IP Library Granted Patent US 8,549,863
Granted Patent B2
US 8,549,863 · App. 11/816,535 · Granted Oct 8, 2013

Device for supplying fuel to a gas turbine engine with regulated fuel flow rate

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Quick Facts
Patent No.
US 8,549,863
App. No.
11/816,535
Granted
Oct 8, 2013
Kind
B2
Abstract

A fuel supply device includes a fuel supply pipe receiving fuel at a non-regulated pressure delivered by a pump, a device for measuring the flow rate of fuel in the pipe, a first controlled variable-restriction valve mounted in the supply pipe, a control system connected to the flow rate measurement device and to the first valve to control the valve to deliver fuel to the engine at a desired flow rate under normal operating conditions of the engine, a second controlled variable-restriction valve mounted in the supply pipe in series with the first valve, and a control for controlling the second valve to enable the engine to be supplied with fuel at an adjustable, reduced flow rate in response to detecting over-speed or over-thrust of the engine.

Claims (15)

1. A supply device for supplying fuel at a regulated flow rate to a gas turbine engine, the device comprising: a supply pipe for supplying fuel to the engine;

a pump connected to the supply pipe and delivering the supply pipe with fuel at a pressure that is a function of engine speed;

a flow rate measuring device for measuring the fuel flow rate in the supply pipe;

a first controlled variable-restriction valve connected in the supply pipe;

a first control circuit connected to the flow rate measurement device and to the first valve to control the first valve to deliver a regulated desired fuel flow rate under normal operating conditions of the engine, the first control circuit comprising at least one first electromechanical actuator for controlling a degree to which the first valve is opened;

a second controlled variable-restriction valve mounted in the supply pipe in series with the first valve; and

a second control circuit connected to the second valve, the second control circuit comprising at least one second electromechanical actuator for controlling the second valve and being configured to reduce the flow rate of fuel in the supply pipe in response to detecting over-speed or over-thrust of the engine, by bringing the second valve into a predetermined partially closed position, and to control thereafter regulation of the fuel flow rate via the second valve over at least a reduced range by modifying the fuel flow rate as a function of a desired engine speed, hereby conserving controllability of the engine, the at least one second electromechanical actuator being controlled from an automatic regulation system of the engine via a second module that is distinct from a first module dedicated to performing regulation by means of the first valve,

wherein the second module controls the regulation of the fuel flow rate over the reduced range based on a difference detected between the measured flow rate and a setpoint flow rate so as to position the second valve to regulate the flow rate on a desired setpoint value after the second valve is brought into the predetermined partially closed position in response to detecting over-speed or over-thrust of the engine.

2. A device according to claim 1 , wherein the flow rate measurement device is a mass flow meter and the first control circuit includes a local servo-control circuit receiving a mass flow rate setpoint value from the automatic regulation system of the engine.

3. A device according to claim 1 , wherein the flow rate measurement device is a volumetric flow meter.

4. A device according to claim 1 , wherein the flow rate measurement device is a device for measuring flow rate on the basis of knowledge of a pressure drop and flow section through the measurement device.

5. A device according to claim 1 , wherein the first control circuit comprises a servo-control loop receiving a signal delivered by the flow rate measurement device and representative of a real fuel flow rate, receiving a setpoint signal representative of the desired fuel flow rate, and delivering a control signal to the at least one first electromechanical actuator as a function of the difference detected between the real and desired flow rate.

6. A device according to claim 5 , wherein the servo-control loop is a loop implanted locally in a vicinity of the first valve and external to an electronic regulation system of the engine supplying the setpoint signal.

7. A device according to claim 5 , wherein the at least one first electromechanical actuator can be pre-positioned on starting of the engine and the first valve includes a slot co-operating with a pressure characteristic delivered by the pump on starting so as to servo-control the fuel flow rate on starting.

8. A device according to claim 1 , further comprising a cutoff, third valve mounted in the supply pipe in series with the first and second valves.

Assignments (4)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 3, 2011
From: HISPANO SUIZA
To: SNECMA
Reel/Frame 026213/0475 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 29, 2008
From: BROCARD, JEAN-MARIE; DELDALLE, REGIS MICHEL PAUL; GALOZIO, PHILIPPE; MARTINI, MICHEL; VARIZAT, ALAIN MICHEL
To: HISPANO SUIZA
Reel/Frame 020872/0419 →