Gasturbinentriebwerk und Brennstoffeinspritzanordnung dafür
Anmelder: General Electric Company 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP4722596
- Anmeldetag
- 10. September 2025
- Veröffentlichung
- 8. April 2026
- Rechtsraum
- EP
- IPC
- F23R3/28
Abstract
A gas turbine engine (10), comprising a compressor section (12), combustion section (14), and turbine section (16) in serial flow arrangement, with the combustion section (14) comprising: a combustor liner (40) at least partially defining a combustion chamber (50); and a fuel injector assembly (48, 100, 200) comprising a mixing tube (38, 110, 210) having a mixing tube body (112, 212) defining a mixing channel (114, 214). The mixing tube body (112, 212) can have a set of fuel passages (132, 232) terminating in fuel orifices (136, 236) fluidly coupled to the mixing channel (114, 214). A set air flow passages (142, 242) terminating in air outlets (144, 244) can be fluidly coupled to the mixing channel (114, 214). At least some of the air outlets (144, 244) circumscribe a corresponding fuel orifice (136, 236).
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.
15.498 Patente in unserer Datenbank
Vertreten von
-
Openshaw & Co
Openshaw & Co · Onex