GB2464025A - Refrigerating container for land, road and rail vehicles - Google Patents
Refrigerating container for land, road and rail vehicles Download PDFInfo
- Publication number
- GB2464025A GB2464025A GB1000515A GB201000515A GB2464025A GB 2464025 A GB2464025 A GB 2464025A GB 1000515 A GB1000515 A GB 1000515A GB 201000515 A GB201000515 A GB 201000515A GB 2464025 A GB2464025 A GB 2464025A
- Authority
- GB
- United Kingdom
- Prior art keywords
- container
- cooling air
- chute
- transverse wall
- shaft
- 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
Links
- 238000001816 cooling Methods 0.000 abstract 5
- 239000002826 coolant Substances 0.000 abstract 1
- 239000003507 refrigerant Substances 0.000 description 4
- 239000004411 aluminium Substances 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 230000001174 ascending effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 210000002105 tongue Anatomy 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000005057 refrigeration Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 239000004743 Polypropylene Substances 0.000 description 1
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002991 molded plastic Substances 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- -1 polypropylene Polymers 0.000 description 1
- 229920001155 polypropylene Polymers 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000009897 systematic effect Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D88/00—Large containers
- B65D88/74—Large containers having means for heating, cooling, aerating or other conditioning of contents
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
- F04D25/166—Combinations of two or more pumps ; Producing two or more separate gas flows using fans
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/58—Cooling; Heating; Diminishing heat transfer
- F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
-
- 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
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D11/00—Self-contained movable devices, e.g. domestic refrigerators
- F25D11/003—Transport containers
-
- 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
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D17/00—Arrangements for circulating cooling fluids; Arrangements for circulating gas, e.g. air, within refrigerated spaces
- F25D17/04—Arrangements for circulating cooling fluids; Arrangements for circulating gas, e.g. air, within refrigerated spaces for circulating air, e.g. by convection
- F25D17/06—Arrangements for circulating cooling fluids; Arrangements for circulating gas, e.g. air, within refrigerated spaces for circulating air, e.g. by convection by forced circulation
- F25D17/067—Evaporator fan units
-
- 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
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D23/00—General constructional features
- F25D23/006—General constructional features for mounting refrigerating machinery components
-
- 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
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D2317/00—Details or arrangements for circulating cooling fluids; Details or arrangements for circulating gas, e.g. air, within refrigerated spaces, not provided for in other groups of this subclass
- F25D2317/06—Details or arrangements for circulating cooling fluids; Details or arrangements for circulating gas, e.g. air, within refrigerated spaces, not provided for in other groups of this subclass with forced air circulation
- F25D2317/068—Details or arrangements for circulating cooling fluids; Details or arrangements for circulating gas, e.g. air, within refrigerated spaces, not provided for in other groups of this subclass with forced air circulation characterised by the fans
- F25D2317/0681—Details thereof
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Cold Air Circulating Systems And Constructional Details In Refrigerators (AREA)
- Devices That Are Associated With Refrigeration Equipment (AREA)
- Passenger Equipment (AREA)
Abstract
The invention relates to a refrigerating container for land, road and rail vehicles, the inside of the rear side of said refrigerating container having formed in it a shaft (18) which extends vertically and largely over the width of the container and has a transverse wall (32) above which heated cooling air which is collected beneath the roof region of the container can be supplied to the shaft with downward deflection, wherein at least one passage opening (38) with an inserted ring part (40) is formed in the transverse wall, and the heated cooling air can be conducted to heat exchange areas of an evaporator of a coolant circuit, which heat exchange areas (22) project into the shaft, via a blower (44) through the free cross section of said ring part, and wherein the cooling air which is cooled down in the heat exchange areas can be conducted back into the base region of the refrigerating container out of the lower side of the shaft. According to the invention, provision is made for guide areas (52) for the heated cooling air which is drawn in by the blower to be provided above and to the side of the transverse wall, in order to laterally conduct said heated cooling air into the free cross section (50) of the ring part (40).
Description
Refrigerated container for land, road and rail vehicles The invention relates to a refrigerated container for land, road and rail vehicles.
Such containers are basically shaped rectangular with a longitudinal axis 40 feet (roughly 14 m) long, for example.
They are generally located on the vehicle so that the longitudinal axis of the container is parallel to the longitudinal axis of the vehicle.
The door of the container is arranged at one end whilst the other end mounts a refrigerating unit inserted through a cut-out. As a rule the refrigerating unit is mostly releasably bolted to a flange surrounding the outer edge of the cut-out.
The internal floor of the container is longitudinal ribbed forming longitudinal channels for conducting refrigerated air.
The tops of the longitudinal ribs conventionally forming an upright tee supporting the cargo of the container.
In the region of the end door, means are provided to ensure that the refrigerated air since having become warmed by the cargo ascends, where not having already done so earlier through the cargo, to the roof of the container. A level mark, or some other means of regulating the height of the cargo is provided so that the warmed air between the cargo and the roof of the container can be returned to the end of the container opposite the end door and thus to the refrigerating unit.
The refrigerating unit forms a vertical chute on the inside of the corresponding end of the container, the chute extending the circulation of the refrigerated air, as described above, to form a closed circuit.
Protruding into the chute are the heat exchanger surfaces of an evaporator of a refrigerant circuit. The refrigerant circuit has a conventionally structure typically comprising in addition to the evaporator a compressor, a condenser and an expansion means connecting the evaporator in the cited sequence in the closed circuit.
The chute is usually covered, rendered permeable to air, for example, by means of an aluminium sheet metal sieve doubling as a safety guard against foreign objects falling in and injury due to unwanted human access. Remaining between this cover, the inner wall surfaces of the front wall and of the container is a plenum open to the storage space of the container within which the return flow of warmed refrigerated air is deflected through the cover into the chute. This plenum extends substantially, or practically completely, over the full width of the container.
Below the cover, clearly spaced away therefrom vertically, the chute is divisioned by a transverse wall in which a port is configured conventionally asymmetrically as a round hole relative to the container extending downwards for the warmed refrigerated air. However, in special instances it is just as possible that merely one, or several ports are provided.
Inserted in each port in the transverse wall is an annular part clasping the transverse wall by an outer flange-type structure on which it is located and expediently secured, the annular part porting the transverse wall to serve as an air feeder to an axial blower in each case. The axial blower directs the ascending warmed refrigerated air to the heat exchanger surface of the evaporator. This results in the heat of the ascending warmed refrigerated air being given off to the refrigerant of the refrigerant circuit, and the refrigerated air, now again suitable for refrigeration, is returned into the longitudinal channels in the floor of the container.
Attempts were made earlier to optimize use of the space availab]e in the refrigerating unit and particu]ar]y in its chute by a simple design, especially by selecting the flow porting cross-section of the annular part for the ascending warmed refrigerated air as large as possible. But the maximum diameter thereof is dictated by the spacing between the inner surface of the end of the container opposite the end door and the adjoining wall surface opposite the cargo and the inner dimensions of the chute derived therefrom. This is why hitherto the outer flange-type structure of the annular part was configured on both sides thereof but not in the axial direction of the container so as not to restrict in this axial direction of the container the flow cross-section of the inner opening of the annular part.
The invention is based on the object to further improve the efficiency in refrigerating the cargo of the refrigerated container by a simple design.
This object is achieved by the features of claim 1.
Comparative test have shown that these aspects alone have made it possible to significantly increase efficiency which, depending on the practical application concerned, can be put to use for a variety of objectives including lower consumption of energy needed to power electric axial blowers, smaller power stages for the motors driving the axial blower as well as an improved throughflow of the cargo with refrigerated air.
It was discovered in particularly that refrigeration, also transversely in the container, is now more uniform than previously. The explanation for this surprising effect is that refrigerated air in the side regions of the cargo space of the container is now circuited better than before by being held back less than before by becoming more or less tacked to the side wall. The flow profile in the return stream of the warmed refrigerated air is now less axialized, in other words more uniform.
As it reads from claim 2, introducing the warmed refrigerated air can be rendered uniform in the flow cross-section of the annular part which also reduces the noise developed, these effects being achieved even more so as it reads from claim 3, one special advantage thereof being a better capture of the more radially removed warmed refrigerated air.
As it reads from claim 4 it can now be avoided, or at least diminished, that free edges of the lateral flow directors as obstacles protruding into the inflow of warmed refrigerated air cause turbulence. This effect, as it reads from claim 5 is now further reduced in avoiding dead spaces in the flow whilst simultaneously making it possible to attain a flange-type support of the annular part at the transverse wall of the chute at least punctiform in the outer region of the annular part.
Claim 6 is based on the idea of arranging the flow directors and, where possible, the flange-type supports so that they now no longer take up valuable space as needed for accommodating the cargo.
Claim 7 -where expounding on the idea of claim 6 -becomes especially significant when the diameter of the flow cross-section in the annular part between the inner side of the front wall of the chute facing the cargo space and the front surface of the rear wall of the container is selected as large as possible.
Conventionally, annular parts consist of a cylindrical sleeve, from the top of which a sub-portion of the annular flange projects at right angles on both sides for securing to the transverse wall, the flow cross-section of this sleeve being circular. Such a circular inner cross-section is also preferred in the scope of the invention, particularly in the configuration as set forth in claim 7. But this does not exclude the sleeve part having a cross-section other than circular not only in conjunction with claim 7 but in the scope of the invention. Especially interesting in this case are flattened flow cross-sections preferably with a curved, for example, oval inner contour, the flattening expediently extending transversely in the chute to avoid influencing cargo space availability.
Claim 8 shows how the invention is achievable particularly simply by a modified integral annular part featuring a few constructive means, resulting in a surprisingly significant increase in efficiency for the same application as in the known case.
The known cylindrical annular part is usually made of aluminium or an aluminium alloy. In the scope of the invention even a thin-walled injected moulded plastics material may be provided as it reads from claim 9 since the three-dimensional outer geometry resulting in conjunction with the flow directors also renders a thin-walled insertion sleeve �n the transverse wall adequately dimensionally stable (see claim 10).
The features of claim 11 are known as such, but the siqnificance of c]aim 11 is that a two-stage b]ower powered without gearing can now be employed in the scope of the invention as a particularly straightforward solution.
Basically any known type of blower can be put to use in the scope of the invention, for example, also a radial blower which, however, involves special adapters and thus, in the scope of the invention, preference is given to using an axial blower as is known.
One such axial blower is, however, expediently further adapted in the scope of the invention to further boost the performance efficiency by minor changes in shape.
Axial blowers as used conventionally have straight blades becoming thicker towards the shaft simply for stabilization.
Instead, in accordance with the invention, preference is given as set forth in claim 13 -preferably with the special features as set forth in claims 14 to 18 -to a shaping serving not only to enhance the dimensional stability of the blades but, where necessary, also effecting their thickness.
It is especially the driving power of the corresponding blower and the noise it develops that are further reduced. Also contributing to such positive effects is the fact that the warmed refrigerated air forwarded by the blades of the axial blower is now received by the corresponding blade radially to radially outwards with some time delay.
Claim 19 firstly recites in its own preamble a restriction to the taken-over features of conventional annular parts. In the further development as it reads from claim 19 and the preferred further aspects thereof as set forth in claims 20 and 21 the preferred embodiment of an annular part used in the scope of the invention is detailed. Configuring a flange structure in accordance with the invention for supporting and, where necessary, securing the annular part to the transverse wall of the shaft is achieved in that the flow directors are now arranged in the radial inner space to the side of the sleeve part, where possible, as claimed in claim 21, along the whole axial extent of the inner cross-section of the chute to maximize the flow whilst being directly connected to the front side of the rear wall of the container with a continuation in a corresponding side flange structure radially further outwards back in the direction of the transverse wall, this flange structure being resolved tongued to advantage.
The surprising boost in the efficiency simply by replacing the conventional annular part -as also used by the applicant hitherto -by an annular part in accordance with the invention as detailed by the example configurations will now become clear from a discussion of the following trial comparisons.
These trial comparisons demonstrate, for one thing, quantitatively to what degree especially the power consumption (wattage) of an electric powered axial blower can be altered by the modification of the annular part in accordance with the invention simply by replacing the known annular part by the novel one.
For another thing, there is also an interaction with the geometry especially of the blades of the axial blower for which no systematic trial comparison results are available at this time.
The axial blower was operated in the trial comparisons still with straight blades pitched 19, 22 and 25 degrees (standard) In all cases the motor powering the axial blower was an electric gearless motor switched two and four pole for low and high speed respectively.
Trial results Power consumption: wattage conventional, novel, novel, novel, pitch pitch pitch pitch _____________ 25 (Standard) 19 22 25 hz fast 1657 985 1280 1430 hz slow 375 228 265 285 hz fast 1008 617 800 870 hz slow 283 181 204 213 m3/hour air flow hz fast 5625,06 5420,76 6209,36 6428,64 hz slow 2906,51 2615,58 3132,60 3234,75 hi fast 4791,52 4459,19 5239,61 5435,47 hi slow 2397,12 2141,06 2557,02 2651,81 This already makes it evident that the power consumption of the axial blower can now be reduced by 13 to 40% even without taking into account any adaptation of the blade geometry of the axial blower in the high speed mode (460 V, 60 Hz) The invention will now be detailed by way of an example embodiment with reference to the diagrammatic drawings in which: FIG. 1 is a partial section view of the rear end portion of a container along its longitudinal axis; FIG. la is a partial section view at the same level as in FIG. 1 but at right angles to the transverse direction of the container; FIG. 2a is a top-down view; FIG. 2b is a bottom-up view; FIG. 2c is a side view of an annular part as employed in the assembly as shown in FIGs. 1 and la; and FIG. 3 is an isometric view of the blade ring of an axial blower likewise employed in the assembly as shown in FIGs. 1 and la.
Referring now to FIG. 1 there is illustrated how the end portion of a container includes the floor panel 2, the roof panel 4 and the rear wall 6 thereof. The top of the floor panel 2 is ribbed in the]onqitudina] direction of the container, channels (not shown) being formed between the ribs for directing refrigerated air.
The rear wall 6 comprises practically over its full height and likewise more or less over its full width a cut-out 10 through which a refrigerating unit 12 is inserted into the interior of the container.
The outer wall 14 of the refrigerating unit 12 is a functional extension of the rear wall 6 of the container as can be deemed functionally identical therewith.
Facing the cargo space 16 of the container in this arrangement the refrigerating unit 12 forms a vertical chute down which warmed refrigerated air is directed to the refrigerating unit 12 at the rear side of the container. Axially the lower portion of the chute 18 is tapered to create in line with the outer side of the rear wall 6 of the container a housing space 20 for the main function elements of the refrigerating unit 12. In the upper portion of the chute of sole interest in the scope of the invention the chute 18 is flared up to the inner side of the outer wall 14 of the refrigerating unit 12 which, as mentioned, takes on the function of the rear wall of the container.
The function elements of the refrigerating unit arranged in the housing space 20 are conventional, i.e. compatible with any known assembly, but of interest for the invention is that the heat exchanger surfaces 22 of an evaporator of the refrigerating unit protrude into the flared portion of the chute 18.
At the heat exchanger surfaces 22 within the chute 18 warmed refrigerated air in the chute 18 is recooled to a low operating temperature and streamed into the longitudinal channels between the ribs 8 at the underside of the waisted portion of the chute 18. The arrows indicate the circulation of the refrigerated air in FIG. 1. The refrigerated air streams upwards from the longitudinal channels along the full length of the cargo space 16 enveloping the cargo to collect below the roof panel 4 and is returned upwards into the flared portion of the chute 18 after having picked up the warmth from the cargo space 16 and its cargo. A setting 24 corresponding roughly to the top of the chute 18 (or somewhat lower) ensures that a plenum 26 remains free to receive the warmed refrigerated air below the roof panel 4.
Level with the setting 24 or somewhat thereabove a grating 28 extends over the top of the flared portion of the chute 18 to conventionally prevent foreign objects or clumped substances from entering the chute 18. In addition, the grating 28 is a safety guard against arm and leg access top-down into the chute 18. The cargo space 16 is formed by the front wall 30 of the refrigerating unit 12 configured substantially planar and extending vertical over the height and width of the container in accordance with the dimensioning of the cut-out 10, it thereby running parallel to the outer wall 14 of the chute 18 waisting the inner configuration of the chute 18 between its top and bottom portion.
Clearly indicated is how a transverse wall 32 is located below the grating 28 (by roughly 20 to 30 cm in this example embodiment) parallel thereto. Disposed in this arrangement between the front wall 30 and the outer wall 14, on the one hand, and the grating 28 and transverse wall 32, on the other, is a plenum 34 at the top of the chute 18 to receive the since warmed refrigerated air. As shown in FIG. la this plenum 34 extends between the side walls practically over the full width thereof in the scope dimensioning the width of the cut-out 10.
In this arrangement the side clearance is maintained so small that for all practical purposes it can be ignored.
Provided to the left and right of the longitudinal centerline (imaginary line 36 in FIG. la) are identical assemblies, only one of which will now be discussed in detail, the other to be imagined mirror-symmetrical at the longitudinal centerline or corresponding centre plane of the container.
Accordingly, illustrated in FIG. 1 is just the left-hand portion as shown in FIG. la.
The transverse wall 32 is ported in the centre, in this case the portion cited on the left, by a port 38 having, as shown here, a circular inner cross-section.
Inserted top-down into the port 38 of the transverse wall 32 is an annular part 40 as will now be detailed with reference to the FIGs. 2a to 2c.
This annular part 40 comprises a cylindrical sleeve 42 inserted in the port 38 and feeds by its flow cross-section the warmed refrigerated air to an axial blower 44 comprising an electrically power gearless two and four pole motor 46 to drive the axial blower 44 optionally at a low or high speed, in other words, an axial blower 44 conventionally powered by an electric motor 46.
Referring now to FIG. 3 there is illustrated how the axial blower 44 also features a ring of blades 48, the novel structure of which will now be detailed in the present context.
But firstly the annular part 40 bottomed by the sleeve 42 will be given more consideration as to its structure at the top of sleeve 42 as shown in FIGs. 2a to 2c.
The complete annular part 40 is an integral injection moulded component with a broad choice of known plastics, polyamide or polypropylene expediently reinforced in both cases by glass or carbon fibres being cited just as one example. Selecting this material makes a wall thickness of just 1.5 mm sufficient which as compared to the usual wall thickness of 2mm when made from aluminium or aluminium alloy constitutes a considerable saving in costs.
The sleeve 42 has a round flow cross-section 50 of maximum diameter, maximum in this case meaning that it corresponds to the diameter of the flow cross-section 50 plus twice the wall thickness of the sleeve 42 in the clearance between the inner side of the outer wall 14 and the inner side of the front wall 30 of the refrigerating unit 12 as is rendered clear in the direction of this clearance in FIG. 2a by the dimension of the flow cross-section with diameter D and twice the dimension d as to the thickness of the sleeve wall.
The top of the sleeve 42 then translates only in both side directions, i.e. in the transverse direction of the container or parallel to its ends into a lateral flow director 52 extending over the full width of the chute 18 by a curvature having a continuously further opening. Each lateral flow director 52 is protracted radially sideways by mdi tongues 54 which as is particularly clearly evident from drawing in FIG. 2c are curved back roughly circularly in the direction of the sur of the transverse wall 32 and the crests of which avoid free edges in the air inflow direction. In addition, the tongues 54 are supported by the top of the transverse wall 32 where they also serve as flange-type fasteners. For this purpose the free end 56 of each tongue 54 can be arranged, for example, (not shown) to engage a supporting groove in the top of the transverse wall.
In conclusion FIG. 3 shows how a fan ring 58 of the axial blower 44 is preferably adapted in shape.
The fan ring 58 comprises a hub 60 which can be secured to the output shaft of the drive motor 46 by means of a clip 62.
Distributed equispaced about the circumference of the hub 60 are the blades 48 of the axial blower 44 which as evident from the isometric view in FIG. 3 are curved concave in the conveying direction, they also being twisted inside out in the direction of rotation which is indicated by an arrow in FIG. 3 whilst the conveying direction is to be viewed as pass�ng through the plane of the drawing.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200720008763 DE202007008763U1 (en) | 2007-06-22 | 2007-06-22 | Refrigerated container for land, road and rail vehicles |
DE102007028787A DE102007028787B4 (en) | 2007-06-22 | 2007-06-22 | Refrigerated container for land, road and rail vehicles |
PCT/EP2008/004953 WO2009000461A2 (en) | 2007-06-22 | 2008-06-19 | Refrigerating container for land, road and rail vehicles |
Publications (3)
Publication Number | Publication Date |
---|---|
GB201000515D0 GB201000515D0 (en) | 2010-03-03 |
GB2464025A true GB2464025A (en) | 2010-04-07 |
GB2464025B GB2464025B (en) | 2013-01-02 |
Family
ID=40186077
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1000515.5A Active GB2464025B (en) | 2007-06-22 | 2008-06-19 | Refrigerated container for land, road and rail vehicles |
Country Status (5)
Country | Link |
---|---|
US (1) | US20100251753A1 (en) |
JP (1) | JP5480806B2 (en) |
DK (1) | DK200970298A (en) |
GB (1) | GB2464025B (en) |
WO (1) | WO2009000461A2 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010530950A (en) * | 2007-06-22 | 2010-09-16 | サーモ キング コンテナ−デンマーク エー/エス | Refrigerated containers for ships |
PT2180277E (en) | 2008-10-24 | 2015-11-23 | Johnson Controls Tech Co | Controlling chilled state of a cargo |
JP2013011420A (en) * | 2011-06-30 | 2013-01-17 | Daikin Industries Ltd | Refrigerating apparatus for container |
JP5751179B2 (en) * | 2012-01-20 | 2015-07-22 | 株式会社デンソー | Container refrigeration equipment |
JP6675196B2 (en) * | 2015-12-28 | 2020-04-01 | 株式会社神戸製鋼所 | Package type compressor |
EP3452313B1 (en) | 2016-05-04 | 2020-08-26 | Carrier Corporation | Refrigeration unit having movable directional element |
WO2018114621A1 (en) * | 2016-12-22 | 2018-06-28 | Maersk Container Industry A/S | Integrated fan grille for a cooling machine in a reefer container |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
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- 2008-06-19 JP JP2010512601A patent/JP5480806B2/en not_active Expired - Fee Related
- 2008-06-19 US US12/665,759 patent/US20100251753A1/en not_active Abandoned
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Also Published As
Publication number | Publication date |
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WO2009000461A4 (en) | 2009-07-16 |
JP5480806B2 (en) | 2014-04-23 |
GB201000515D0 (en) | 2010-03-03 |
GB2464025B (en) | 2013-01-02 |
WO2009000461A3 (en) | 2009-05-14 |
DK200970298A (en) | 2009-12-23 |
WO2009000461A2 (en) | 2008-12-31 |
US20100251753A1 (en) | 2010-10-07 |
JP2010530949A (en) | 2010-09-16 |
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