Fuel metering circuit and method with compensation for fuel-density variability

US11365692B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11365692-B2
Application numberUS-201816630705-A
CountryUS
Kind codeB2
Filing dateJul 13, 2018
Priority dateJul 13, 2017
Publication dateJun 21, 2022
Grant dateJun 21, 2022

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

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.

First claim

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.

Assignees

Inventors

Classifications

  • F02C9/263Primary

    by means of fuel metering valves · CPC title

  • F02C7/22Primary

    Fuel supply systems · CPC title

  • Combustors or associated equipment · CPC title

  • for aircraft propulsion, e.g. jet engines · CPC title

  • Fuel valves {(control of fuel supply by means of fuel metering valves F02C9/263)}; Draining valves or systems (valves in general F16K) · CPC title

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What does patent US11365692B2 cover?
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 valv…
Who is the assignee on this patent?
Safran Aircraft Engines
What technology area does this patent fall under?
Primary CPC classification F02C9/263. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jun 21 2022 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).