IP Library Granted Patent US 6,988,356
Granted Patent B2
US 6,988,356 · App. 10/692,796 · Granted Jan 24, 2006

Fuel metering unit with a compensated regulator valve in a turbomachine

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Quick Facts
Patent No.
US 6,988,356
App. No.
10/692,796
Granted
Jan 24, 2006
Kind
B2
Abstract

A fuel metering unit in a turbomachine is connected between a high pressure pump which draws fuel from a fuel tank and a plurality of fuel injectors disposed in a combustion chamber of the turbomachine, the unit comprises a meter which receives the fuel for injection from a regulator valve at a pressure P 1 and delivers it at a pressure P 2 to said plurality of injectors via a stop valve, said regulator valve serving to recirculate fuel back to said high pressure pump as a function of the pressure difference between pressures taken directly from the terminals of the meter and injected into two end inlets of the regulator valve.

Claims (7)

1. A fuel metering unit in a turbomachine, the unit being mounted between a high pressure pump which draws fuel from a fuel tank and a plurality of fuel injectors for injecting the fuel into a turbomachine combustion chamber, the unit comprising a meter which has an inlet receiving fuel for injection from a regulator valve at a pressure P 1 and has an outlet which delivers the fuel at a pressure P 2 to said plurality of injectors via a stop valve, said regulator valve comprising a hydraulic slide movable in a sheath under drive from the pressures P 1 and P 2 taken directly from the terminals of the meter and acting on two end inlets of said regulator valve on respective sectional areas S 1 and S 2 of the hydraulic slide, said slide having a first annular neck for allowing fuel to recirculate to said high pressure pump by puffing a first feed inlet of said sheath connected to an outlet of said high pressure pump into communication with a feed outlet of said sheath connected to an inlet of said high pressure pump, wherein said hydraulic slide further includes a second annular neck for providing another recirculation path to said high pressure pump by puffing a second feed inlet of said sheath connected to said inlet of the meter into communication with an auxiliary feed outlet of said sheath connected to said inlet of the high pressure pump.

2. A fuel metering unit according to claim 1 , wherein said second feed inlet is connected to said inlet of the meter via a fixed diaphragm.

3. A fuel metering unit according to claim 2 , wherein said fixed diaphragm has an orifice either pierced through said sheath or else made outside said regulator valve.

4. A fuel metering unit according to claim 1 , wherein said auxiliary feed outlet is connected to said inlet of the high pressure pump via a variable diaphragm.

5. A fuel metering unit according to claim 4 , wherein said variable diaphragm comprises a plurality of orifices of identical shape distributed in equidistant manner around said sheath through which they are pierced and offset from one another in the travel direction of said regulator valve.

6. A fuel metering unit according to claim 5 , wherein said orifices are of a section selected from the following sections: circular, rectangular, triangular, and oblong.

7. A fuel metering unit according to claim 6 , wherein said orifices are made by electroerosion.

Assignments (3)
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 Dec 17, 2012
From: SUIZA, HISPANO
To: SNECMA
Reel/Frame 029481/0429 →