System for supplying a turbine engine with fluid having a low pressure pumping assembly comprising two pumps in parallel
US-2017101935-A1 · Apr 13, 2017 · US
US11365692B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11365692-B2 |
| Application number | US-201816630705-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 13, 2018 |
| Priority date | Jul 13, 2017 |
| Publication date | Jun 21, 2022 |
| Grant date | Jun 21, 2022 |
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A fuel metering circuit for a turbomachine includes: a meter; a pump; a control valve configured to return an excess flow of fuel delivered to the meter towards the pump on the basis of a fuel pressure differential at the terminals of the meter; a diaphragm; and a volumetric flow meter. The diaphragm and the volumetric flow meter are mounted parallel to the meter, downstream of the control valve, in order to determine a density of the fuel flowing in the metering circuit.
Opening claim text (preview).
The invention claimed is: 1. A fuel metering circuit for a turbomachine comprising: a metering device; a pump configured to circulate a fuel flow rate toward the metering device; a regulating valve configured to regulate the fuel flow rate delivered to the metering device according to a difference in fuel pressure at terminals of the metering device; a diaphragm; and a volume flow meter configured to determine a volume flow rate of fuel passing through the diaphragm, wherein the diaphragm and the volume flow meter are mounted in parallel with the metering device in a bypass duct, downstream of the regulating valve, in order to determine a density of the fuel circulating in the metering circuit. 2. The metering circuit according to claim 1 , wherein the volume flow meter is mounted upstream or downstream of the diaphragm. 3. The metering circuit according to claim 1 , further comprising an electronic card configured to receive information from the volume flow meter on the volume flow rate of the fuel and adjust a metering device monitoring setpoint by taking into account the fuel density thus determined. 4. The metering circuit according to claim 1 , wherein the pump comprises a volumetric pump. 5. A turbomachine comprising a fuel metering circuit according to claim 1 . 6. An aircraft comprising the turbomachine of claim 5 . 7. A fuel metering method implemented in a fuel metering circuit according to claim 1 , the method comprising: determining the difference in fuel pressure at the terminals of the metering device; measuring the volume flow rate of the fuel using the volume flow meter; and calculating, from the difference in fuel pressure, from the volume flow rate and from constants related to the diaphragm, the fuel density. 8. The metering method according to claim 7 , further comprising a step during which the flow meter transmits information on the volume flow rate of the fuel to an electronic card and the electronic card adjusts a metering device monitoring setpoint by taking into account the fuel density. 9. The metering method according to claim 7 , wherein the fuel flow rate is monitored by recirculating a variable fuel flow rate toward the pump by the regulating valve.
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