IP Library Granted Patent US 8,387,400
Granted Patent B2
US 8,387,400 · App. 13/348,682 · Granted Mar 5, 2013

Thermal management for fuel injectors

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Quick Facts
Patent No.
US 8,387,400
App. No.
13/348,682
Granted
Mar 5, 2013
Kind
B2
Abstract

Methods of managing fuel temperatures in fuel injectors for gas turbine engines include cooling fuel circuits by initiating fuel flow therethrough using opened, closed, and semi-open control techniques. A fuel injector for a gas turbine engine includes a feed arm having a fuel inlet fitting for delivering fuel to at least one fuel conduit extending through the feed arm. A nozzle body depends from the feed arm and has at least one fuel circuit extending therethrough. The fuel circuit is configured and adapted to receive fuel from the feed arm and to issue fuel from an exit orifice of the nozzle body. Sensing means are provided adjacent to the at least one fuel circuit. The sensing means are configured and adapted to provide temperature feedback in order to control fuel flow in the at least one fuel circuit to maintain fuel temperature within a predetermined range.

Claims (6)

1. A fuel injector for a gas turbine engine comprising:

a) a feed arm having a fuel inlet fitting for delivering fuel to at least one fuel conduit extending through the feed arm;

b) a nozzle body depending from the feed arm having a pilot fuel circuit and a main fuel circuit outboard of the pilot circuit extending therethrough, wherein the pilot fuel circuit and the main fuel circuit are configured and adapted to receive fuel from the feed arm and to issue fuel from an exit orifice of the nozzle body; and

c) sensing means configured and adapted to provide temperature feedback in order to control fuel flow in at least one of the main and pilot fuel circuits to maintain fuel temperature within a predetermined range, wherein the sensing means are in a swirler housing of the nozzle body adjacent to at least one of the main and pilot fuel circuits for sensing fuel temperature.

2. A fuel injector as recited in claim 1 , wherein the sensing means are adjacent a portion of the at least one of the main and pilot fuel circuits configured and adapted to experience highest peak wetted wall temperatures within the fuel circuit.

3. A fuel injector as recited in claim 1 , wherein the nozzle body includes a pure airblast nozzle having an on-axis inner air circuit inboard of the fuel circuit, and an outer air circuit outboard of the nozzle body.

Assignments (1)
CHANGE OF NAME Recorded May 23, 2022
From: DELAVAN INC
To: COLLINS ENGINE NOZZLES, INC.
Reel/Frame 060158/0981 →