Flow draining enhancement system for engine sump cavities

US12331667B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12331667-B2
Application numberUS-202318314900-A
CountryUS
Kind codeB2
Filing dateMay 10, 2023
Priority dateMay 10, 2023
Publication dateJun 17, 2025
Grant dateJun 17, 2025

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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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  7. Citations and related patents

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Abstract

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Scavenge systems for a gas turbine engine including a valve positioned at a first drainage outlet of an enclosure to selectively open and evacuate liquid from the cavity through the first drainage outlet in response to the valve being submerged in liquid are provided. Methods of reducing suction of air from an enclosure of a cavity of a gas turbine engine are further provided.

First claim

Opening claim text (preview).

What is claimed is: 1. An oil sump system for a gas turbine engine, the oil sump system comprising: a first oil drainage outlet in a surface of an enclosure of the oil sump system; a second oil drainage outlet in the surface, the second oil drainage outlet in liquid communication with the first oil drainage outlet, wherein the surface is substantially unobstructed between at least the first oil drainage outlet and the second oil drainage outlet such that liquid is free to flow between the first oil drainage outlet and the second oil drainage outlet along the surface due to, at least in part, an orientation of the gas turbine engine; wherein an entry of the first oil drainage outlet, an entry of the second oil drainage outlet, and the surface extending therebetween are substantially coplanar; a suction pump in liquid communication with the first oil drainage outlet and the second oil drainage outlet; and a valve positioned at the first oil drainage outlet to selectively open and evacuate the liquid from the enclosure of the oil sump system through the first oil drainage outlet in response to the valve being submerged in the liquid, the liquid accumulating on the surface when the gas turbine engine is at level flight. 2. The oil sump system of claim 1 , wherein the valve is a float valve. 3. The oil sump system of claim 2 , wherein a float of the float valve is buoyant in the liquid. 4. The oil sump system of claim 1 , wherein the liquid is a lubricant. 5. The oil sump system of claim 1 , further comprising a second valve positioned at the second oil drainage outlet to selectively open and evacuate fluid from the enclosure of the oil sump system through the second oil drainage outlet in response to the second valve being submerged in the liquid. 6. The oil sump system of claim 1 , comprising a third oil drainage outlet in the surface, the third oil drainage outlet in liquid communication with the first oil drainage outlet and the second oil drainage outlet, the third oil drainage outlet being unobstructed such that the third oil drainage outlet is open during all operating conditions of the gas turbine engine and the liquid is free to drain out of the third oil drainage outlet during all operating conditions of the gas turbine engine. 7. The oil sump system of claim 6 , wherein the third oil drainage outlet is positioned at a location in the surface of the enclosure of the oil sump system that is farther from the suction pump along a scavenge conduit in fluid communication with the suction pump and the third oil drainage outlet than the first oil drainage outlet and the second oil drainage outlet, the first oil drainage outlet and the second oil drainage outlet in fluid communication with the suction pump by the scavenge conduit. 8. The oil sump system of claim 1 , wherein the first oil drainage outlet is positioned at a location in the surface of the enclosure of the oil sump system that is closer to the suction pump along a scavenge conduit in fluid communication with the suction pump and the first oil drainage outlet than the second oil drainage outlet, the first oil drainage outlet and the second oil drainage outlet in fluid communication with the suction pump by the scavenge conduit. 9. The oil sump system of claim 1 , wherein the surface of the enclosure is a bottom surface of the enclosure, and wherein the first oil drainage outlet and the second oil drainage outlet are axially spaced apart from one another along the bottom surface. 10. The oil sump system of claim 1 , wherein the enclosure includes an aft wall, a forward wall axially spaced apart from the aft wall, and a bottom wall extending between and interconnecting bottom ends of the aft wall and the forward wall, and wherein the bottom wall defines the surface through which the first oil drainage outlet and the second oil drainage outlet are formed. 11. A scavenge system for a gas turbine engine, the scavenge system comprising: a first drainage outlet in a surface of an enclosure of a cavity in the gas turbine engine; a second drainage outlet in the surface, the second drainage outlet in liquid communication with the first drainage outlet, wherein an entry of the first drainage outlet, an entry of the second drainage outlet, and the surface extending therebetween are substantially coplanar; a suction pump in liquid communication with the first drainage outlet and the second drainage outlet; and a valve positioned at the first drainage outlet to selectively open and evacuate liquid from the cavity through the first drainage outlet in response to the valve being submerged in the liquid, the liquid accumulating on the surface when the gas turbine engine is at level flight, and wherein the second drainage outlet is unobstructed such that the second drainage outlet is open during all operating conditions of the gas turbine engine and the liquid is free to drain out of the second drainage outlet during all operating conditions of the gas turbine engine. 12. The scavenge system of claim 11 , wherein the valve is a float valve. 13. The scavenge system of claim 11 , wherein the liquid is a lubricant. 14. The scavenge system of claim 11 , further comprising a third drainage outlet in the surface, the third drainage outlet in liquid communication with the first drainage outlet and the second drainage outlet. 15. The scavenge system of claim 14 , further comprising a second valve positioned at the third drainage outlet to selectively open and evacuate the liquid from the cavity through the third drainage outlet in response to the second valve being submerged in the liquid, and wherein the first drainage outlet and the third drainage outlet are positioned closer to the suction pump along a scavenge conduit than the second drainage outlet, the first drainage outlet, the second drainage outlet, and the third drainage outlet being in fluid communication with the suction pump by the scavenge conduit. 16. The scavenge system of claim 15 , wherein the surface is substantially unobstructed between at least the first drainage outlet, the second drainage outlet, and the third drainage outlet such that liquid is free to flow between the first drainage outlet, the second drainage outlet, and the third drainage outlet along the surface due to, at least in part, an orientation of the gas turbine engine. 17. The scavenge system of claim 11 , wherein the first drainage outlet is positioned at a location in the surface of the enclosure that is closer to the suction pump along a scavenge conduit in fluid communication with the suction pump and the first drainage outlet than the second drainage outlet, the first drainage outlet and the second drainage outlet in fluid communication with the suction pump by the scavenge conduit. 18. The scavenge system of claim 11 , wherein the surface is substantially unobstructed between at least the first drainage outlet and the second drainage outlet such that liquid is free to flow between the first drainage outlet and the second drainage outlet along the surface due to, at least in part, an orientation of the gas turbine engine. 19. The scavenge system of claim 11 , wherein the surface of the enclosure is a bottom surface of the enclosure, and wherein the first drainage outlet and the second drainage outlet are axially spaced apart from one another along the bottom surface. 20. The scavenge system of claim 11 , wherein the enclosure includes an aft wall, a forward wall axially spaced apart from the aft wall, and a bottom wall extending between and interconne

Assignees

Inventors

Classifications

  • F01M11/062Primary

    Accommodating movement or position of machines or engines, e.g. dry sumps · CPC title

  • Oilsumps · CPC title

  • concerning lubricant level · CPC title

  • Sump drainage devices, e.g. valves, plugs · CPC title

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What does patent US12331667B2 cover?
Scavenge systems for a gas turbine engine including a valve positioned at a first drainage outlet of an enclosure to selectively open and evacuate liquid from the cavity through the first drainage outlet in response to the valve being submerged in liquid are provided. Methods of reducing suction of air from an enclosure of a cavity of a gas turbine engine are further provided.
Who is the assignee on this patent?
Rolls Royce Nam Tech Inc
What technology area does this patent fall under?
Primary CPC classification F01M11/062. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jun 17 2025 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).