Axial Kraftstoffstagsystem für Gasturbinenbrenner
Anmelder: General Electric Technology GmbH, General Electric Company 🇨🇭
Details
- Veröffentlichungs-Nr.
- EP3495736
- Aktenzeichen
- EP18210148
- Anmeldetag
- 4. Dezember 2018
- Veröffentlichung
- 11. September 2024
- Erteilung
- 11. September 2024
- Rechtsraum
- EP
- IPC
- F23R3/34
Abstract
A gas turbine combustor includes: a head end 70 comprising a primary fuel nozzle 80; a liner 40 defining a primary combustion zone 90 proximate the head end and a downstream secondary combustion zone 100; a forward casing 130 radially outward of and surrounding at least a portion of the liner; and an axial fuel staging system 200. The axial fuel staging system includes a plurality of fuel injection assemblies 210. Each fuel injection assembly includes a thimble assembly 160 mounted to the liner, and an injector unit 110 attached to the forward casing. A thimble of the thimble assembly extends through a thimble aperture 146 in the liner. The injector unit extends through the forward casing 130, such that a portion of the injector unit is disposed within the thimble, and a fuel line fitting is disposed outward of the forward casing. The injector unit 110 introduces fuel into air flowing through the thimble for injection into the secondary combustion zone 100.
Anmelder
- Firmen
- General Electric Technology GmbH
General Electric Company - Land
- 🇨🇭 Schweiz
Schweizer Konzerngesellschaft im Bereich Energietechnik, verbunden mit dem US-Konzern General Electric. Entwickelt Technologien für Stromerzeugung und Energieübertragung, darunter Turbinen und Netzlösungen.
2.949 Patente in unserer Datenbank
US-amerikanischer Technologiekonzern mit Sitz in Massachusetts. Historisch aktiv in Energieerzeugung, Luftfahrttriebwerken, Medizintechnik und Industrietechnik über verschiedene Geschäftsbereiche.
15.498 Patente in unserer Datenbank
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