Multipoint fuel injection system for a turbomachine and associated regulation method

Patent metadata

Field	Value
Publication number	US-10473032-B2
Application number	US-201414916077-A
Country	US
Kind code	B2
Filing date	Sep 1, 2014
Priority date	Sep 3, 2013
Publication date	Nov 12, 2019
Grant date	Nov 12, 2019

Abstract

The invention concerns a fuel system ( 1 ) for a turbomachine comprising: —a control circuit ( 9 a ), —a main circuit ( 9 b ), —a flow rate regulator ( 2 ), suitable for regulating the flow of fuel in the control circuit ( 9 a ) and in the main circuit ( 9 b ) depending on the speed of the turbomachine, and —a drain tank ( 4 ) being designed to draw fuel from, store fuel in and drain fuel into the main circuit ( 9 b ) on the basis of the pressure difference between the main circuit ( 9 b ) and the tank ( 5 ) or the high-pressure pump ( 6 ) to which it is connected.

First claim

The invention claimed is:

1. A fuel system for a turbine engine, adapted to inject fuel into a combustion chamber of the turbine engine, comprising:
a pilot circuit, adapted to inject fuel into the combustion chamber,
a main circuit, adapted to inject fuel into the combustion chamber, and
a flow rate regulator, adapted to regulate the fuel flow rate in the pilot circuit and in the main circuit as a function of the speed of the turbine engine, said flow rate regulator comprising a mobile spool between a first configuration, in which the main circuit is blocked and the pilot circuit is passing, and a second configuration in which at the same time the main circuit and the pilot circuit are passing,
a pressure regulator downstream of the flow rate regulator,
the fuel system being characterized in that it further comprises:
a fuel tank,
a high-pressure pump, adapted to pressurise the fuel at the outlet of the fuel tank, and
a purge tank, connected on one side via a first port selectively to the fuel tank such that the pressure at the first port is equal to the pressure of the fuel tank, or to the high-pressure pump such that the pressure at the first port is equal to the pressure at an outlet of the high-pressure pump, and the purge tank being connected on another side at a purge port to the main circuit, said purge tank being adapted to suction, store and purge fuel in the main circuit through the purge port as a function of the pressure difference between the main circuit and the fuel tank or the high-pressure pump to which it is connected;
wherein the purge tank is connected to the main circuit downstream of the pressure regulator.

2. The fuel system according to claim 1 , wherein the pressure regulator is adapted to modify the pressure in the pilot circuit and the main circuit and reduce the differences in pressure losses between the pilot circuit and the main circuit upstream of the pressure regulator.

3. The fuel system according to claim 2 , wherein the pressure regulator comprises regulating means adapted to modify a passage section of the main circuit and of the pilot circuit downstream of the flow rate regulator to limit the pressure losses in said circuits.

4. The fuel system according to claim 3 , wherein the regulating means are controlled by two antagonist pressures respectively corresponding to the pressure at the inlet of the pilot circuit and to the pressure at the inlet of the main circuit to adapt the passage section of said main and pilot circuits.

5. The fuel system according to claim 4 , wherein the regulating means further comprise a regulating spool adapted to adjust the passage section of the main circuit and of the pilot circuit, the position of the regulating spool being in dynamic balance as a function of the pressure at the inlet of the pilot circuit and of the pressure at the inlet of the main circuit.

6. The fuel system according to claim 1 , wherein the purge tank is controlled by the flow rate regulator which selectively connects the purge tank to the fuel tank or to the high-pressure pump, such that:
in the first configuration of the spool, the purge tank is connected to the fuel tank and stores fuel contained in the main circuit, and
in the second configuration of the spool, the purge tank is connected to the high-pressure pump and purges in the main circuit the fuel stored when the spool was in the first configuration.

7. The fuel system according to claim 1 , further comprising a fuel metering unit FMU upstream of the flow rate regulator.

8. The fuel system according to claim 1 , wherein the flow rate regulator is actuated by a servo valve and further comprises a linear variable differential transformer LVDT adapted to determine the configuration of the spool in the flow rate regulator.

9. A turbine engine comprising a combustion chamber, characterized in that it comprises a fuel system adapted to inject fuel into the combustion chamber according to claim 1 .

10. A regulating method, characterized in that it uses a fuel system injecting fuel having an inlet flow rate in the combustion chamber of the turbine engine by means of the pilot circuit and the main circuit according to claim 1 , said regulating method comprising the following steps:
regulating distribution of the fuel flow rate in the pilot circuit and in the main circuit as a function of a speed of the turbine engine by moving the mobile spool between the first configuration, wherein the main circuit is blocked and the pilot circuit is passing, and the second configuration wherein at the same time the main circuit and the pilot circuit are passing, and
controlling the purge tank as a function of the position of the mobile spool of the flow rate regulator by selectively connecting the purge tank to the fuel tank or the high-pressure pump so as to suction, store or purge fuel in the main circuit.

11. The regulating method according to claim 10 , wherein:
distribution of the inlet fuel flow rate between the pilot circuit and the main circuit is regulated by controlling the position of the mobile spool which modifies a fuel passage section at the inlet of the pilot circuit and a fuel passage section at the inlet of the main circuit, the pilot circuit and the main circuit each receiving a fraction of the inlet flow rate,
each position of the mobile spool fixing the fraction of the inlet flow rate received by the pilot circuit and the fraction of the inlet flow rate received by the main circuit, irrespective of the inlet fuel flow rate, enabling regulation of the distribution of the inlet flow rate from control of the position of the spool,
the method further comprising a step during which distribution of the fuel inlet flow rate is corrected so as to respect a minimum or maximum flow rate of fuel to be received for the pilot circuit and/or the main circuit.

Assignees

• Snecma
• Safran Aircraft Engines

Inventors

• Bernard Clement
• Pora Loic
• Chalaud Sebastien

Classifications

• F23K2300/206

  Control devices · CPC title

• F23N2237/02

  two or more burners · CPC title

• F23K5/04

  Feeding or distributing systems using pumps (from a central source to a plurality of burners F23K5/06) · CPC title

• F23N1/002

  using electronic means (F23N1/04 - F23N1/10 take precedence) · CPC title

• F02C9/34

  Joint control of separate flows to main and auxiliary burners · CPC title