Device for supplying an oil tank from a second tank

Patent metadata

Field	Value
Publication number	US-11512615-B2
Application number	US-201816771401-A
Country	US
Kind code	B2
Filing date	Dec 17, 2018
Priority date	Dec 20, 2017
Publication date	Nov 29, 2022
Grant date	Nov 29, 2022

Abstract

An evaluation of the oil level of an aircraft engine tank from doses of oil delivered from another tank by a pump can be checked by comparing the evaluation of the volume provided by a sensor associated with the engine tank with an estimation of the volume extracted from the aircraft rank, either by another level sensor associated with this tank, or directly from the control of the pump. This comparison is made by a module capable of notifying staff of the need to check or maintain the device, and in particular to check if the sensor is operating correctly. Application to aeronautics, in particular to devices wherein a single aircraft tank supplies all the engine tanks.

First claim

The invention claimed is:

1. An aircraft, comprising:
a first oil tank adjacent to a propulsion engine of the aircraft;
a second oil tank separate from the engine;
a supply system for supplying the first tank with lubrication oil extracted from the second tank;
a first sensor of oil level in the first tank;
a second sensor of oil level in the second tank; and
a unit for controlling the supply system, comprising a comparing unit for estimating and comparing doses of oil extracted from the second tank with doses of oil received by the first tank, the comparing unit being informed by units for acquiring measurements from said first and second sensors.

2. The aircraft according to claim 1 , wherein the first sensor and the second sensor are sensors with a magnetic float and with a row of switches succeeding one another along a vertical row of float movement.

3. The aircraft according to claim 1 , wherein the comparing unit is informed by the unit for controlling the supply system, according to a duration of operation of the supply system.

4. The aircraft according to claim 1 , further comprising an alarming device, triggered by the comparing unit, when an inconsistency between estimations of the doses received by the first tank and estimations of the doses extracted from the second tank exceeds a threshold.

5. An aircraft comprising:
a plurality of first oil tanks adjacent to respective propulsion engines of the aircraft, said first oil tanks and propulsion engines being on opposite sides of the aircraft;
a single second oil tank separate from the propulsion engines and placed in a fuselage of the aircraft;
respective supply systems for respectively supplying the first tanks with lubrication oil extracted from the second tank;
a first sensor of oil level in each of the first tanks;
a second sensor of oil level in the second tank;
a unit for controlling each of the supply systems, comprising a comparing unit for estimating and comparing doses of oil extracted from the second tank with doses of oil received by a respective one of the first tanks, the comparing unit being informed by units for acquiring measurements from the second sensor and a respective one of the first sensors.

6. The aircraft according to claim 5 , wherein each said first sensor and the second sensor are sensors with a magnetic float and with a row of switches succeeding one another along a vertical row of float movement.

7. The aircraft according to claim 5 , wherein each said comparing unit is respectively informed by the unit for controlling the supply system, according to a duration of operation of the supply system.

8. The aircraft according to claim 5 , further comprising an alarming device, triggered by each said comparing unit, when an inconsistency between estimations of the doses received by the first tanks and estimations of the doses extracted from the second tank exceed a threshold.

Assignees

• Safran Aircraft Engines

Inventors

• Dupays Clement
• Santin Mathieu Jean Jacques
• Frantz Caroline Marie
• Gaillot-Drevon Benoit

Classifications

• F02C7/06 Primary

  Arrangements of bearings (bearings F16C); Lubricating ({of turbo machines F01D25/18; of machines or} engines in general F01M) · CPC title

• F05D2220/323

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

• F01D25/18

  Lubricating arrangements (of machines or engines in general F01M) · CPC title

• F16N2210/08

  Aircraft · CPC title

• F05D2260/80

  Diagnostics · CPC title