Centrifugal debris pre-separator for turbine engine oil filter

Patent metadata

Field	Value
Publication number	US-11970960-B2
Application number	US-202117329473-A
Country	US
Kind code	B2
Filing date	May 25, 2021
Priority date	May 8, 2018
Publication date	Apr 30, 2024
Grant date	Apr 30, 2024

Abstract

A fluid filtration assembly (FFA) includes a housing having a thickness defined between an internal surface and an external surface, the housing receiving a filter and defining an outer annular flow passage between an outer surface of the filter and the internal surface of the housing; an inlet pipe communicates with the FFA and injects a fluid into the housing to impart a centrifugal force; an outlet pipe communicates with the FFA and discharges the fluid from the housing; and a collection area disposed towards an end of the outer annular flow passage collects particulate matter from the fluid; wherein a width of the outer annular flow passage increases towards the collection area.

First claim

What is claimed is:

1. A fluid filtration assembly, comprising:
a housing having a thickness defined between an internal surface of the housing and an external surface of the housing, the housing extending in an axial direction from a first end to a second end, the external surface defining an outer diameter of the housing, the outer diameter remaining constant from the first end to the second end;
a first filter having a first radially outer surface and a first radially inner surface, the first filter disposed in the housing, the first radially outer surface and the internal surface of the housing defining an outer annular flow passage;
a cavity disposed radially inward of the first filter;
an inlet pipe in fluid communication with the outer annular flow passage, the inlet pipe disposed at the first end, the inlet pipe disposed substantially tangentially to the internal surface of the housing;
an outlet pipe in fluid communication with the cavity to discharge the fluid from the housing, the outlet pipe disposed at the first end; and
a collection area disposed at the second end of the housing, the collection area configured to collect particulate matter from the fluid, wherein:
the fluid is configured to flow radially from the outer annular flow passage through the first radially outer surface of the first filter and the first radially inner surface of the first filter into the cavity,
the fluid is configured to flow axially from the cavity out the outlet pipe, and
in response to injecting the fluid substantially tangentially to the internal surface of the housing through the inlet pipe, the particulate matter is forced against the internal surface of the housing within the outer annular flow passage, wherein the thickness of the housing gradually decreases towards the collection area.

2. The fluid filtration assembly of claim 1 , wherein a width of the outer annular flow passage increases towards the collection area to augment a centrifugal force.

3. The fluid filtration assembly of claim 1 , wherein the fluid filtration assembly is an oil filtration assembly and the fluid is an oil.

4. The fluid filtration assembly of claim 1 , further comprising a drain plug proximate an end cap near the collection area.

5. The fluid filtration assembly of claim 1 , further comprising a turning vane assembly proximate the inlet pipe.

6. The fluid filtration assembly of claim 1 , further comprising a second filter configured within the first filter.

7. The fluid filtration assembly of claim 1 , wherein the thickness gradually decreases from a first section to a second section of the fluid filtration assembly along an overlength of the housing.

8. A gas turbine engine, comprising:
a fan section configured to induce air from a surrounding environment into the gas turbine engine;
a compressor section in fluid communication with the fan section and configured to compress the air received from the fan section;
a combustor section in fluid communication with the compressor section and configured to ignite a fuel-air mixture to generate combustion gases;
a turbine section in fluid communication with the combustor section; and
a debris capture device to remove particulate matter from fluids associated with lubricating rotating components of the gas turbine engine, comprising:
an inlet pipe disposed substantially tangentially to an internal surface of a housing;
an outlet pipe; and
an oil filtration assembly, comprising:
the housing having a thickness defined between the internal surface of the housing and an external surface of the housing, the housing extending in an axial direction from a first end to a second end, the inlet pipe and the outlet pipe both disposed at the first end, the external surface defining an outer diameter of the housing, the outer diameter remaining constant from the first end to the second end;
a first filter having a first radially outer surface and a first radially inner surface, the first filter disposed in the housing, the first radially outer surface and the internal surface of the housing defining an outer annular flow passage;
a cavity disposed radially inward of the first filter, the cavity in fluid communication with the outer annular flow passage; and
a collection area disposed at the second end of the housing, the collection area configured to collect the particulate matter from an oil, wherein:
the inlet pipe is in fluid communication with the outer annular flow passage,
the outlet pipe is in fluid communication with the cavity to discharge the oil from the housing,
the oil is configured to flow radially from the outer annular flow passage through the first radially outer surface of the first filter and the first radially inner surface of the first filter into the cavity,
in response to injecting the oil substantially tangentially to the internal surface of the housing, the particulate matter is forced against the internal surface of the housing within the outer annular flow passage, and
the thickness of the housing gradually decreases towards the collection area.

9. The gas turbine engine of claim 8 , wherein a width of the outer annular flow passage increases towards the collection area to augment a centrifugal force.

10. The gas turbine engine of claim 8 , further comprising a drain plug proximate an end cap near the collection area.

11. The gas turbine engine of claim 8 , further comprising a turning vane assembly proximate the inlet pipe.

12. The gas turbine engine of claim 8 , further comprising a second filter configured within the first filter.

Assignees

• Raytheon Tech Corp
• Rtx Corp

Inventors

• Stachowiak David Allen

Classifications

• F01M11/03 Primary

  Mounting or connecting of lubricant purifying means relative to the machine or engine; Details of lubricant purifying means (filters B01D) · CPC title

• B01D21/265

  by using a vortex inducer or vortex guide, e.g. coil (B01D21/0054 takes precedence) · CPC title

• B01D29/21

  with corrugated, folded or wound sheets · CPC title

• B01D29/33

  arranged for inward flow filtration · CPC title

• B01D29/58

  arranged concentrically or coaxially · CPC title