IP Library › Granted Patent US 12,311,330
Granted Patent B2
US 12,311,330 · App. 18/054,735 · Granted May 27, 2025

Self-cleaning conduits for hydrocarbon fluids

Inventors: Ravindra Shankar Ganiger (Bengaluru, IN); Hiranya Nath (Bengaluru, IN); Thomas D. Woodrow (Wyoming, OH); Scott Alan Schimmels (Miamisburg, OH); Arvind Namadevan (Bengaluru, IN); Mohan Raju (Bengaluru, IN); Subramani Adhiachari (Bengaluru, IN); Prasant Bilaiya (Bengaluru, IN); Rajesh Kumar (Bengaluru, IN)
Assignee: GENERAL ELECTRIC COMPANY
B01J19/0026F16N39/00F16N2210/02
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,311,330
App. No.
18/054,735
Granted
May 27, 2025
Kind
B2
Abstract

A self-cleaning conduit for a hydrocarbon fluid. The conduit includes a tube and a mesh. The tube has an interior surface defining a flow passage for the hydrocarbon fluid. The mesh is positioned within the flow passage to abut the interior surface and movable along the interior surface to break-up deposits on the interior surface. The mesh is characterized by a mesh activation parameter (MAP) from one ten thousandths to six tenths.

Claims (31)

1. A self-cleaning conduit for a hydrocarbon fluid, the conduit comprising:

a tube having an interior surface defining a flow passage for the hydrocarbon fluid; and

a mesh positioned within the flow passage to abut the interior surface and movable along the interior surface to break-up deposits on the interior surface, the mesh being characterized by a mesh activation parameter (MAP) from one ten thousandths to six tenths.

2. The conduit of claim 1 , wherein the mesh activation parameter (MAP) is from one tenth to three tenths.

3. The conduit of claim 1 , wherein the hydrocarbon fluid is oil, and

wherein the conduit is configured to be operated at a working temperature ratio from four tenths to one.

4. The conduit of claim 1 , wherein the mesh is characterized by an absolute value of a deformation factor from one tenth to nine tenths.

5. The conduit of claim 1 , wherein the mesh is characterized by an absolute value of a deformation factor from seven tenths to nine tenths.

6. The conduit of claim 1 , wherein the mesh has a mesh density between one tenth and one.

7. The conduit of claim 1 , wherein the mesh has a mesh density from two tenths to five tenths.

8. The conduit of claim 1 , wherein the mesh is a sleeve.

9. The conduit of claim 1 , wherein the mesh is formed of a shape memory alloy.

10. The conduit of claim 9 , wherein the shape memory alloy is one of a nickel-titanium alloy, a cobalt-nickel-aluminum alloy, or a nickel-iron-gallium alloy.

11. The conduit of claim 9 , wherein the tube is a metal having a Young's modulus, the shape memory alloy has a Young's modulus, and a ratio of the Young's modulus of the mesh to the Young's modulus of the tube is a stiffness ratio, the stiffness ratio being from two tenths to ninety-six hundredths.

12. The conduit of claim 11 , wherein the stiffness ratio is from five tenths to seven tenths.

13. A lubrication system comprising:

an oil reservoir configured to hold oil; and

an oil sump fluidly connected to the oil reservoir by the conduit of claim 1 , wherein the hydrocarbon fluid is the oil.

14. The lubrication system of claim 13 , further comprising a pump fluidly connected to each of the oil reservoir and the oil sump and configured to circulate the oil through the conduit.

15. A gas turbine engine comprising:

the lubrication system of claim 13 ;

a compressor section including at least one rotor, the at least one rotor being configured to compress air flowing therethrough;

a combustion section configured to mix fuel with the compressed air and to combust the mixture of fuel and air to generate combustion products; and

a turbine section including at least one turbine configured to be driven by the combustion products,

wherein the compressor section, the combustion section, and the turbine section together define at least part of a core air flow path, the conduit being located in the core air flow path.

16. The gas turbine engine of claim 15 , further comprising at least one frame, the frame including at least one service tube assembly, the service tube assembly having the conduit.

17. The gas turbine engine of claim 16 , wherein the frame includes a plurality of service tube assemblies.

18. The gas turbine engine of claim 16 , wherein the frame is a turbine rear frame.

19. The gas turbine engine of claim 16 , further comprising a shaft connecting the at least one turbine with the at least one rotor; and

a bearing supporting the shaft, the frame providing structural load paths from the bearing.

20. The gas turbine engine of claim 19 , wherein the lubrication system is configured to provide oil to the bearing.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 11, 2022
From: GANIGER, RAVINDRA SHANKAR; NATH, HIRANYA; WOODROW, THOMAS D.; SCHIMMELS, SCOTT ALAN; NAMADEVAN, ARVIND; RAJU, MOHAN; ADHIACHARI, SUBRAMANI; BILAIYA, PRASANT; KUMAR, RAJESH
To: GENERAL ELECTRIC COMPANY
Reel/Frame 061742/0876 →
Priority Claims (1)
IN 202211037978 · Jul 1, 2022 · national
Continuity (1)
Related Publication 20240001323A1 · Jan 4, 2024
References Cited (42)
US 4481154A · Gough et al. · 1984 [cited by applicant]
US 5194231A · Gough et al. · 1993 [cited by applicant]
US 5725955A · Tawil et al. · 1998 [cited by applicant]
US 5829246A · Abrams et al. · 1998 [cited by applicant]
US 6125624A · Prociw · 2000 [cited by applicant]
US 6431837B1 · Velicki · 2002 [cited by applicant]
US 6523350B1 · Mancini et al. · 2003 [cited by applicant]
US 6569255B2 · Sivacoe · 2003 [cited by applicant]
US 6579628B2 · Takeuchi et al. · 2003 [cited by applicant]
US 6715292B1 · Hoke · 2004 [cited by applicant]
US 6808816B2 · Mancini et al. · 2004 [cited by applicant]
US 6989197B2 · Schneider · 2006 [cited by applicant]
US 7326469B2 · Dye et al. · 2008 [cited by applicant]
US 7431981B2 · Schneider · 2008 [cited by applicant]
US 8104793B2 · Browne et al. · 2012 [cited by applicant]
US 8177488B2 · Manteiga et al. · 2012 [cited by applicant]
US 8291710B2 · Webster · 2012 [cited by applicant]
US 8298656B2 · Schneider · 2012 [cited by applicant]
US 8529849B2 · Pranda et al. · 2013 [cited by applicant]
US 9062563B2 · Varanasi et al. · 2015 [cited by applicant]
US 9341117B2 · Remer et al. · 2016 [cited by applicant]
US 10100944B2 · Calkins et al. · 2018 [cited by applicant]
US 10196934B2 · Khan et al. · 2019 [cited by applicant]
US 10683807B2 · McMasters et al. · 2020 [cited by applicant]
US 11143170B2 · Foutch · 2021 [cited by applicant]
US 11661891B1 · Janakiraman et al. · 2023 [cited by applicant]
US 20100266770A1 · Mazany et al. · 2010 [cited by applicant]
US 20170370376A1 · Kray et al. · 2017 [cited by applicant]
CN 103977996B · 2016 [cited by applicant]
CN 109070152A · 2018 [cited by applicant]
CN 111303847A · 2020 [cited by applicant]
CN 113532189A · 2021 [cited by applicant]
GB 2555598A · 2018 [cited by applicant]
JP 2015014265A · 2015 [cited by applicant]
WO 2020243394A1 · 2020 [cited by applicant]
Eftifeeva et al., “Two-way shape memory effect in [001]B2-oriented Co—Ni—Al single crystals”, Materials Today: Proceedings 4, 2017, pp. 4789-4796. [cited by applicant]
Dilibal et al., “On the volume change in Co—Ni—Al during pseudoelasticity”, Materials Science and Engineering A 528, 2011, pp. 2875-2881. [cited by applicant]
Li et al., “Martensitic transformation and magnetization of Ni—Fe—Ga ferromagnetic shape memory alloys”, Scripta Materialia 48, 2003, pp. 1255-1258. [cited by applicant]
Sun et al., “Giant negative thermal expansion in Fe—Mn—Ga magnetic shape memory alloys”, Applied Physics Letters 113, 2018, pp. 041903-1-041903-5. [cited by applicant]
Kireeva et al., “Effect of oriented precipitates on shape memory effect and superelasticity in Co—Ni—Ga single crystals”, Acta Materialia 68, 2014, pp. 127-139. [cited by applicant]
Seldin “Stress-Strain Properties of Polycrystalline Graphites in Tension and Compression at Room Temperature”, Carbon, vol. 4, 1966, pp. 177-191. [cited by applicant]
Uchil et al., “Thermal expansion in various phases of Nitinol using TMA”, Physica B: Condensed Matter, vol. 270, Issues 3-4, Oct. 1999, pp. 289-297. [cited by applicant]