Fuel nozzle for a turbine engine with a passive purge air passageway
AssigneeGeneral Electric Company
InventorsJohn Intile, Predrag Popovic, Lucas John Stoia
Life of this patent
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Abstract
A secondary fuel nozzle for a turbine includes a passive purge air passageway which provides purge air to the secondary nozzle at all times that the nozzle is in operation. The passive purge air passageway draws in air from a location adjacent an upstream end of the nozzle. Because of a pressure differential between air located at the downstream end of the nozzle and air located at the upstream end of the nozzle, purge air will run through the passive purge air passageway at all times the nozzle is in operation. There is no need for a supply of compressed purge air.
Claims11
A fuel nozzle for a turbine engine, comprising:
- an elongated housing having a central longitudinal axis;
- at least one fuel delivery passageway that extends down at least a portion of the housing;
- an active purge air passageway that extends down the housing and that delivers purge air to at least one active purge air discharge opening that is located at the discharge end of the nozzle;
- and
- a passive purge air passageway having an inlet that admits air from a position outside the nozzle and adjacent an upstream end of the housing, and having an outlet that is located at the discharge end of the nozzle, wherein the inlet of the passive purge air passageway comprises:
- a first transfer passageway that extends radially through the nozzle from an upstream end of the passive purge air passageway;
- and
- a second transfer passageway that extends from an outward end of the first transfer passageway toward the discharge end of the nozzle in a direction that is substantially parallel to the central longitudinal axis of the housing such that air traveling through the second transfer passageway and into the passive purge air passageway travels in an upstream direction.
A fuel nozzle for a turbine engine, comprising:
- an elongated housing having a central longitudinal axis;
- a fuel delivery passageway that extends along at least a portion of the housing;
- an active purge air passageway that extends along the housing and that delivers purge air to at least one active purge air discharge opening that is located at a downstream end of the nozzle;
- and
- a passive purge air passageway having an inlet that admits air from a position outside the nozzle and adjacent an upstream end of the housing, and having an outlet that is located at the downstream end of the nozzle, wherein when the fuel nozzle is in use in an operational turbine engine, a pressure differential between air outside the nozzle and adjacent the upstream end of the housing and air located at the outlet of the passive purge air passageway causes purge air to flow along the passive purge air passageway from the inlet to the outlet, wherein the passive purge air passageway comprises:
- a first section that extends from the inlet in a direction substantially parallel to the longitudinal axis, wherein air flowing through the first section of the passive purge air passageway is flowing in an upstream direction;
- a second section that extends inward in a radial direction from an upstream end of the first section;
- and
- a third section that extends in a direction substantially parallel to the longitudinal axis from the inward end of the second section to the outlet at the downstream end of the nozzle.
Dependencies are inferred from the claim text.