GB2128310A - Heat pump - Google Patents

Heat pump Download PDF

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Publication number
GB2128310A
GB2128310A GB08326270A GB8326270A GB2128310A GB 2128310 A GB2128310 A GB 2128310A GB 08326270 A GB08326270 A GB 08326270A GB 8326270 A GB8326270 A GB 8326270A GB 2128310 A GB2128310 A GB 2128310A
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GB
United Kingdom
Prior art keywords
container
inner container
containers
side wall
flowpath
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB08326270A
Other versions
GB2128310B (en
GB8326270D0 (en
Inventor
John Hughes
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Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB08326270A priority Critical patent/GB2128310B/en
Publication of GB8326270D0 publication Critical patent/GB8326270D0/en
Publication of GB2128310A publication Critical patent/GB2128310A/en
Application granted granted Critical
Publication of GB2128310B publication Critical patent/GB2128310B/en
Expired legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C39/00Relieving load on bearings
    • F16C39/06Relieving load on bearings using magnetic means
    • F16C39/063Permanent magnets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B29/00Combined heating and refrigeration systems, e.g. operating alternately or simultaneously

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Abstract

A heat pump device for producing a temperature difference between two regions includes an evacuated outer annular container (2), and an inner annular container (6) spaced from and mounted coaxially within the outer container (2) for rotation about a common axis (4). The inner container (6) is supported in the outer container (2) by a magnetic bearing (8), and the inner container (6) holds a suitable gas. Permanent magnets (12) are spaced around the rotation path on the inner container (6), and four associated electromagnets (10) are similarly positioned on the outer container (2). In operation, the electromagnets (10) are sequentially actuated to revolve the inner container (6) at high speed thereby causing the temperature at the inner side wall (20) of the inner container (6) to fall and the temperature of the outer side wall of the inner container (6) to rise. This temperature change can be used to cool a fluid passing through the central flowpath (16) and to heat a fluid passing along an outer flowpath defined in part by the outer wall (18) of the outer container. <IMAGE>

Description

SPECIFICATION A device for producing a temperature difference Technical Field The present invention relates to a device for producing a temperature difference between two regions.
In one application of the invention two separate fluid streams can be passed each through its respective region, and these fluid streams can be used for any suitable purpose, such as for example heating, cooling and power generation.
Statement of Invention According to the present invention there is provided a device for producing a temperature difference between two regions, said device comprising an evacuated outer endless tubular container, a gas containing inner endless tubular container spaced from and mounted coaxially within said outer container, said containers being relatively rotatable about their common axis, and each container being of circular section in a plane perpendicular to said common axis, a central flow path, defined by the inner side wall of the outer container, passing through the device about the common axis, an outer flow path defined partly by the outer side wall of the outer container, and drive means for producing relative rotation of the two containers.
The inner and outer tubular containers may each have any suitable transverse cross-section, such as for example a square or rectangular crosssection.
Preferably the external side surface of the inner container and the internal side surface of the outer container are given a dark matt colour, and both internal side surfaces of the inner container are silvered to reduce internal radiation.
In a preferred arrangement, the inner container is mounted in the outer container by a circular magnetic bearing. The drive means may comprise a plurality of permanent magnets spaced round the rotation path on one of the containers, and associated sequentially actuated electromagnets similarly positioned on the other container.
Figures in the Drawings One embodiment of the invention will now be described by way of example with reference to the accompanying illustrative drawings in which: FIGURE 1 is a cross-sectional side elevation of one device of the invention, FIGURE 2 is a plan view from above of the device of Figure 1, FIGURE 3 is a plan view from above of the inner container of the device of Figure 1, and FIGURE 4 is a plan view from above of the bottom of the outer container.
Description of the Drawings Referring to the drawings, one device of the invention includes an endless outer container (2) of square cross-section. This container is of circular section in a plane perpendicular to a central axis (4). An inner container (6), of the same cross-section and shape as the outer container (2), is rotatably mounted in the outer container (2) by means of a circular magnetic bearing (8). Four electro-magnets (10) are mounted on the upper wall of the outer container (2). These electromagnets (10) are equally spaced on the circumference of the circle having the axis (4) as its centre. Four permanent magnets (12) are mounted on the upper side of the inner container (6).These permanent magnets (12) are spaced and positioned similarly to the electro-magnets (10), so that the four permanent magnets (12) can be located immediately beneath the respective electro-magnets (10).
The inner side wall (14) of the outer container (2) defines a central flow path (16) passing through the device. An outer flow path (not shown) is formed partly by the outer side wall (1 8) of the outer container (2). In order to reduce heat or cold losses, the upper and lower walls of both the inner and outer containers are made of a nonmetallic material. The inner and outer side walls of the inner and outer containers may be made of either a metallic or a non-metallic material. The magnetic bearing (8) may be either sloped or rounded in order to provide lateral stability for the inner container (6). The inner container (6) contains a gas, and the outer container (2) is evacuated.
In operation, the inner container (6) is rotated at high speed within the outer container (2) by sequentially actuating the electro-magnets (10) which thereby react with the permanent magnets (12) on the inner container (6). When the inner container (6) is rotating at a high speed the temperature of the gas inside the inner container decreases in the region of the inner container inner side wall (20), and increases in the region of the inner container outer side wall (22). This temperature difference is then transmitted to the inner side wall (14) and the outer side wall (18) of the outer container (2). Two streams of gas or liquid can then be passed along the central flowpath (1 6) and the outer flowpath, and these cooled and heated fluid streams can then be used for any appropriate purpose such as for example air conditioning, refrigeration, space heating or power generation.
Any gas or vapour can be used inside the inner container (6). Air is perfectly suitable, but it is a question of the higher the specific heat the better.
The pressure of the gas or vapour in the inner container (6) should be as high as possible limited only by the strength of the inner container (6).
It will be necessary for the inner container outer side wall (22) to travel at 1000-1 200 feet per second in order to obtain temperature differences of 500C between the central flowpath (16) and the outerflowpath.
If a plentiful supply of air at 200C is passed down the central flowpath (1 6) then a small amount of air at 200C passed along the outer flowpath will reach a temperature of approximately 6O0C. If this air is split into two and passed through another similar device then the resultant temperatures of the inner and outer air streams will be 400C and 800C respectively. This process can be repeated to obtain any required temperature within reasonable limits.
If a large quantity of air or water is passed down the central flowpath (16) at 200C and a small quantity of air or water is passed along the outer flowpath at 2O0C, then this air or water in the outer flowpath will be heated to 600C.
Conversely if a large quantity of air or water is passed along the outer flowpath then the temperature of a small quantity of air or water passing through the central flowpath (16) will be reduced from 200C to -200C. If a low volume is passed along both flowpaths then temperatures of OOC and 400C will result in the central and outer flowpaths respectively.
By making the upper and lower walls of both the inner and outer containers of a non-metallic material it is possible to reduce the electrical eddy current losses.
The magnetic bearing (8) may have any suitable shape in order to provide lateral stability for the inner container (6).
The external sidewalls of the inner container (6) and the internal sidewalls of the outer container (2) are painted matt black in order to assist heat transfer into the central flowpath (16) and the outer flowpath.
The magnetic bearing (8) may be sloped or rounded in order to provide lateral stability.
In order to reduce any lateral oscillations or vibrations of the inner container (6), the device includes outwardly extending brushes (24) which are mounted on the inner surface of the inner side wall (14) of the outer container (2). These brushes (24) are dimensioned to touch the inner container (6) only if the container (6) moves out of its central position. These brushes (24) thereby assist in retaining the inner container (6) in its central position. The brushes may be made of any suitable material such as for example a suitable plastics material.

Claims (8)

1. A device for producing a temperature difference between two regions, said device comprising an evacuated outer endless tubular container, a gas containing inner endless tubular container spaced from and mounted coaxially within said outer container, said containers being relatively rotatable about their common axis, and each container being of circular section in a plane perpendicular to the common axis, a central flowpath, defined by the inner side wall of the outer container, passing through the device about said common axis, an outer flowpath, defined partly by the outer side wall of the outer container, and drive means for producing relative reotation of the two containers.
2. A device as claimed in Claim 1, in which the inner container is mounted in the outer container by a circular magnetic bearing.
3. A device as claimed in Claim 2, in which the magnetic bearing is shaped to provide lateral stability.
4. A device as claimed in any preceding Claim in which the drive means comprises a plurality of permanent magnets spaced round the rotational path of one of said containers, and associated sequentially actuated electromagnets similarly positioned on the other container.
5. A device as claimed in any preceding Claim in which the upper and lower walls of the inner and outer containers are made of a non-metallic material.
6. A device as claimed in any preceding Claim in which the external side surface of the inner container and the internal side surface of the outer container are of a dark matt colour.
7. A device as claimed in any preceding Claim in which both internal side surfaces of the inner container are silvered to reduce internal radiation.
8. A device for producing a temperature difference between two regions substantially as herein described and shown in the accompanying drawings.
GB08326270A 1982-10-04 1983-09-30 Heat pump Expired GB2128310B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08326270A GB2128310B (en) 1982-10-04 1983-09-30 Heat pump

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8228319 1982-10-04
GB08326270A GB2128310B (en) 1982-10-04 1983-09-30 Heat pump

Publications (3)

Publication Number Publication Date
GB8326270D0 GB8326270D0 (en) 1983-11-02
GB2128310A true GB2128310A (en) 1984-04-26
GB2128310B GB2128310B (en) 1986-08-06

Family

ID=26284026

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08326270A Expired GB2128310B (en) 1982-10-04 1983-09-30 Heat pump

Country Status (1)

Country Link
GB (1) GB2128310B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2619201A1 (en) * 1987-08-05 1989-02-10 Boone Jacques Rotary heat pump
FR2640361A1 (en) * 1988-12-14 1990-06-15 Chaouat Louis Heat pump which uses variations in temperatures undergone by a gas which runs through the gravitational field or that of the centrifugal force
WO1996024015A1 (en) * 1995-01-31 1996-08-08 Eremin, Andrei Leonidovich Method of transferring heat from a lower temperature level to a higher temperature level and a device for carrying out said method

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1573783A (en) * 1977-02-23 1980-08-28 Kantor F W Rotary thermodynamic system and method
GB1575684A (en) * 1976-06-28 1980-09-24 Ultra Centrifuge Nederland Nv Installation proveded with a hollow rotor

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1575684A (en) * 1976-06-28 1980-09-24 Ultra Centrifuge Nederland Nv Installation proveded with a hollow rotor
GB1573783A (en) * 1977-02-23 1980-08-28 Kantor F W Rotary thermodynamic system and method

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2619201A1 (en) * 1987-08-05 1989-02-10 Boone Jacques Rotary heat pump
FR2640361A1 (en) * 1988-12-14 1990-06-15 Chaouat Louis Heat pump which uses variations in temperatures undergone by a gas which runs through the gravitational field or that of the centrifugal force
WO1996024015A1 (en) * 1995-01-31 1996-08-08 Eremin, Andrei Leonidovich Method of transferring heat from a lower temperature level to a higher temperature level and a device for carrying out said method

Also Published As

Publication number Publication date
GB2128310B (en) 1986-08-06
GB8326270D0 (en) 1983-11-02

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PCNP Patent ceased through non-payment of renewal fee