System und Verfahren zur Verringerung der Verbrennungsdynamik in einer Turbomaschine
Anmelder: General Electric Company 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP2634488
- Aktenzeichen
- EP12197453
- Anmeldetag
- 17. Dezember 2012
- Veröffentlichung
- 20. September 2017
- Erteilung
- 20. September 2017
- Rechtsraum
- EP
- IPC
- F23R3/28F23R3/54
Abstract
A system for reducing combustion dynamics in a combustor includes an end cap having an upstream surface (42) axially separated from a downstream surface (44), and tube bundles (24) extend from the upstream surface (42) through the downstream surface (44). A divider (32) inside a tube bundle (24) defines a diluent passage (34) that extends axially through the downstream surface (44), and a diluent supply (58) in fluid communication with the divider (34) provides diluent flow to the diluent passage (34). A method for reducing combustion dynamics in a combustor (10) includes flowing a fuel through tube bundles (24), flowing a diluent through a diluent passage (34) inside a tube bundle (24), wherein the diluent passage (34) extends axially through at least a portion of the end cap into a combustion chamber (26), and forming a diluent barrier in the combustion chamber (26) between the tube bundle (24) and at least one other adjacent tube bundle (24).
Anmelder
- Firma
- General Electric Company
- Land
- 🇺🇸 USA
US-amerikanischer Technologiekonzern mit Sitz in Massachusetts. Historisch aktiv in Energieerzeugung, Luftfahrttriebwerken, Medizintechnik und Industrietechnik über verschiedene Geschäftsbereiche.
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Fachgebiete
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Cleary, Fidelma
NoneLondon