Aircraft engine lubrication circuit and method, using a non-return pressurisation valve with two plugs

Patent metadata

Field	Value
Publication number	US-11466599-B2
Application number	US-201816014252-A
Country	US
Kind code	B2
Filing date	Jun 21, 2018
Priority date	Jun 22, 2017
Publication date	Oct 11, 2022
Grant date	Oct 11, 2022

Abstract

A non-return valve with twin plugs is connected to a fluid reservoir and equipment that can receive a small overflow quantity essentially in the gaseous state from the reservoir. This occurs when the primary valve is open. In the case of a larger overflow essentially in the liquid state, the openings are switched over to evacuate the overflow to another outlet branch of the non-return valve, without it being transferred to the equipment. The invention is useful in an oil lubrication circuit, in which a hypothetical fuel leak into the oil could cause the oil reservoir to overflow into the non-return valve and in which a significant flow of liquid to the equipment must be avoided; oil outlet through the other branch of the outlet can remain in a reservoir provided with a drain system.

First claim

The invention claimed is:

1. An aircraft engine lubrication oil circuit, the circuit comprising:
a non-return valve comprising a case fitted with a connector on an upstream side and an outlet on a downstream side,
an oil supply on said upstream side of the non-return valve,
a first valve plug and a second valve plug housed in a manner free to move in the case to open and to create a communication between the connector and the outlet, when a first overpressure threshold is reached on the upstream side for the first valve plug; and when a second overpressure threshold on the upstream side higher than the first threshold is reached, for the second valve plug,
in which the outlet comprises two branches, a first branch leading to a device to be lubricated remaining open at least up to the second overpressure threshold, and a second branch,
a switching device that opens the second branch when the second overpressure threshold is reached,
the second branch of the outlet connected to an exterior of the circuit.

2. The aircraft engine lubrication oil circuit according to claim 1 , wherein the switching device comprises an element of the second plug comprising a first opening prolonging an opening of the first branch when the second plug is closed, and not prolonging said opening of the first branch when the second plug is open.

3. The aircraft engine lubrication oil circuit according to claim 2 , wherein the switching device consists of a sleeve extending in the direction of movement of the second plug and comprising two openings, including the first opening, staged in this direction, and a second of the openings in the sleeve prolonging an opening in the second branch when the second plug is open.

4. The aircraft engine lubrication oil circuit according to claim 1 , wherein the switching device comprises a third valve plug that opens the second branch when the second overpressure threshold has been reached, the first branch being controlled by a gas flow calibration orifice, with a smaller passage section than the second branch.

5. The aircraft engine lubrication oil circuit according to claim 1 , wherein the device to be lubricated is an engine auxiliary equipment gearbox.

6. The aircraft engine lubrication oil circuit according to claim 5 , further comprising a heat exchanger on the upstream side of the non-return valve.

7. The aircraft engine lubrication oil circuit according to claim 1 , wherein the circuit is evacuated to an exterior of the non-return valve.

8. The aircraft engine lubrication oil circuit according to claim 1 , wherein the evacuation from the circuit uses a reservoir.

9. A method of lubricating an aircraft engine lubrication oil circuit, the circuit comprising:
a non-return valve comprising a case fitted with a connector on an upstream side and an outlet on a downstream side,
an oil supply on said upstream side of the non-return valve,
a first valve plug and a second valve plug housed in a manner free to move in the case to open and to create a communication between the connector and the outlet, when a first overpressure threshold is reached on the upstream side for the first valve plug; and when a second overpressure threshold on the upstream side higher than the first threshold is reached, for the second valve plug,
in which the outlet comprises two branches, a first branch leading to a device to be lubricated remaining open at least up to the second overpressure threshold, and a second branch,
a switching device that opens the second branch when the second overpressure threshold is reached,
the second branch of the outlet connected to an exterior of the circuit, the method comprising a pressure limitation of the oil circuit by means of the non-return valve by extraction of an overflow and a flow from the overflow to the device to be lubricated, wherein when an overpressure threshold is reached in the circuit, the method comprises opening of the evacuation outside the circuit and said chamber and switching of the non-return valve to direct at least most of the overflow towards the evacuation.

Assignees

• Safran Aircraft Engines

Inventors

• Rigouste Jérôme

Classifications

• F05D2260/98

  Lubrication · CPC title

• F01D17/06 Primary

  responsive to speed · CPC title

• F01D17/105

  by passing part of the fluid · CPC title

• F01M2001/1085

  comprising non-return valves · CPC title

• F02C7/14

  of fluids in the plant {, e.g. lubricant or fuel (F02C7/185 takes precedence)} · CPC title