WO2010100614A2 - Dispositif passif pour séparer et refroidir un flux d'air - Google Patents
Dispositif passif pour séparer et refroidir un flux d'air Download PDFInfo
- Publication number
- WO2010100614A2 WO2010100614A2 PCT/IB2010/050921 IB2010050921W WO2010100614A2 WO 2010100614 A2 WO2010100614 A2 WO 2010100614A2 IB 2010050921 W IB2010050921 W IB 2010050921W WO 2010100614 A2 WO2010100614 A2 WO 2010100614A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- output pipe
- air output
- insert
- separation chamber
- pipe
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B9/00—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
- F25B9/02—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using Joule-Thompson effect; using vortex effect
- F25B9/04—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using Joule-Thompson effect; using vortex effect using vortex effect
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/04—Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
- H01M8/04007—Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids related to heat exchange
- H01M8/04014—Heat exchange using gaseous fluids; Heat exchange by combustion of reactants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B9/00—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
- F25B9/10—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point with several cooling stages
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/50—Fuel cells
Definitions
- the present invention concerns a passive device for separating and cooling an air stream in a cold air stream and/or a hot air stream.
- active devices meaning devices that use energy to operate on the inflowing air stream (generally at room temperature) , and obtain a higher- temperature air stream (hot air) and/or a lower- temperature air stream.
- the object of the present invention is to manufacture a passive device for separating an inflowing air stream into a cold air stream and/or a hot air stream, with considerable thermal gradient.
- This object is achieved by a device made in agreement with the claim 1.
- the characteristics and the advantages of the device according to the present invention will be clearer from the description provided below by way of example only, in agreement with the attached illustrations, wherein: [0010] - the figure 1 represents an axonometric view of the devices in accordance with the present invention;
- FIG. 1 shows an axonometric partially section view of the device in the figure 1;
- FIG. 1 shows a further axonometric partially section view of the device in the figure 1;
- FIG. 1 shows a further axonometric partially section view of the device in the figure 1;
- FIG. 5 shows an axonometric separate-part view of the device in the figure 1.
- the device 1 comprises an input pipe 6 for the inflow of an air stream under pressure. [0017] The device 1 further comprises an output pipe for cold air 8, for the output of a stream of cold air, meaning air at a temperature below that of the inflowing air stream. [0018] Furthermore, the device 1 comprises an intermediate hot air output pipe 2, for the output of a stream of intermediate hot air, and a final hot air output pipe 4, for the output of a stream of final hot air. [0019] Furthermore, the device 1 has, internally, a first separation chamber 10, into which leads the input pipe 6 and from which branches the intermediate hot air output pipe 2 and a further passage 12.
- the separation chamber 10 has a lateral wall 10a shaped like a spiral, e.g., with axial direction coinciding with the direction of output of the intermediate hot air 2.
- the pattern of the lateral wall 10a is such that the direction of the inflowing air, meaning the direction of the axis of the input pipe 6, is tangent to the initial section of the wall; said wall, proceeding in the direction of air input, evolves like a spiral to again connect with the input pipe 6.
- the air input pipe 6 is coplanar to the intermediate chamber 10, i.e., with the curve defining the spiral wall 10a.
- the intermediate hot air output pipe 2 is perpendicular with the intermediate chamber 10 and perpendicular with the air input pipe 6.
- the lateral wall 10a extends in an axial direction in a convergent way towards the passage opening 12.
- the intermediate hot air output pipe 2 is aligned with the passage 12.
- the internal surface of the wall 10a, lapped during normal operation by the stream of air, is polished, e.g., like a mirror.
- an intermediate hot air stream is channelled which has a temperature above that of the inflowing air stream, while in the passage 12, an intermediate cold air stream is channelled, which has a temperature below that of the inflowing air stream.
- the device 1 also has, internally, a final separation chamber 14, into which leads the passage 12 and from which branch the final hot air output pipe 4 and the cold air output pipe 8.
- the final hot air output pipe 4 and the cold air output pipe 8 are aligned; the passage 12 is perpendicular to these.
- the device 1 has an accommodating compartment and comprises a rotating insert 16.
- the rotating insert has an extension prevalently along an insert axis Z and comprises a head 18 and a tail 20.
- the head and the tail are hollow inside, thus defining an insert pipe 22 in communication with the cold air output pipe 8.
- the insert 16 is positioned so as to be aligned with the insert axis Z with the cold air output pipe 8 and with the final hot air output pipe 4.
- the head 18 is accommodated in the accommodating compartment, so the room remaining in the compartment defines the final separation chamber 14.
- the head 18 of the insert 16 has a head surface 30 substantially perpendicular to the insert axis Z .
- a plurality of slits 32 angled with respect to the tangential direction, in agreement with one another, so as to produce a turbine effect .
- the head 30 comprises a plurality of paddles 34 arranged in circumferential succession, protruding axially from the head surface 30, separated the one from the other circumferentially by said slits 32.
- the head 30 On the surface of the head 30 also opens, preferably in central position, the insert pipe 22 which, on the other hand, emerges towards the cold air output pipe 8. [0038] The head 18 of the insert 16 is stopped up against the wall surrounding the opening of the final hot air output pipe 4.
- a cold air stream is channelled with a temperature below that of the intermediate air stream, while in the final hot air stream, a hot air stream is channelled with a temperature higher than that of the intermediate air stream.
- the device 1 comprises : [0042] - a cover body 100, made up of a plate from which protrudes the intermediate hot air outlet pipe 2;
- the above components are made of plastic material, e.g., by means of moulding or injection moulding.
- the cover body 100 is coupled with the first body 200 on the side of the first separation chamber 10, so as to delimit this.
- the head 18 of the insert 16 is housed in the housing compartment of the first body 200.
- the second body 300 is coupled with the first body 200, on the side of the housing compartment, so the tail
- the separation and refrigeration device described above allows obtaining a considerable temperature gradient between the inflowing stream of air and the outflowing stream of cold air.
- the structure of the device is particularly compact and therefore easy to use even in systems of reduced dimensions.
- the device can be economically made, being made up of simple- geometry pieces, assembled together.
- the device is of reduced dimensions and makes up, when assembled, a transportable whole.
- a fuel cell is an electro-chemical device which allows obtaining electricity directly from certain substances, typically hydrogen and oxygen, without a heat combustion process occurring. The difference in potential stems from the flow of electrons produced during the chemical reaction.
- the device cools the cell down to maintain a high level of efficiency.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Separation By Low-Temperature Treatments (AREA)
Abstract
L'invention porte sur un dispositif passif pour séparer et refroidir (1), comprenant un tuyau d'entrée d'air (6), une première chambre de séparation (10), un tuyau de sortie d'air chaud intermédiaire (2), un passage (12), une chambre de séparation finale (14), un tuyau de sortie d'air chaud final (4), un tuyau de sortie d'air froid (8) et un insert (16) rotatif sous l'action du flux d'air fourni à la chambre de séparation finale (14). Des flux d'air sont canalisés à différentes températures vers le tuyau de sortie d'air froid (8) et vers le tuyau de sortie d'air chaud final (4).
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ITBS2009A000036 | 2009-03-04 | ||
ITBS2009A000036A IT1394495B1 (it) | 2009-03-04 | 2009-03-04 | Dispositivo passivo di separazione e refrigerazione di un flusso di aria |
ITBS2009A000058 | 2009-03-24 | ||
ITBS2009A000058A IT1393497B1 (it) | 2009-03-24 | 2009-03-24 | Cella a combustibile con dispositivo di refrigerazione |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2010100614A2 true WO2010100614A2 (fr) | 2010-09-10 |
WO2010100614A3 WO2010100614A3 (fr) | 2010-11-25 |
Family
ID=42308321
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/IB2010/050921 WO2010100614A2 (fr) | 2009-03-04 | 2010-03-03 | Dispositif passif pour séparer et refroidir un flux d'air |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2010100614A2 (fr) |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2042089C1 (ru) | 1993-07-30 | 1995-08-20 | Николай Ефимович Курносов | Вихревая труба |
US6250086B1 (en) | 2000-03-03 | 2001-06-26 | Vortex Aircon, Inc. | High efficiency refrigeration system |
ITMI20061472A1 (it) | 2006-07-26 | 2008-01-27 | Antonio Lanti | Dispositivo meccanico statico per la separazione dei fluidi a due o piu'uscite a temperatura differenziata e a basso consumo energetico |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3361336A (en) * | 1964-06-23 | 1968-01-02 | Joseph V. Foa | Method of energy separation and apparatus for carrying out the same |
US4051689A (en) * | 1976-06-08 | 1977-10-04 | Macdonald Ronald A | Air separating apparatus |
SU826159A1 (ru) * | 1979-08-06 | 1981-04-30 | Od T I Kholodilnoj Promyshlenn | Многоступенчатая вихревая холодильная установка 1 |
SU1076712A1 (ru) * | 1982-11-15 | 1984-02-29 | Куйбышевский ордена Трудового Красного Знамени политехнический институт им.В.В.Куйбышева | Вихревой холодильник |
JP2007280794A (ja) * | 2006-04-07 | 2007-10-25 | Toyota Motor Corp | 燃料電池システム |
JP2008226676A (ja) * | 2007-03-14 | 2008-09-25 | Toyota Industries Corp | 燃料電池システム |
-
2010
- 2010-03-03 WO PCT/IB2010/050921 patent/WO2010100614A2/fr active Application Filing
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2042089C1 (ru) | 1993-07-30 | 1995-08-20 | Николай Ефимович Курносов | Вихревая труба |
US6250086B1 (en) | 2000-03-03 | 2001-06-26 | Vortex Aircon, Inc. | High efficiency refrigeration system |
ITMI20061472A1 (it) | 2006-07-26 | 2008-01-27 | Antonio Lanti | Dispositivo meccanico statico per la separazione dei fluidi a due o piu'uscite a temperatura differenziata e a basso consumo energetico |
Also Published As
Publication number | Publication date |
---|---|
WO2010100614A3 (fr) | 2010-11-25 |
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