Oil system with flow restrictor

Patent metadata

Field	Value
Publication number	US-11525399-B1
Application number	US-202117350950-A
Country	US
Kind code	B1
Filing date	Jun 17, 2021
Priority date	Jun 17, 2021
Publication date	Dec 13, 2022
Grant date	Dec 13, 2022

Abstract

An oil system, has: a pump driving an oil flow in an oil conduit, the pump having an outlet pump pressure; a heat exchanger providing heat exchange between the oil flow and one or more fluid; a component downstream of the heat exchanger, the component having a maximum oil pressure requirement and a minimum oil pressure requirement; and a flow restrictor in fluid flow communication with the oil conduit, the flow restrictor having an orifice sized to provide a restrictor pressure differential across the flow restrictor, the restrictor pressure differential being equal to at least the outlet pump pressure minus pressure differentials through the heat exchanger and the oil conduit from an outlet of the pump to the component minus the maximum oil pressure requirement, and at most the outlet pump pressure minus the pressure differentials through the heat exchanger and the oil conduit minus the minimum oil pressure requirement.

First claim

The invention claimed is:

1. An oil system for an aircraft engine, comprising:
a pump driving an oil flow in an oil conduit, the pump having an outlet pump pressure;
a heat exchanger providing heat exchange between the oil flow and one or more fluid;
a component downstream of the heat exchanger, the component fluidly connected to the oil conduit for receiving at least a portion of the oil flow, the component having a maximum oil pressure requirement and a minimum oil pressure requirement; and
a flow restrictor in fluid flow communication with the oil conduit, the flow restrictor having an orifice sized to provide a restrictor pressure differential across the flow restrictor, the restrictor pressure differential being equal to
at least the outlet pump pressure minus pressure differentials through the heat exchanger and the oil conduit from an outlet of the pump to the component minus the maximum oil pressure requirement, and
at most the outlet pump pressure minus the pressure differentials through the heat exchanger and the oil conduit minus the minimum oil pressure requirement.

2. The oil system of claim 1 , wherein the component includes one or more bearing cavity and/or a gearbox.

3. The oil system of claim 1 , wherein the heat exchanger includes a first heat exchanger providing heat exchange between the oil flow and an air flow and a second heat exchanger providing heat exchange between the oil flow and a fuel flow.

4. The oil system of claim 3 , wherein the flow restrictor is hydraulically connected to the oil conduit downstream of the second heat exchanger.

5. The oil system of claim 3 , wherein the flow restrictor is hydraulically connected on the oil conduit upstream of the first heat exchanger.

6. The oil system of claim 1 , wherein a size of the orifice is variable.

7. The oil system of claim 6 , comprising a member being movable to vary the size of the orifice, the member engaged by an actuator.

8. The oil system of claim 7 , wherein the actuator is operatively connected to a controller having a processing unit operatively connected to a computer-readable medium having instructions stored thereon executable by the processing unit for:
receiving a signal from at least one sensor, the signal indicative of an oil pressure in the oil conduit;
determining that the oil pressure is outside a desired pressure operating range of the component based on the signal received from the at least one sensor; and
changing the size of the orifice until the oil pressure is within the desired pressure operating range.

9. The oil system of claim 8 , wherein the receiving of the signal from the at least one sensor includes receiving the signal from a pressure sensor and/or a temperature sensor operatively connected to the oil conduit.

10. The oil system of claim 8 , wherein the changing of the size of the orifice includes:
determining that the oil pressure is below the minimum oil pressure requirement; and
increasing the size of the orifice.

11. The oil system of claim 8 , wherein the changing of the size of the orifice includes:
determining that the oil pressure is above the maximum oil pressure requirement; and
decreasing the size of the orifice.

12. The oil system of claim 8 , wherein the changing of the size of the orifice includes powering the actuator.

13. A method of feeding oil of an oil system to a component of an aircraft engine, comprising:
transferring heat from an oil flow to one or more fluid via a heat exchanger;
decreasing a pressure of the oil flow with a flow restrictor such that the pressure of the oil flow is within a desired pressure operating range of the component downstream of the heat exchanger; and
feeding the oil flow to the component in need of oil after the decreasing of the pressure of the oil flow;
wherein the decreasing of the pressure with the flow restrictor includes flowing the oil flow through the flow restrictor having an orifice sized to create a restrictor pressure differential being equal to:
at least an outlet pump pressure of a pump driving the oil flow in an oil conduit of the oil system minus pressure differentials through the heat exchanger and the oil conduit from an outlet of the pump to the component minus a maximum oil pressure requirement of the desired pressure operating range, and at most the outlet pump pressure minus the pressure differentials through the heat exchanger and the oil conduit minus a minimum oil pressure requirement of the desired pressure operating range.

14. The method of claim 13 , comprising dynamically adjusting the pressure of the oil flow.

15. The method of claim 14 , comprising:
receiving a signal from at least one sensor, the signal indicative of the pressure;
determining that the pressure is outside the desired pressure operating range of the component based on the signal received from the at least one sensor; and
changing a size of an orifice until the pressure is within the desired pressure operating range.

16. The method of claim 15 , wherein the receiving of the signal from the at least one sensor includes receiving the signal from a pressure sensor and/or a temperature sensor operatively connected to the oil system.

17. The oil system of claim 15 , wherein the changing of the size of the orifice includes:
determining that the pressure is below a minimum oil pressure requirement; and
increasing the size of the orifice.

18. The oil system of claim 15 , wherein the changing of the size of the orifice includes:
determining that the pressure is above a maximum oil pressure requirement; and
decreasing the size of the orifice.

Assignees

• Pratt & Whitney Canada

Inventors

• Smith Sarah Nangle

Classifications

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• F05D2260/98

  Lubrication · CPC title

• F02C7/224

  Heating fuel before feeding to the burner · CPC title

• F02C7/06 Primary

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

• F05D2260/213

  by the provision of a heat exchanger within the cooling circuit · CPC title