Method and apparatus for decongealing a lubricating fluid in a heat exchanger apparatus

Patent metadata

Field	Value
Publication number	US-9593594-B2
Application number	US-201414502750-A
Country	US
Kind code	B2
Filing date	Sep 30, 2014
Priority date	Sep 30, 2014
Publication date	Mar 14, 2017
Grant date	Mar 14, 2017

Abstract

A decongealing channel for use in a heat exchanger apparatus, including a supersaturated solution contained therein and an actuation component in fluid communication with a lubricating fluid coupled to the decongealing channel. The actuation component is responsive to a change in pressure exerted thereon by the lubricating fluid so as to actuate an exothermic response in the supersaturated solution. The heat exchanger apparatus is disposed in a bypass fan duct of an aircraft engine. The heat exchanger apparatus including a manifold portion, one or more flow through openings extending therethrough the manifold portion to define one or more flow through channels having contained therein the lubricating fluid. In addition, the manifold portion including one or more additional openings extending therethrough to define one or more decongealing channels. Further disclosed is an engine including the heat exchanger apparatus and a method of decongealing a lubricating fluid in the heat exchanger apparatus.

First claim

What is claimed is:

1. A decongealing channel for use in a heat exchanger apparatus comprising:
a decongealing channel body enclosing therein a supersaturated solution; and
an actuation component coupled to the decongealing channel body and in fluid communication with a lubricating fluid, the actuation component responsive to a change in a fluid pressure exerted thereon by the lubricating fluid so as to actuate an exothermic response in the supersaturated solution.

2. The decongealing channel of claim 1 , wherein the actuation component includes a linearly configured piston drive and a deformable disk.

3. The decongealing channel of claim 2 , wherein the linearly configured piston drive includes a piston and a spring, and wherein the actuation component is configured to linearly move the piston to deform the deformable disk in response to a fluid pressure exerted thereon by the lubricating fluid.

4. The decongealing channel of claim 3 , wherein the deformable disk is configured to deform relative to the supersaturated solution so as to initiate the exothermic response in the supersaturated solution.

5. The decongealing channel of claim 3 , wherein the supersaturated solution is sodium acetate trihydrate.

6. The decongealing channel of claim 1 , wherein the supersaturated solution is comprised of a solution capable of producing an exothermic reaction and providing heat that can be conducted to a congealed lubricating fluid.

7. The decongealing channel of claim 1 , wherein the decongealing channel is configured for use in an aerospace application.

8. The decongealing channel of claim 1 , wherein the decongealing channel is configured for use in an oil cooling system of an aircraft engine.

9. A heat exchanger apparatus for use in an oil cooling system of an aircraft engine comprising:
a manifold portion including a radially inner surface and a radially outer surface, an upstream wall and an opposite downstream wall;
one or more flow through openings enclosed by the manifold portion and extending therethrough, the one or more flow through openings defining one or more flow through channels having contained therein a lubricating fluid; and
one or more additional openings enclosed by the manifold portion and extending therethrough, the one or more additional openings defining one or more decongealing channels, each of the one or more decongealing channels comprising:
a decongealing channel body enclosing therein a supersaturated solution; and
an actuation component coupled to the decongealing channel body and in fluid communication with the lubricating fluid, the actuation component responsive to a change in a fluid pressure exerted thereon by the lubricating fluid so as to actuate an exothermic response in the supersaturated solution.

10. The heat exchanger apparatus of claim 9 , wherein the heat exchanger apparatus has a circumferential and axial profile that conforms to a circumferential and axial profile of a fan duct at a location within the fan duct where the heat exchanger apparatus is mounted.

11. The heat exchanger apparatus of claim 9 , further comprising a plurality of cooling fins formed unitarily with the manifold portion and positioned perpendicular to the one or more flow through openings and the one or more additional openings.

12. The heat exchanger apparatus of claim 9 , wherein the actuation component includes a linearly configured piston drive and a deformable disk.

13. The heat exchanger apparatus of claim 12 , wherein the linearly configured piston drive includes a piston and a spring, and wherein the actuation component is configured to linearly move the piston to deform the deformable disk in response to a fluid pressure exerted thereon by the lubricating fluid.

14. The heat exchanger apparatus of claim 13 , wherein the deformable disk is configured to deform relative to the supersaturated solution so as to initiate the exothermic response in the supersaturated solution.

15. The heat exchanger apparatus of claim 9 , wherein the supersaturated solution is comprised of a solution capable of producing an exothermic reaction and providing heat that can be conducted to the lubricating fluid contained therein the one or more flow through channels so as to provide decongealing of the lubricating fluid.

16. The heat exchanger apparatus of claim 15 , wherein the supersaturated solution is sodium acetate trihydrate.

17. An engine comprising:
a fan assembly;
a core engine downstream of the fan assembly;
a fan casing circumscribing the fan assembly;
a booster casing circumscribing the core engine such that a bypass duct is defined between the fan casing and the booster casing; and
an arcuate heat exchanger apparatus coupled to one of the fan casing or the booster casing, the arcuate heat exchanger apparatus comprising:
a manifold portion including a radially inner surface and a radially outer surface, an upstream wall and an opposite downstream wall;
one or more flow through openings enclosed by the manifold portion and extending therethrough, the one or more flow through openings defining one or more flow through channels having contained therein a lubricating fluid; and
one or more additional openings enclosed by the manifold portion and extending therethrough, the one or more additional openings defining one or more decongealing channels, each of the one or more decongealing channels comprising:
a decongealing channel body enclosing therein a supersaturated solution; and
an actuation component coupled to the decongealing channel body and in fluid communication with the lubricating fluid, the actuation component responsive to a change in a fluid pressure exerted thereon by the lubricating fluid so as to actuate an exothermic reaction in the supersaturated solution.

18. The engine of claim 17 , wherein the supersaturated solution is comprised of a solution capable of producing the exothermic reaction and providing heat that can be conducted to the lubricating fluid contained therein the one or more flow through channels so as to provide decongealing of the lubricating fluid.

19. The engine of claim 18 , wherein the supersaturated solution is sodium acetate trihydrate.

20. A method of decongealing a lubricating fluid in a heat exchanger apparatus, the method comprising:
actuating an exothermic reaction in a supersaturated solution contained within a decongealing channel as a result of a rise in pressure of a congealed lubricating fluid impinging thereon an actuation component;
conducting heat generated by the exothermic reaction from within the decongealing channel to a congealed lubricating fluid disposed in an adjacent flow through channel; and
returning the actuation component to a home position and the supersaturated solution to a metastable state as the congealed lubricating fluid decongeals and decreases in pressure.

Assignees

• Gen Electric

Inventors

• Diaz Carlos Enrique
• Gerstler William Dwight
• Storage Michael Ralph

Classifications

• F28D20/003

  using thermochemical reactions · CPC title

• F02C7/00

  Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title

• F01D25/18 Primary

  Lubricating arrangements (of machines or engines in general F01M) · CPC title

• Y02E60/14

  Thermal energy storage · CPC title