WO2024251509 - GAS TURBINE ARRANGEMENT WITH AMMONIA CRACKER AND POWER PLANT WITH SUCH AND METHOD TO OPERATE A GAS TURBINE ARRANGEMENT
National phase entry:
Publication Number
WO/2024/251509
Publication Date
12.12.2024
International Application No.
PCT/EP2024/063920
International Filing Date
21.05.2024
Title **
[English]
GAS TURBINE ARRANGEMENT WITH AMMONIA CRACKER AND POWER PLANT WITH SUCH AND METHOD TO OPERATE A GAS TURBINE ARRANGEMENT
[French]
AGENCEMENT DE TURBINE À GAZ AVEC CRAQUEUR D'AMMONIAC, CENTRALE ÉLECTRIQUE DOTÉE D'UN TEL AGENCEMENT ET PROCÉDÉ DE FONCTIONNEMENT D'UN AGENCEMENT DE TURBINE À GAZ
Applicants **
SIEMENS ENERGY GLOBAL GMBH & CO. KG
Inventors
ANDERSSON, Mats
Priority Data
2308457.7
07.06.2023
GB
Application details
| Total Number of Claims/PCT | * |
| Number of Independent Claims | * |
| Number of Priorities | * |
| Number of Multi-Dependent Claims | * |
| Number of Drawings | * |
| Pages for Publication | * |
| Number of Pages with Drawings | * |
| Pages of Specification | * |
| * | |
| Number of Office Actions | * |
| * | |
International Searching Authority |
EPO
* |
| Recordal of a Change of the Applicant's Name/Address |
Change of Applicant's Name and Address
* |
| Type of Assignment |
The Standard Agent's Assignment
* |
| Applicant's Legal Status |
Legal Entity
* |
| * | |
| * | |
| * | |
| * | |
| * | |
| Entry into National Phase under |
Chapter I
* |
| Patent Delivery |
Send the Letters Patent by Courier
* |
| Translation |
|
* The data is based on automatic recognition. Please verify and amend if necessary.
** IP-Coster compiles data from publicly available sources. If this data includes your personal information, you can contact us to request its removal.
Quotation for National Phase entry
| Country | Stages | Total | |
|---|---|---|---|
| China | Filing, Examination, Granting | 1985 | |
| EPO | Filing, Examination, Granting | 8688 | |
| Japan | Filing, Examination, Granting | 2229 | |
| South Korea | Filing, Examination, Granting | 2091 | |
| USA | Filing, Examination, Granting | 5340 |
Total:
20,333
The term for entry into the National Phase has expired. This quotation is for informational purposes only
Contact Us
Abstract[English]
Combustion arrangement (01) of a gas turbine comprising a burner (02), a combustion chamber (03) and an ammonia cracker (11). The ammonia cracker comprises heating means and a reaction channel (12), wherein an outlet of the reaction channel is fluidly connected to the combustion chamber and an inlet of the reaction channel is configured to be fluidly connected to a source of ammonia. To increase the efficiency and to reduce the installation effort it is intended to use a transfer section (13) as heating means, wherein the transfer section limits the combustion chamber in sections and enables a heat transfer from the combustion chamber to the reaction channel.[French]
L'invention concerne un agencement de combustion (01) d'une turbine à gaz comprenant un brûleur (02), une chambre de combustion (03) et un craqueur d'ammoniac (11). Le craqueur d'ammoniac comprend des moyens de chauffage et un canal de réaction (12), une sortie du canal de réaction étant en communication fluidique avec la chambre de combustion et une entrée du canal de réaction étant conçue pour être en communication fluidique avec une source d'ammoniac. Pour augmenter l'efficacité et réduire l'effort d'installation, il est prévu d'utiliser une section de transfert (13) en tant que moyen de chauffage, la section de transfert limitant la chambre de combustion dans des sections et permettant un transfert de chaleur de la chambre de combustion au canal de réaction.