Field of the Invention
The field of the invention relates to heat sinks, and more particularly to heat pipes for use in aviation and aerospace.
Description of the Related Art
Passive heat transfer systems are not typically used in today's aeronautic platforms due to hydrostatic pressure requirements for such systems. For example, heat pipes using an internal wick structure for return of a working fluid from an evaporator end to a condenser end, such as that illustrated in
Thus, there is a critical need to provide evaporative cooling of a heat source such as power electronics in a high-gravity (g) environment without consuming excess electrical power and without introducing unnecessary weight.
An osmotic transport apparatus includes a heat conducting chamber having an inner wall, a heat absorption end and a heat dissipation end, an osmotic membrane extending substantially longitudinally along an inner wall of the heat conducting chamber from the heat absorption end to the heat dissipation end, a liquid salt solution enclosed in the osmotic membrane, and an inner vapor cavity so that when heat is applied to the heat absorption end, vapor is expelled from the osmotic membrane at the heat absorption end, is condensed on the osmotic membrane at the heat dissipation end, and is drawn into the osmotic membrane at the heat dissipation end for passive pumping transport back to the heat absorption end as more condensate is drawn through the osmotic membrane. The apparatus may also include a heat conductive mesh disposed against and restraining axial movement of the osmotic membrane. The osmotic membrane may be a first closed osmotic membrane tube. A second closed osmotic membrane tube may extend substantially longitudinally within the heat conducting chamber from the heat absorption end to the heat dissipation end. A plurality of heat-conductive fibers may be interspersed between the first and second osmotic membrane tubes. The salt solution may be selected from the group consisting of NaCl and Na2SO4, and the salt solution may have a concentration of 0.1-1.5 mol. In embodiments, the osmotic membrane may have a circular cross section. In other embodiments, the osmotic membrane may have an annular cross section.
An osmotic transport cooling method may include accepting heat into a liquid salt solution disposed in respective interiors of a plurality of osmotic membranes at a heat absorption end of a heat conducting chamber, expelling vapor from the respective interiors in response to the introducing of heat into the liquid salt solution to form a concentrated liquid salt solution, transporting the expelled vapor through an inner vapor cavity disposed longitudinally within the heat conducting chamber to a heat dissipation end of the heat conducting chamber, accepting condensate into the respective interiors of the plurality of osmotic membranes at the heat dissipation end in response to osmotic pumping of the condensate through respective walls of the respective plurality of osmotic membranes into the liquid salt solution to form a diluted liquid salt solution, and transporting the diluted liquid salt solution back to the heat absorption end in response to osmotic pumping action resulting from accepting the condensate into the respective interiors at the heat dissipation end. The method may also include radially restraining the osmotic membranes using a rigid and heat conducting mesh. The plurality of osmotic membranes may include a plurality of tubular osmotic membranes. In embodiments, the method may include accepting excess heat through an outer wall of the heat conducting chamber into a heat sink. Accepting heat into the liquid salt solution disposed in respective interiors of a plurality of osmotic membranes at a heat absorption end further may also include transporting heat from an interior surface of the heat conducting chamber, through a plurality of metallic fibers and into the respective interiors of the plurality of osmotic membranes. The diluted salt solution may include a salt solution selected from the group consisting of NaCl and Na2SO4. The salt solution may have a concentration of 0.1-1.5 mol.
An osmotic transport apparatus may include a cylindrical heat conducting chamber, a plurality of closed osmotic membranes extending from a first end to a second end of the heat conducting chamber, and an inner vapor cavity extending from the first end to the second end. Each of the plurality of closed osmotic membranes may have a cross section selected from the group consisting of: circular and annular. A heat source may also be included that faces an exterior wall of the heat conducting chamber at the first end. The apparatus may also include vapor disposed adjacent the plurality of closed osmotic membranes at the first end and condensate on the plurality of closed osmotic membranes at the second end.
The components in the figures are not necessarily to scale, emphasis instead being placed upon illustrating the principals of the invention. Like reference numerals designate corresponding parts throughout the different views.
The inventive system described herein is able to constantly transfer liquid and heat in high-gravity (g) environment without consuming electrical power, benefitting from its exceptional osmotic transport mechanism. This invention is able to create a new, light-weight and highly efficient heat transfer system and technology, satisfying the needs of the aeronautic industry. In one example, the estimated heat carrying capability may be 3,500 W over a maximum heat transfer distance of 10 m under 10 g gravitational force.
An osmotic membrane 308 may extend circumferentially and substantially longitudinally along the inner wall 304 of the heat conducting chamber from a heat absorption end 309 to a heat dissipation end 310. As described herein, the heat absorption end 309 is generally the end of the osmotic transport system 300 that accepts excess heat (indicated with arrows) from the heat source (not shown) such as power electronics. The heat dissipation end 310 may be used to accept excess heat. Each end of the osmotic membrane 308 is closed (i.e., a “closed osmotic membrane”) to enclose a liquid salt solution 312. An inner vapor cavity 314 is established by the osmotic membrane 308 as it extends circumferentially about the inner surface 304 of the heat conducting chamber 302 for transporting vapor 316. The membrane material has an inner surface 320 and serves to separate the salt solution from the vapor and solvent condensate 318. The system 300 may also include a heat conductive mesh 322 disposed against and restraining radial movement of the plurality of osmotic membranes 308. The heat conductive mesh 322 may prevent large deformation of the membrane when under internal pressure during operation. For example, if nucleate boiling is accidentally triggered inside the osmotic membrane 308, the heat conductive mesh 322 would constrain the expansion tendency of the osmotic membrane 308.
When operating against gravity, the heat absorption end (the evaporator) 309 of the heat conducting chamber 302 absorbs heat (indicated by arrows). The absorbed heat serves to evaporate a portion of solvent of the salt solution 312 in the osmotic membrane 308 to create vapor. The vapor passes through the semi-permeable membrane of the osmotic membrane 308 and into the inner vapor cavity 314. Driven by a saturation pressure difference, the vapor 316 flows down to the heat dissipation end 310 which functions as a lower condenser for condensing the vapor 316 into solvent condensate 318. Such condensing of the vapor may also induce solvent vapor flow downward with a vacuum effect on the evaporator side. After releasing latent heat as the condensate is formed, the solvent condensate 318 is sucked into an interior of the osmotic membrane 308 under osmotic pressure and into the solution 312. In response to the passive and forceful entrance into the osmotic membrane 308, the chamber having only a limited ability to expand under such pressures, liquid is transported against the high hydrostatic pressure back to the evaporator section (heat absorption end 309). Because of its symmetrical structure of the osmotic transport system 300, multiple heat or cooling sources may be applied to the exterior surface 306 while maintaining the systems ability to overcome high hydrostatic pressure for liquid transport between heat absorption and heat dissipation regions. In addition, vapor flow may automatically balance the saturation pressure and temperature, providing a uniform temperature distribution along the osmotic transport system 300.
In one embodiment, the salt solution may be Sodium Sulfate (Na2SO4). Solution concentration may vary between 0.1 to 1.5 mol.
In one implementation, the osmotic membrane tubes may be organic polymer based, such as the ultrafiltration (UF) family of membranes offered by the GE Power division of GE Corporation in Vista, Calif. With such a membrane material implementation, the salt solution may be Sodium Sulfate (Na2SO4) having a concentration of approximately between 0.1 to 1.5 mol. In other implementations, such as those using Sodium Chloride, a reverse osmosis (RO) membrane may be used to obtain a desired passive osmotic pumping action. In other embodiments, a nanofiltration (NF) or microfiltration (MF) material may be used, such as found in GE Corporation's spiral wound membranes. For embodiments having membrane tubes, the membranes may be configured having an inner diameter of approximately 1-2 mm. The length of the membrane tubes may correspond to the chosen application, but in one non-limiting example, may extend between 0.3 to 10 m. The inner vapor cavity 314 may have a diameter of approximately 1 to 4 cm.
While various implementations of the embodiments have been described, it will be apparent to those of ordinary skill in the art that many more embodiments and implementations are possible that are within the scope of this invention.
This application claims priority to and benefit of U.S. Provisional Application No. 62/263,114 filed Dec. 4, 2015 which is hereby incorporated by reference for all purposes.
Number | Name | Date | Kind |
---|---|---|---|
2506984 | Anderson | May 1950 | A |
3561525 | Baer | Feb 1971 | A |
3563309 | Basiulis | Feb 1971 | A |
3677337 | Midolo | Jul 1972 | A |
3682239 | Abu-Romia | Aug 1972 | A |
3741289 | Moore | Jun 1973 | A |
3779310 | Russell | Dec 1973 | A |
3786861 | Eggers | Jan 1974 | A |
3990502 | Best | Nov 1976 | A |
4043387 | Lamp | Aug 1977 | A |
4135371 | Kesselring | Jan 1979 | A |
4300624 | Minning | Nov 1981 | A |
4331200 | Basiulis | May 1982 | A |
4365664 | Basiulis | Dec 1982 | A |
4422501 | Franklin | Dec 1983 | A |
4441548 | Franklin | Apr 1984 | A |
4470451 | Alario | Sep 1984 | A |
4807697 | Gernert | Feb 1989 | A |
4854379 | Shaubach | Aug 1989 | A |
4862708 | Basiulis | Sep 1989 | A |
4890668 | Cima | Jan 1990 | A |
4934160 | Mueller | Jun 1990 | A |
5358799 | Gardner | Oct 1994 | A |
5685289 | Yogev | Nov 1997 | A |
6220338 | Grandi | Apr 2001 | B1 |
6351951 | Guo | Mar 2002 | B1 |
6438992 | Smith et al. | Aug 2002 | B1 |
6446706 | Rosenfeld | Sep 2002 | B1 |
6474100 | Smith | Nov 2002 | B1 |
6533781 | Heim et al. | Mar 2003 | B2 |
7043935 | Hunter | May 2006 | B2 |
7137442 | Kawahara | Nov 2006 | B2 |
7265979 | Erturk | Sep 2007 | B2 |
7875066 | Cohen et al. | Jan 2011 | B2 |
8109325 | Kroliczek | Feb 2012 | B2 |
9157659 | Lowenstein | Oct 2015 | B2 |
9593866 | Baldwin | Mar 2017 | B2 |
9651311 | Hsieh et al. | May 2017 | B2 |
9693484 | Shelnutt et al. | Jun 2017 | B2 |
9804607 | Coleman | Oct 2017 | B1 |
10271458 | Asai | Apr 2019 | B2 |
20030062149 | Goodson | Apr 2003 | A1 |
20050286227 | Erturk | Dec 2005 | A1 |
20060039113 | Cheng | Feb 2006 | A1 |
20070144716 | Doh | Jun 2007 | A1 |
20080283221 | Terp | Nov 2008 | A1 |
20090020269 | Chang | Jan 2009 | A1 |
20100254090 | Trautman | Oct 2010 | A1 |
20110146956 | Stroock | Jun 2011 | A1 |
20120241122 | Xiang | Sep 2012 | A1 |
20130011332 | Boyden | Jan 2013 | A1 |
20130312939 | Uchida | Nov 2013 | A1 |
20140197355 | Ram | Jul 2014 | A1 |
20150140367 | Yagi et al. | May 2015 | A1 |
20170141724 | O'Donnell et al. | May 2017 | A1 |
20170229375 | Haj-Hariri | Aug 2017 | A1 |
20180051937 | Thiers | Feb 2018 | A1 |
20180135880 | Moghaddam et al. | May 2018 | A1 |
20180142958 | Hanganu | May 2018 | A1 |
Number | Date | Country |
---|---|---|
2334628 | Dec 1999 | CA |
2127143 | Apr 1984 | GB |
57047189 | Mar 1982 | JP |
57047190 | Mar 1982 | JP |
2004077051 | Mar 2004 | JP |
20040017211 | Feb 2004 | KR |
WO-2016047098 | Mar 2016 | WO |
Entry |
---|
Thermal Degradation—Schniewind (1989). |
Heat Pipes—Review, Opportunities and Challenges—Faghri (2014). |
Membranes—University of Mississippi (Nov. 2014) (Year: 2014). |
WO-9964147-A2 (Year: 1999). |
Doshi and Eastman,“Osmotic Heat Pipe: Problems and Promises”, Letters and Heat and Mass Transfer, vol. 4, pp. 429-436, 1977, Pergamon Press, Great Britain. |
Ippohshi and Imura, “Study of Heat Transport of an Osmotic Heat Pipe: part 1. Effects of the Initial Concentration on Heat Transport Limits”, Heat Transfer Asian Research 29, 2000. |
Ippohshi and Imura, “Study of Heat Transport of an Osmotic Heat Pipe: Part 2 Flow in the Membrane Module”, Heat Transfer Asian Research 29 (4), 2000. |
Ippohshi et al. “Fundamental Study on an Osmotic Heat Pipe with a Two-Phase Solution Loop”,Heat pipe Science and Technology, Proceedings of the 11th Int. Heat Pipe Conference, Tokyo-Japan, 1999, pp. 414-419. |
Kazadi et al. “A Membrane-Enabled Solar Heat Pipe for Solar Thermal Water Heating”, The 2nd International Symposium On Environment Friendly Energies And Applications, IEEE, 2012, pp. 173-178. |
Number | Date | Country | |
---|---|---|---|
20170234624 A1 | Aug 2017 | US |
Number | Date | Country | |
---|---|---|---|
62263114 | Dec 2015 | US |