior of the sealing body.
[0007] Such a hot gas seal can be effectively cooled by guiding a
cooling fluid through the interior of the sealing body.
[0008] In a first embodiment of the present invention, at least one
cooling channel is formed to extend through the interior of the
sealing body as said means for allowing a cooling fluid to flow
through the interior of the sealing body.
[0009] In the first embodiment, the sealing body may be shaped in a
tube like manner such that it comprises a circumferential portion
and an interior space surrounded by said circumferential portion
which defines a cooling channel for allowing a cooling fluid to
flow through the interior of the tube like shaped sealing body.
[0010] In a second embodiment of the inventive hot gas seal, the
sealing body is made from a porous material the pores of which are
inter-connected so that the pores form said means for allowing a
cooling fluid to flow through the interior of the sealing body.
Such a porous material allows for an effective distribution of the
cooling air in the interior of the sealing body and, therefore, for
evenly cooling the hot gas seal.
[0011] In an advantageous development of the second embodiment, the
porous material is an elastic porous material. Such a hot gas seal
can be fixed between neighboring heat shield elements by spring
forces. As the elastic porous material, a ceramic material, metal
foam, or a suitable polymer material may be used. The choice of the
material to be used may depend on the temperatures of the hot gas
which is to be prevented from passing through the gaps between two
heat shield elements.
[0012] A hot gas seal assembly according to the invention comprises
a hot gas seal which comprises a sealing body in which at least one
cooling channel extending through the interior of the sealing body
is formed as a means for allowing a cooling fluid to flow through
the interior of the sealing body. The inventive hot gas seal
assembly further comprises means which are arranged outside of the
hot gas seal for channeling a cooling fluid flow, preferably a
cooling air flow, at least partly through the cooling channel of
the hot gas seal. By providing such means a highly efficient
cooling of the hot gas seal of the assembly is possible.
[0013] The means for channeling cooling fluid through the cooling
channel may be designed such that a high static pressure is build
up in front of them which channels the cooling fluid at least
partly through the cooling channel.
[0014] The inventive hot gas seal assembly may further comprise a
means arranged outside the hot gas seal for guiding the cooling
fluid which has flown through the cooling channel back into the
cooling fluid flow. Such a means may be designed such that a high
static pressure is build up in front of them which guides the
cooling fluid back into the cooling fluid flow.
[0015] As a means for building up high static pressure, a fixing
bolt for fixing a heat shield element or any other flow restriction
may be used.
[0016] Further features, properties, and advantages of the present
invention are described hereinafter with reference to the
accompanying drawings, by means of detailed embodiments.
BRIEF DESCRIPTION OF THE DRAWINGS
[0017] FIG. 1 shows a first embodiment of the inventive hot gas
seal.
[0018] FIG. 2 shows a modification of the inventive hot gas seal of
the first embodiment.
[0019] FIG. 3 shows a further development of the inventive hot gas
seal of the first embodiment.
[0020] FIG. 4 shows a second embodiment of the inventive hot gas
seal.
[0021] FIG. 5 shows an embodiment of the inventive hot gas seal
assembly.
DETAILED DESCRIPTION OF INVENTION
[0022] A first embodiment of the inventive hot gas seal is shown in
FIG. 1. The figure shows, in a schematic fashion, a first heat
shield element 10 comprising a first front face 12 in which a first
grove 14 is arranged and a second heat shield element 16 having a
second front face 18 in which a second grove 20 is arranged. The
heat shield elements 10, 16 are arranged such that the first front
face 12 and the second front face 18 are disposed opposite to each
other with the first grove 14 and the second grove 20 forming a
space for accommodating an inventive hot gas seal 22, therein.
[0023] The hot gas seal 22 comprises a sealing body 24 which has a
tube-like shape. The interior of the sealing body 24 forms a
cooling channel 26 for allowing a cooling fluid, which in the
present embodiment is cooling air, to flow through the hot gas seal
22. In the present embodiment, the sealing body 24 comprises a
ceramic portion 28 as a highly heat resistant portion.
[0024] The hot gas seal 22 is arranged such in the space formed by
the first grove 14 and the second grove 20 that the ceramic portion
28 shows towards the hot gas side of the liner, i.e. the sides of
the heat shield elements which are disposed to the hot gas.
[0025] Inside the cooling channel 26, an axial flow of cooling air
30 and a convective cooling air flow which originates from the
axial flow 30 and flows clockwise and counter-clockwise along the
wall of cooling channel towards the center of the ceramic portion
28 (indicated by arrows) are provided. At the center of the ceramic
portion 28, the convective cooling air flow is directed back
towards the axial cooling air flow 30. With the described hot gas
seal, an effective cooling of the ceramic portion, which is
disposed to the hot gas, is possible.
[0026] A modification of the first embodiment is shown in FIG. 2.
Again, a hot gas seal 122 is arranged in a space formed by groves
114 and 120 which are arranged in first and second front faces 112
and 118 of first and second heat shield elements 110, 116,
respectively. The modification differs from the first embodiment in
the cross-sectional shape of the groves 114, 120, the hot gas seal
122, and the cooling channel 126. As shown in FIG. 2, the
cross-sectional shape of the sealing body 124 and the cooling
channel 126 is chosen to be heart like with the ceramic portion 128
lying opposite to an apex like portion 123 and being indented at
its center part towards said apex like portion 123.
[0027] In the modification shown in FIG. 2, the axial cooling air
flow 130 takes place close to the apex like portion 123 of the
cross-section of the cooling channel. Like in FIG. 1, a clockwise
and a counter-clockwise convective cooling air flow (indicated by
arrows) takes place along the inner walls of the sealing body 124.
However, compared to the cross-sectional shape of the cooling
channel in FIG. 1, the re-direction of the convective cooling air
flow towards the axial cooling air flow 130 is improved.
[0028] A further development of the first embodiment is shown in
FIG. 3. FIG. 3 shows a hot gas seal 222 comprising a sealing body
224 which forms a tube with the interior of the tube forming a
cooling channel 226 for allowing cooling air to flow through the
hot gas seal 222. In difference to the hot gas seals shown in FIGS.
1 and 2, the hot gas seal of FIG. 3 does not comprise a ceramic
portion. Instead, it comprises ceramic or metallic balls 228 or a
ceramic or metallic powder which are/is arranged in an elastic
matrix 224 which forms the sealing body. In the hot gas seal 222
shown in FIG. 3, due to the ceramic or metallic balls 228 or the
ceramic or metallic powder, the sealing body is elastic and shows a
good sealing ability.
[0029] A second embodiment of the present invention is shown in
FIG. 4. In FIG. 4, a first heat shield element 310, a second heat
shield element 312 and a hot gas seal 322 are shown in a schematic
fashion. The first heat shield element 310 and the second heat
shield element 318 comprise a first front face 312 and a second
front face 316, respectively. They further comprise a first hot gas
side 313 and a second hot gas side 317.
[0030] In the second liner 318, a recess 320 is formed in the
second front face 316 at the edge to the hot gas side 317. The heat
shield elements 310, 318 are arranged such that the front faces
312, 316 are disposed opposite to each other and that the recess
320 forms, together with the first front face 312, a space for a
accommodating therein the hot gas seal 322 according to the second
embodiment.
[0031] Through the gap 331 between the first front face 312 and the
second front face 316, a cooling air flow 332 outgoing from a
carrier structure flows towards the hot gas side of the liner.
[0032] The sealing body 324 of the hot gas seal 322 is made from a
porous material the pores of which are interconnected such that
they form channels through which the cooling air of the cooling air
flow 332 can pass through the hot gas seal. Thus, the cooling air
can flow through the hot gas seal 322.
[0033] In addition, the material of the sealing body 324 is an
elastic material, so that the hot gas seal 322 is held in place by
spring forces which act on the first front face 312 and the part of
the recess 320 which lies opposite to the first front face 312. As
elastic material, all materials which are suitable for being
disposed to a hot gas can be used. Examples for such materials are
porous ceramics, like abradable TBC, metal foams or polymeric
materials.
[0034] An embodiment for an inventive hot gas seal assembly 400 is
shown in FIG. 5. The figure shows, in a schematic fashion, a heat
shield element 410 which is fixed by means of hooks (not shown) and
fixing bolts 434, 436 of a generally cylindrical cross section. The
fixing bolts 434, 436 are arranged in front of and behind a hot gas
seal 422, e.g. a hot gas seal as described with respect to FIG. 3.
Due to the high static pressure built up in front of the fixing
bolt 434, the cooling air 432 is partly guided into the cooling
channel of the hot gas seal 422. After passing through the hot gas
seal 422, the cooling air is guided back into the cooling air flow
432 by a low static pressure built up in behind of the fixing bolt
436.
[0035] Although in the shown embodiment for the hot gas seal
assembly the fixing bolts 434, 436 are used to build up high and
low static pressure, other means could be used as well as long as
they allow for building up a high pressure in front of and a low
pressure behind the hot gas seal 422.
* * * * *