Reduced coking of fuel nozzles

Patent · Tue Jan 17 00:00:00 EST 1989

OSTI ID:6239742

Mancini, A A; Sager, J W; Kobish, T R

This patent describes a fuel nozzle useful for a gas turbine engine and having a nozzle face, the combination of fuel supply means on the nozzle, the fuel supply means including an annular fuel discharge body converging in a downstream direction toward a longitudinal central axis of the nozzle and terminating in a downstream fuel discharge orifice substantially on the central axis for discharging fuel from the orifice for mixing with air downstream of the nozzle face, air supply means on the nozzle for discharging air from the nozzle face, and means on the nozzle around the fuel discharge body cooperating with the air supply means for controllably discharging sufficient air flow with locally reduced swirl strength over the fuel discharge body to establish a recirculation zone spaced away from the nozzle face downstream thereof a sufficient distance to substantially reduce coking on the nozzle face.

• Assignee: Fuel Systems Textron Inc., Zeeland, MI
• Patent Number(s): US 4798330
• OSTI ID: 6239742
• Resource Relation: Patent File Date: Filed date 14 Feb 1986
• Country of Publication: United States
• Language: English

Related Subjects

33 ADVANCED PROPULSION SYSTEMS
FUEL SYSTEMS
NOZZLES
GAS TURBINE ENGINES
SCALE CONTROL
AIR FLOW
DEPOSITS
DESIGN
FLOW REGULATORS
CONTROL
CONTROL EQUIPMENT
ENGINES
EQUIPMENT
FLUID FLOW
GAS FLOW
HEAT ENGINES
INTERNAL COMBUSTION ENGINES
330103* - Internal Combustion Engines- Turbine