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Sommaire du brevet 2118178 

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Disponibilité de l'Abrégé et des Revendications

L'apparition de différences dans le texte et l'image des Revendications et de l'Abrégé dépend du moment auquel le document est publié. Les textes des Revendications et de l'Abrégé sont affichés :

  • lorsque la demande peut être examinée par le public;
  • lorsque le brevet est émis (délivrance).
(12) Demande de brevet: (11) CA 2118178
(54) Titre français: METHODE ET APPAREIL POUR PRODUIRE DES GAZ SERVANT A FAIRE FONCTIONNER UNE TURBINE A GAZ
(54) Titre anglais: METHOD AND APPLIANCE FOR GENERATING GASES FOR OPERATING A GAS TURBINE
Statut: Réputée abandonnée et au-delà du délai pour le rétablissement - en attente de la réponse à l’avis de communication rejetée
Données bibliographiques
(51) Classification internationale des brevets (CIB):
  • F02C 1/08 (2006.01)
  • F01K 23/00 (2006.01)
  • F01K 23/10 (2006.01)
  • F02C 3/26 (2006.01)
  • F02C 3/34 (2006.01)
  • F02C 7/224 (2006.01)
  • F02C 9/38 (2006.01)
(72) Inventeurs :
  • LEITHNER, REINHARD (Allemagne)
(73) Titulaires :
  • ALSTOM ENERGY SYSTEMS GMBH
(71) Demandeurs :
  • ALSTOM ENERGY SYSTEMS GMBH (Allemagne)
(74) Agent: ROBIC AGENCE PI S.E.C./ROBIC IP AGENCY LP
(74) Co-agent:
(45) Délivré:
(22) Date de dépôt: 1994-10-14
(41) Mise à la disponibilité du public: 1995-04-16
Licence disponible: S.O.
Cédé au domaine public: S.O.
(25) Langue des documents déposés: Anglais

Traité de coopération en matière de brevets (PCT): Non

(30) Données de priorité de la demande:
Numéro de la demande Pays / territoire Date
P 43 35 136.0 (Allemagne) 1993-10-15

Abrégés

Abrégé anglais


11
Abstract
In the method, the raw gas flowing out of the com-
bustion chamber - when the temperature is above the
melting temperature of the ash - is first cooled by
recirculated exhaust gas and/or air and/or oxygen to
under the ash melting point temperature but above the
gas turbine inlet temperature, is subsequently further
cooled to approximately 650-950 °C by giving up heat to
the clean gas and by admixture of recirculated exhaust
gas and/or air and/or oxygen, is cleaned at this tem-
perature by known methods from dust, including alkali
metal compounds, SO2 and NOx, is again heated as clean
gas to the permissible gas turbine inlet temperature by
taking up heat from the raw gas and then flows through
a gas turbine and, subsequently, a waste heat steam
generator, in which water for operating a steam turbine
of one or more pressure stages is preheated, evaporated
and superheated.
The method is distinguished by particularly high
efficiencies for the electrical current generators.

Revendications

Note : Les revendications sont présentées dans la langue officielle dans laquelle elles ont été soumises.


Patent claims
1. A method for generating gases for operating a
gas turbine in a combined gas turbine and steam turbine
power station, in which fine-grained to pulverized coal
is almost completely burned at a pressure greater than
1 bar and a temperature greater than 1000 °C with air,
with air enriched with oxygen or with pure oxygen alone
or mixed with recirculated exhaust gas in each case to
form a combustion gas which consists essentially of CO2
and steam and, when air is used, also of nitrogen, and
which is subsequently cleaned at least from dust
including alkali metal compounds and possibly from SO2
and NOX, which combustion gas flows in sequence through
a gas turbine and a waste heat steam generator in which
water for operating a steam turbine is preheated,
evaporated and superheated at one or a plurality of
pressure stages, wherein combustion gas = raw gas
flowing from the combustion chamber is cooled to
approximately 650-950 °C, by rejecting heat to the
clean gas and by subsequent admixture via the
connecting piece of recirculated exhaust gas or a gas
similar to that used for combustion, and is cleaned at
this temperature, using known methods such as cyclones
or ceramic filters, at least from dust including alkali
metal compounds and possibly from SO2 and/or NOx by
likewise known methods, for example the supply of lime
dust (dry additive method) and ammonia (SNCR method),
and is heated again to the permissible gas turbine
inlet temperature as clean gas by acceptance of heat
from raw gas.

2. The method for generating gases as claimed in
claim 1, wherein the combustion in the combustion
chamber is carried out above the gas turbine inlet tem-
perature and below the ash melting point by correspond-
ing air and/or oxygen surplus and/or exhaust gas recir-
culation so that the ash can be withdrawn in dust form
via the ash outlet connecting piece.
3. The method for generating gases as claimed in
claim 1, wherein combustion in the combustion chamber
takes place at such temperatures that the ash is with-
drawn in a molten state via the ash outlet connecting
piece and the combustion gas at the outlet from the
combustion chamber is cooled to a temperature below the
ash melting point but above the permissible gas outlet
temperature by admixture via the connecting piece of
recirculated exhaust gas or a gas similar to that used
for combustion.
4. An appliance for carrying out the method as
claimed in claim 1, wherein the combustion chamber is
configured as a cyclone combustion chamber, the inside
of the walls of the combustion chamber pressure vessel,
of the connecting conduit and of the heat exchanger
pressure vessel are respectively provided with a ther-
mal insulation and a jacket, the jacket being con-
figured as a heat exchanger which has sequentially con-
nected ducts, and the last duct is connected, if appro-
priate, via a heat exchanger by the outlet connecting
piece of the cleaning pressure vessel and, if appropri-
ate, a heat exchanger is arranged in the heating

surface space of the heat exchanger pressure vessel,
the inside of the enclosing walls of the connecting
piece conduits and of the gas cleaning pressure vessel
being provided with thermal insulation.
5. The appliance for carrying out the method, as
claimed in claim 4, wherein the gas cleaning pressure
vessel is provided with a filter which is configured as
a fabric filter.
6. The appliance for carrying out the method, as
claimed in claims 4 and 5, wherein the gas cleaning
pressure vessel is provided with a filter which is con-
figured as a ceramic filter.
7. The appliance for carrying out the method, as
claimed in claims 4 to 6, wherein the sequentially con-
nected ducts are each formed by a plurality of ducts
arranged in parallel.
8. The appliance for carrying out the method, as
claimed in claims 4 to 7, wherein the jacket is fire-
resistant, substantially impermeable to gas and ther-
mally conducting.
9. The appliance for carrying out the method, as
claimed in claims 4 to 8, wherein the connecting con-
duit to the gas cleaning pressure vessel or to the gas
cleaning pressure vessels is provided with an appliance
for spraying in additives.

Description

Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.


^- ~118178
The invention relates to a method, and an appli-
ance for carrying out the method, for generating ga~es
for operating a gas turbine in a combined gas turbine
and ~team turbine power station, in which fine-grained
to pulverized coal ic almost completely burned at a
pres~ure greater than 1 bar and a temperature greater
than 1000 C with air, with air enriched with oxygen or
with pure oxygen alone or mixed with recirculated
exhaust gas in each case to form a combustion gas which
consists essentially of C02 and steam and, when air is
used, also of ni~rogen, and which i8 subsequently
cleaned at least from dust including alkali metal
compounds and possibly from S02 and N0x, which
combustion gas flows in sequence through a gas turbine
and a waste heat steam generator in whiah water for
operating a steam turbine is preheated, evaporated and
superheated at one or a plurality of pressure stages.
Such installations have become known from the
journal VGB Xraftwerkstechnik (70) 1990, No. 5,
Pages 399-406, inter alia. The gases generated contain
pollutant materials which would damage the gas turbine
and a gas cleaning system is therefore absolutely
necessary. Because it is scarcely possible to carry
out effectivè cleaning of such hot, pollutant-laden
gases with temperatures above the permissible entry

: 21182178
temperature of modern gas turbine~, i.e. above 1200 C,
the temperature of the gases must be reduced to a level
of approximately 650-950 C co that the gas cleaning
can be carried out by known and tested methods. Thi~
temperature level i8, in partiaular, also decisive for
the dry additive method (desulphurization by spraying
in lime dust) and the selective non-catalytic reduction
- SNCR - method (reduction of the oxide~ of nitrogen by
ammonia or a catalyzer). In order to achieve this tem~
perature level, heat is generally removed in a steam
:: ~ .
power process or the sy3tem i~ operated with a very
high level of excess air.
In the known method - removing heat in a steam
: . . -:
process or operating with a high level of excess air -
disadvantageous features are the 1088 of efficiency due
to the heat transfer to the steam process at a rela-
tively low temperature or due to the reduced gas tur-
bine inlet temperature in the ca~e of a high level of
excess air and the increased exhaust gas lo~ses. The
coupling of gas turbine operation and waste heat boiler
operation is also disadvantageous.
As a consequence of the discussion ahout the
climate, of environmental protection and of the preser-
vation of resources, the not unsubstantial increase in
efficiency due to the method proposed and the appliance
proposed have gained great importance, particularly in
recent years.
The objec~ of the invention i8 to create a method
of the type de~cribed at the beginning and the

2118178
associated appliance in which the disadvant2ges
described are avoided and a decisive improvement to the
efficiency i8 aahieved in the generation of electrical
current from coal. This object is achieved by means of
the characterizing part of Patent Claim 1.
Advantageous embodiments of the invention may be
taken from the su~-claims 2 to 9.
The following advantages relative to the known
prior art are achieved by mean~ of the measures accord-
ing to the invention:
1) Higher clean gas temperatures (1200-1400 C) can
be achieved 80 that gas turbine~ can be operated
with higher inlet temperatures and correspondingly
higher efficiency.
2) The heat losses relative to the prior art are
smaller due to the raw gas/clean gas heat exchange
and the efficiency of the overall installation is
improved by this means.
3) The gas turbine can be operated with its own chim-
ney independently of the waste heat boiler.
.5 4) The internal insulation of the pressure ves3elsand the connecting conduits, which are necessary
in any case, is simultaneously used as a heat
exchanger and the temperature of the pressure ves-
sels and the connecting conduit walls is reduced

--J ~118178 ~ ~
for the same in~ulation thickne~s. Under certain
circumstances, it is possible to dispense with the
separate heat exchanger (15 in Figure 2).
.
The invention is explained in more detail using
the description and Figures 1 and 2.
Figure 1 show3 a combined gas turbine and steam
turbine power station which includes the installation
complex 31-37, namely the compressor for exhaust gas
31, the compressor for air or for air enriched with
oxygen or for pure oxygen 32, the combu~tion chamber
33, the heat exchanger 34, the gas cleaning system 35,
the gas turb,ine ~with electrical generator) 36 and the
wa~te heat steam generator (including steam turbine and
electrical generator) 37.
Figure 2 shows the installation parts 33, 34 and
35, fine-grained to pulverized coal under pressure, for
example 16 bar, together with air or with air enriched
with oxygen ox with pure oxygen alone or with recircu-
lated exhaust gas in each case being supplied via theconnecting piece 11 to the combustion chamber 27 and
'being burned in the latter. The combustion then takes
place either at a temperature at which the ash remains
solid or at a temperature at which the ash can be witih-
drawn in the molten state. The combustion temperaturecan be adjusted by the selection of the air excess
and/or oxygen excess and~or exhaust gas recirculation.
The combustion chamber 27 is of cyclone type 90 that a
major proportion of the ash can be precipitated and

: --- 211817~
extracted via the connecting piece 14. If the combus-
tion temperature in the combustion chamber is above the
ash melting point, the combustion gas at the outlet
connecting piece of the combustion chamber 12 is cooled
to a temperature below the a h melting point by admix-
ture of recirculated exhaust gas or a gas similar to
that used for combustion (via the connecting piece 25)
in order to avoid slagging of the subsequent conduit
and of the heat exchanger. In both cases (solid or
molten ash in the combu~tion chamber), the combustion
gases (~ raw gases) then flow through the connecting
conduits 2, which are configured as a heat exchanger~
and - if necessary - via the raw gas inlet connecting
piece 16 through the heat exchanger 15, which i8
arranged for cooling the raw gases and heating the
clean gases in the heating surface space 22 of the heat
exchanger pressure vessel 3.
The raw gases leave the heat exchanger pressure
vessel via the raw gas outlet 17 and flow via the con-
necting conduit 4, which i8 provided with insulation 7only, and via the raw gas inlet 18 into the gas clean-
ing pressure vessel 5, recirculated exhaust gas or a
gas similar to that used for combustion being mixed via
the connecting piece 30 with the raw gases, which have
already been cooled by giving up heat to the clean gas,
that they are cooled to a temperature between
approximately 650 to 950 C. At this temperature, the
raw ga~es can have dust (including alkali metal com-
pounds) removed by known methods, such as cyclones,

~. ~118178 :~ ~
- 6
ceramic filter tubes 24 etc. and are, furthermore,
desulphurized by likewise known method~, for example
the dry additive method, i.e. by spraying in lime dust,
and are freed from oxides of nitrogen by, for example,
the selective non-catalytic reduction - SNCR - method,
i.e. by spraying in ammonia. These gas cleaning meth-
ods 35 are arranged in a vessel 5 from which fly ash
and other residue~ such as gypsum can be withdrawn via
the outlet 20. The supply of the additives take~ place
via the connecting piece 28. The cleaned combustion
gases (~ clean gases) then flow via the clean gas out-
let 19, the connecting conduit 6 - which is only pro-
vided with insulation 7 - and the connecting piece 23
back to the heat exchanger pressure vessel 3. The
clean gas then flows through the heat exchanger 15
and/or the ducts 10, 9 and 8, which are configured as
heat exchangers, of the heat exchanger pressure vessel
3, of the connecting conduit 2 and of the combustion
chamber pressure vessel 1, taking up heat from the
uncleaned combustion gaseE (= raw gases) in the process
and leaving the combustion chamber pressure vessel via
the connecting piece 13 at the permissible gas turbine
inlet temperature. The clean gas then flows sequen-
tially through the gas turbine 36 in Figure 1 and the
waste heat steam generator 37 in Figure 1. In this
waste heat steam generator 37, water for operating a
steam turbine is preheated, evaporated and superheated
at one or a plurality of pre~sure stages (a possible
cycle with three pre~sure stages is represented in

~118178
Figure 1). Water can also be tapped off for heating
purposes.
After the exhaust heat boiler, part of the exhaust
gases can be recirculated by means of a compressor 31
driven by the ga~ turbine, see Figure 1, to the pos-
itions-ll, 26 and 30 listed above. The rest can - if
this is necessary or has not already occurred - be
cleaned in known manner to permissible emi~sion figures
and leaves the power station via a chimney. If pure
oxygen i8 used as the oxidizing agent, a gas mixture
which consists almost exclusively of C02 and steam
occurs - as already mentioned - as the exhaust gas.
With appropriate further cooling, stéam condenses first
and finally the C02 with the residual gas traces also
becomes fluid or freezes. This produces a power
station which i8 free of exhaust gas, if the nitrogen
separated from the air during the production of the
oxygen is ignored. In addition, the compressor for air
or for air enriched with oxygen or for pure oxygen 32 -
see Figure 1 - is also driven by the gas turbine 36.
The combustion chamber pressure vessel 1, the con-
necting conduit 2 and the heat exchanger pres~ure ves-
sel 3 are constructed in such a way that the pre3sure-
carrying wall is located on the outside. Insulation !7~
ducts 8, 9 and 10 in which clean gas flows and a jacket
21, which is heat conducting, substantially impermeable
to gas and fire-resistant, follow in sequence towards
the inside. It is only within this jacket that raw gas
flows.

Dessin représentatif
Une figure unique qui représente un dessin illustrant l'invention.
États administratifs

2024-08-01 : Dans le cadre de la transition vers les Brevets de nouvelle génération (BNG), la base de données sur les brevets canadiens (BDBC) contient désormais un Historique d'événement plus détaillé, qui reproduit le Journal des événements de notre nouvelle solution interne.

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Historique d'événement

Description Date
Inactive : CIB de MCD 2006-03-11
Inactive : CIB de MCD 2006-03-11
Inactive : CIB de MCD 2006-03-11
Demande non rétablie avant l'échéance 2001-10-15
Le délai pour l'annulation est expiré 2001-10-15
Réputée abandonnée - omission de répondre à un avis sur les taxes pour le maintien en état 2000-10-16
Demande publiée (accessible au public) 1995-04-16

Historique d'abandonnement

Date d'abandonnement Raison Date de rétablissement
2000-10-16

Taxes périodiques

Le dernier paiement a été reçu le 1999-09-08

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  • taxe pour paiement en souffrance ; ou
  • taxe additionnelle pour le renversement d'une péremption réputée.

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Historique des taxes

Type de taxes Anniversaire Échéance Date payée
TM (demande, 3e anniv.) - générale 03 1997-10-14 1997-09-26
TM (demande, 4e anniv.) - générale 04 1998-10-14 1998-10-09
Enregistrement d'un document 1999-04-08
TM (demande, 5e anniv.) - générale 05 1999-10-14 1999-09-08
Titulaires au dossier

Les titulaires actuels et antérieures au dossier sont affichés en ordre alphabétique.

Titulaires actuels au dossier
ALSTOM ENERGY SYSTEMS GMBH
Titulaires antérieures au dossier
REINHARD LEITHNER
Les propriétaires antérieurs qui ne figurent pas dans la liste des « Propriétaires au dossier » apparaîtront dans d'autres documents au dossier.
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Description du
Document 
Date
(aaaa-mm-jj) 
Nombre de pages   Taille de l'image (Ko) 
Revendications 1995-04-16 3 186
Dessins 1995-04-16 2 134
Abrégé 1995-04-16 1 58
Page couverture 1995-04-16 1 69
Description 1995-04-16 7 441
Dessin représentatif 1998-02-24 1 25
Courtoisie - Certificat d'enregistrement (document(s) connexe(s)) 1999-04-29 1 117
Courtoisie - Lettre d'abandon (taxe de maintien en état) 2000-11-14 1 183
Rappel - requête d'examen 2001-06-18 1 118
Taxes 1998-10-09 1 37
Taxes 1997-09-26 1 41
Taxes 1999-09-08 1 30
Taxes 1996-09-23 1 42
Courtoisie - Lettre du bureau 1994-12-05 2 79
Correspondance reliée au PCT 1995-01-06 1 29
Courtoisie - Lettre du bureau 1994-12-19 1 35