EP1948930B1 - Compressor arrangement having bypass means for avoiding freezing of the cooler unit - Google Patents
Compressor arrangement having bypass means for avoiding freezing of the cooler unit Download PDFInfo
- Publication number
- EP1948930B1 EP1948930B1 EP06818455.5A EP06818455A EP1948930B1 EP 1948930 B1 EP1948930 B1 EP 1948930B1 EP 06818455 A EP06818455 A EP 06818455A EP 1948930 B1 EP1948930 B1 EP 1948930B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- bypass pipe
- unit
- compressor
- cooler unit
- cooler
- 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.)
- Not-in-force
Links
- 238000007710 freezing Methods 0.000 title claims description 10
- 230000008014 freezing Effects 0.000 title claims description 10
- 238000001816 cooling Methods 0.000 claims description 42
- 238000011144 upstream manufacturing Methods 0.000 claims description 4
- 238000010276 construction Methods 0.000 claims description 3
- 238000002194 freeze distillation Methods 0.000 claims description 3
- 238000005266 casting Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 230000009172 bursting Effects 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/06—Cooling; Heating; Prevention of freezing
- F04B39/068—Cooling; Heating; Prevention of freezing prevention of freezing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B25/00—Multi-stage pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/06—Cooling; Heating; Prevention of freezing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/06—Cooling; Heating; Prevention of freezing
- F04B39/066—Cooling by ventilation
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- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/6416—With heating or cooling of the system
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- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/87265—Dividing into parallel flow paths with recombining
- Y10T137/87338—Flow passage with bypass
- Y10T137/87362—Including cleaning, treating, or heat transfer feature
Definitions
- the present invention relates to a compressor arrangement for generating compressed air by means of a motor-driven compressor unit, which is followed by at least one cooler unit for cooling the generated compressed air, which enters the cooler unit via at least one inlet, where it flows through adeluftumströmte cooling structure of a plurality of parallel-connected cooling channels and the cooler unit via at least one outlet, wherein between the inlet and the outlet of the radiator unit bypass means for avoidance a freezing of the cooler unit are provided at low ambient temperatures.
- the field of application of the present invention extends primarily to oil-free piston compressors, which are used for the production of compressed air, for example in commercial and rail vehicle construction.
- the compressor assembly must operate over a temperature range of -50 ° C to + 50 ° C ambient temperature. Since the cooler design also provides a maximum cooling capacity at + 50 ° C, under specific environmental conditions - for example, 100% humidity, - 20 ° C ambient temperature and 50% duty cycle - icing of the cooling channels can be observed within the cooler unit of the compressor assembly. During the operation of the compressor unit, this icing may even progress over a period of several hours to the extent that sufficient air delivery is no longer possible and the compressor arrangement finally fails.
- valve and control technology causes a corresponding equipment expense.
- interruption of the power supply for the control electronics or wear a seal in the valve could freeze the cooling unit unhindered until its destruction.
- this solution is primarily for protecting the units downstream of the cooler unit from icing.
- the invention includes the technical teaching that is provided as a bypass means only a permanently open bypass pipe without any lying in the compressed air flow valves between the region of the inlet and the region of the outlet of the cooler unit.
- the internal cross section of the bypass tube is matched to the capacity of the compressor unit and to the pressure difference between the inlet and outlet so that the bypass tube causes a higher flow resistance than the cooling structure at normal ambient temperatures. Normal ambient temperatures are primarily temperatures above freezing. At temperatures below freezing and progressive freezing of the cooling structure, however, the compressed air increasingly flows over the bypass tube.
- the advantage of the solution according to the invention lies in particular in the fact that compressed air generation can be maintained in the case of a freezing of the cooler unit with minimal loss of cooling and conveying power via this specially dimensioned bypass tube. Since the invention does not require any valves, this is feasible with very little technical effort.
- the solution according to the invention has an independent control activity based on the dimensioning of the bypass tube.
- the bypass pipe is designed such that the outlet temperature (measured after the radiator unit) is limited so that the function of downstream equipment - such as air dryer, control valves - is not affected.
- the bypass pipe according to the invention is to be dimensioned to achieve optimum function such that in the case of a frozen cooler unit, which no longer lets compressed air through, the pressure difference between the two ends of the bypass pipe increases to a maximum of 0.5 bar.
- a pressure drop is quite acceptable as a minimal loss of capacity.
- the bypass tube has screw connections at both ends, with which a releasable fastening the bypass tube can be made on the radiator unit.
- the bypass tube is totally integrated in the cooler unit, for example by soldering or welding.
- the bypass tube itself is a tube made of steel or a light metal, which can be used on a normalized semi-finished, for example, a tube with the basic dimensions of 10 x 1.5 mm.
- bypass pipe is provided with cooling fins or cooling fins or is designed in the manner of a finned tube in order to improve the cooling effect, if necessary.
- the bypass tube can be designed as a casting-produced hollow body, or contain such.
- steel and non-metallic materials for production are conceivable, provided that they are sufficiently temperature resistant and pressure resistant.
- the bypass pipe is designed as a hose line, or includes such.
- the bypass tube is arranged relative to the cooler unit in such a way that it lies in the flow of the cooling air flowing through the cooler unit. This ensures that the bypass tube exerts a minimum cooling effect on the compressed air flowing through it.
- the bypass tube can be arranged either vertically or horizontally relative to the radiator unit and run straight. If the self-cooling effect of the bypass pipe is not sufficient for a straight course, the bypass pipe can alternatively be designed in the manner of a pipe coil or the like.
- a drain valve or a safety valve in the wall of the bypass pipe, if that makes sense.
- a drain valve would be located at the lowest point of the bypass tube.
- the solution according to the invention is suitable for use in both single-stage and multi-stage compressor units.
- the cooler unit is provided as an aftercooler, which can then be equipped with at least one bypass pipe according to the invention.
- each individual compressor stage is provided with a downstream cooler unit in the form of an intermediate or aftercooler, wherein each cooling unit is associated with at least one bypass tube.
- the at least one associated bypass pipe is preferably designed such that even with a totally frozen cooler unit, the entire capacity of the upstream compressor unit via the at least one associated bypass pipe is conductive.
- a compressor assembly consists of a driven by an electric motor 1 multi-stage compressor unit 2 for generating compressed air. For this purpose, 3 air is sucked from the environment via a filter unit.
- Each compressor stage of the compressor unit 2 is assigned its own cooler unit 4a and 4b, which serve for cooling the compressed air generated in the respective upstream compressor stage.
- the first compressor stage downstream cooler unit 4a as intercooler and a second compressor stage of the compressor unit 2 downstream cooler unit 4b is to be referred to as aftercooler.
- Each radiator unit 4a and 4b has an inlet 5 for incoming heated compressed air.
- the heated compressed air passes for cooling via a cooling air-circulated cooling structure 6, which - in a conventional manner - from a plurality of parallel-connected cooling channels of smaller diameter flows to leave the cooler unit 4a or 4b via an outlet 7 again.
- the cooling air for flowing around the cooling structure 6 is generated via a motor or shaft-driven fan wheel 8 arranged between the cooler units 4 a and 4 b and the compressor unit 2.
- the cooler unit 4a shown here by way of example between the inlet 5 and the outlet 7 has a bypass tube 9 for avoiding freezing of the cooler unit 4a at low ambient temperatures.
- the continuous, permanently open bypass pipe 9 is characterized by an internal cross-section, which is matched to the capacity of the compressor unit 2 and the pressure difference between inlet 5 and outlet 7 such that the bypass pipe 9 causes a higher flow resistance than the cooling structure 6 at normal ambient temperatures, whereas with progressive freezing of the cooling structure 6 as a result of crystal attachment to the wall and inner disks, the compressed air increasingly flows via the bypass pipe 9. It has been shown that the bypass pipe 9 does not freeze itself under these conditions, since it is heated up quickly by the compressed air itself and its flow friction in the bypass pipe 9.
- the bypass pipe 9 is designed here as a horizontal straight pipeline, which lies in the flow of cooling air flowing through the cooler unit 4 a, in order to also cool the bypass pipe 9.
- a safety valve 10 is inserted, which opens from a defined pressure value to prevent bursting of the bypass tube 9.
- the bypass tube 9 in the interior can also have surface and cross-sectional changes to achieve a nozzle function, if flow dynamic sense.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Compressor (AREA)
Description
Die vorliegende Erfindung betrifft eine Kompressoranordnung zur Erzeugung von Druckluft mittels einer motorbetriebenen Verdichtereinheit, der mindestens eine Kühlereinheit zur Abkühlung der erzeugten Druckluft nachgeschaltet ist, die über mindestens einen Einlass in die Kühlereinheit eintritt, dort durch eine kühlluftumströmte Kühlstruktur aus mehreren parallelgeschalteten Kühlkanälen strömt und die Kühlereinheit über mindestens einen Auslass verlässt, wobei zwischen dem Einlass und dem Auslass der Kühlereinheit Bypassmittel zur Vermeidung eines Einfrierens der Kühlereinheit bei geringen Umgebungstemperaturen vorgesehen sind.The present invention relates to a compressor arrangement for generating compressed air by means of a motor-driven compressor unit, which is followed by at least one cooler unit for cooling the generated compressed air, which enters the cooler unit via at least one inlet, where it flows through a Kühlluftumströmte cooling structure of a plurality of parallel-connected cooling channels and the cooler unit via at least one outlet, wherein between the inlet and the outlet of the radiator unit bypass means for avoidance a freezing of the cooler unit are provided at low ambient temperatures.
Das Anwendungsgebiet der vorliegenden Erfindung erstreckt sich vornehmlich auf ölfreie Kolbenkompressoren, welche zur Erzeugung von Druckluft beispielsweise im Nutz- und Schienenfahrzeugbau zum Einsatz kommen. Bei derartigen Anwendungen hat die Kompressoranordnung über einen Temperaturbereich von - 50° C bis + 50° C Umgebungstemperatur zu funktionieren. Da die Kühlerauslegung auch eine maximale Kühlleistung bei +50°C vorsieht, kann bei speziellen Umgebungsbedingungen - beispielsweise 100 % Luftfeuchtigkeit, - 20° C Umgebungstemperatur und 50 % Einschaltdauer - eine Vereisung der Kühlkanäle innerhalb der Kühlereinheit der Kompressoranordnung beobachtet werden. Diese Vereisung kann beim Betrieb der Verdichtereinheit über einen Zeitraum von mehreren Stunden sogar soweit fortschreiten, dass keine ausreichende Luftförderung mehr möglich ist und die Kompressoranordnung schließlich ausfällt.The field of application of the present invention extends primarily to oil-free piston compressors, which are used for the production of compressed air, for example in commercial and rail vehicle construction. In such applications, the compressor assembly must operate over a temperature range of -50 ° C to + 50 ° C ambient temperature. Since the cooler design also provides a maximum cooling capacity at + 50 ° C, under specific environmental conditions - for example, 100% humidity, - 20 ° C ambient temperature and 50% duty cycle - icing of the cooling channels can be observed within the cooler unit of the compressor assembly. During the operation of the compressor unit, this icing may even progress over a period of several hours to the extent that sufficient air delivery is no longer possible and the compressor arrangement finally fails.
Aus der
Nachteilig bei dieser bekannten technischen Lösung ist jedoch, dass die hier vorgesehene Ventil- und Steuerungstechnik einen entsprechenden gerätetechnischen Aufwand verursacht. Bei einem Versagen oder einer Fehlfunktion von Ventil- bzw. Steuerelektronik durch beispielsweise Unterbrechung der Stromversorgung für die Steuerelektronik oder Verschleiß einer Dichtung im Ventil könnte ein Einfrieren der Kühleinheit ungehindert bis zu deren Zerstörung fortschreiten. Weiterhin eignet sich diese Lösung in erster Linie dafür, die der Kühlereinheit nachgeschalteten Aggregate vor Vereisung zu schützen.A disadvantage of this known technical solution, however, is that the valve and control technology provided here causes a corresponding equipment expense. In case of failure or malfunction of valve or control electronics by, for example, interruption of the power supply for the control electronics or wear a seal in the valve could freeze the cooling unit unhindered until its destruction. Furthermore, this solution is primarily for protecting the units downstream of the cooler unit from icing.
Aus der
Es ist daher die Aufgabe der vorliegenden Erfindung, eine Kompressoranordnung zu schaffen, deren mindestens eine Kühlereinheit durch einfach aufgebaute Bypassmittel wirksam gegen Einfrieren geschützt wird.It is therefore the object of the present invention to provide a compressor assembly whose at least one cooler unit is effectively protected against freezing by simply constructed bypass means.
Die Aufgabe wird ausgehend von einer Kompressoranordnung gemäß dem Oberbegriff von Anspruch 1 in Verbindung mit dessen kennzeichnenden Merkmalen gelöst. Die nachfolgenden abhängigen Ansprüche geben vorteilhafte Weiterbildungen der Erfindung wieder.The object is achieved on the basis of a compressor arrangement according to the preamble of claim 1 in conjunction with its characterizing features. The following dependent claims give advantageous developments of the invention.
Die Erfindung schließt die technische Lehre ein, dass als Bypassmittel lediglich ein permanent offenes Bypassrohr ohne jegliche in der Druckluftströmung liegende Ventile zwischen dem Bereich des Einlasses und dem Bereich des Auslasses der Kühlereinheit vorgesehen ist. Der Innenquerschnitt des Bypassrohres ist dabei derart auf die Förderleistung der Verdichtereinheit sowie auf die Druckdifferenz zwischen Einlass- und Auslass abgestimmt, dass das Bypassrohr bei normalen Umgebungstemperaturen einen höheren Strömungswiderstand als die Kühlstruktur verursacht. Als normale Umgebungstemperaturen gelten vornehmlich Temperaturen oberhalb des Gefrierpunkts. Bei Temperaturen unterhalb des Gefrierpunkts und fortschreitendem Einfrieren der Kühlstruktur strömt die Druckluft allerdings zunehmend über das Bypassrohr.The invention includes the technical teaching that is provided as a bypass means only a permanently open bypass pipe without any lying in the compressed air flow valves between the region of the inlet and the region of the outlet of the cooler unit. The internal cross section of the bypass tube is matched to the capacity of the compressor unit and to the pressure difference between the inlet and outlet so that the bypass tube causes a higher flow resistance than the cooling structure at normal ambient temperatures. Normal ambient temperatures are primarily temperatures above freezing. At temperatures below freezing and progressive freezing of the cooling structure, however, the compressed air increasingly flows over the bypass tube.
Der Vorteil der erfindungsgemäßen Lösung liegt insbesondere darin, dass über dieses speziell dimensionierte Bypassrohr die Drucklufterzeugung im Falle eines Einfrierens der Kühlereinheit unter minimalem Verlust von Kühl- und Förderleistung aufrechterhalten werden kann. Da die Erfindung völlig ohne Ventile auskommt, ist diese mit denkbar geringem technischen Aufwand umsetzbar. Die erfindungsgemäße Lösung besitzt eine auf die Dimensionierung des Bypassrohres basierende, selbständige Regeltätigkeit. Dabei ist das Bypassrohr derart auszulegen, dass die Austrittstemperatur (nach der Kühlereinheit gemessen) so begrenzt ist, dass die Funktion nachgeschalteter Geräte - wie Lufttrockner, Regelventile - nicht beeinträchtigt wird.The advantage of the solution according to the invention lies in particular in the fact that compressed air generation can be maintained in the case of a freezing of the cooler unit with minimal loss of cooling and conveying power via this specially dimensioned bypass tube. Since the invention does not require any valves, this is feasible with very little technical effort. The solution according to the invention has an independent control activity based on the dimensioning of the bypass tube. In this case, the bypass pipe is designed such that the outlet temperature (measured after the radiator unit) is limited so that the function of downstream equipment - such as air dryer, control valves - is not affected.
Versuche haben ergeben, dass insbesondere bei ölfreien Kolbenkompressoren für den Schienenfahrzeugbereich das optimale Verhältnis von Innenquerschnitt des Bypassrohres zu Förderleitung bei 10 bar Betriebsdruck im Bereich zwischen 0,8 bis 1,2 liegt. Diese Kenngröße trifft bei mehreren Kühlereinheiten einer Kompressorenanordnung allein für den Nachkühler zu. Die Maßeinheit für den Innenquerschnitt des Bypassrohres ist mm2. Die Maßeinheit für die Förderleistung ist l/min.Experiments have shown that, especially in oil-free piston compressors for rail vehicles, the optimum ratio of internal cross section of the bypass tube to delivery line at 10 bar operating pressure in the range between 0.8 to 1.2. This parameter applies to several cooler units of a compressor assembly only for the aftercooler. The unit of measure for the internal cross section of the bypass tube is mm 2 . The unit of measure for the delivery rate is l / min.
Vorzugsweise ist das erfindungsgemäße Bypassrohr zur Erzielung einer optimalen Funktion derart zu dimensionieren, dass im Falle einer eingefrorenen Kühlereinheit, welche keine Druckluft mehr durchlässt, die Druckdifferenz zwischen den beiden Enden des Bypassrohres auf maximal 0,5 bar ansteigt. Ein derartiger Druckabfall ist als minimaler Verlust der Förderleistung durchaus hinnehmbar. Durch die erfindungsgemäße Lösung kann erzielt werden, dass bei total eingefrorener Kühlereinheit die Förderleistung um nicht mehr als 5% absinkt und die Austrittstemperatur nach der Kühlereinheit um nicht mehr als 20 °C gegenüber dem Kühler ohne Bypass ansteigt.Preferably, the bypass pipe according to the invention is to be dimensioned to achieve optimum function such that in the case of a frozen cooler unit, which no longer lets compressed air through, the pressure difference between the two ends of the bypass pipe increases to a maximum of 0.5 bar. Such a pressure drop is quite acceptable as a minimal loss of capacity. By the solution according to the invention can be achieved that at totally frozen cooler unit, the flow rate drops by not more than 5% and the outlet temperature rises after the cooler unit by not more than 20 ° C relative to the cooler without a bypass.
Gemäß einer weiteren, die Erfindung verbessernden Maßnahme ist vorgesehen, dass das Bypassrohr zu beiden Enden hin Verschraubungen aufweist, mit welchen eine lösbare Befestigung des Bypassrohres an der Kühlereinheit erfolgen kann. Durch diese Maßnahme ist es möglich, auch Kühlereinheiten ohne Bypassrohr als weitere Produktvariante zu fertigen. Es ist auch denkbar, dass das Bypassrohr in die die Kühlereinheit total integriert ist, beispielsweise durch Einlöten oder Einschweißen. Für das Bypassrohr selbst eignet sich ein Rohr aus Stahl oder einem Leichtmetall, wozu auf ein normiertes Halbzeug zurückgegriffen werden kann, beispielsweise auf ein Rohr mit den Grundmaßen 10 x 1,5mm. Bei der Auswahl und Dimensionierung des Bypassrohrs ist darüber hinaus darauf zu achten, dass dieses dem erforderlichen Prüfdruck standhält.According to a further measure improving the invention, it is provided that the bypass tube has screw connections at both ends, with which a releasable fastening the bypass tube can be made on the radiator unit. By this measure, it is possible to produce cooler units without bypass tube as a further product variant. It is also conceivable that the bypass tube is totally integrated in the cooler unit, for example by soldering or welding. For the bypass tube itself is a tube made of steel or a light metal, which can be used on a normalized semi-finished, for example, a tube with the basic dimensions of 10 x 1.5 mm. When selecting and dimensioning the bypass pipe, care must also be taken to ensure that it withstands the required test pressure.
Weiterhin ist es möglich, dass das Bypassrohr mit Kühllamellen oder Kühlrippen versehen ist oder nach Art eines Rippenrohrs ausgeführt ist, um die Kühlwirkung erforderlichenfalls zu verbessern. Das Bypassrohr kann als ein gießtechnisch hergestellter Hohlkörper ausgeführt werden, oder einen solchen enthalten. Neben Stahl sind auch nichtmetallische Materialien zur Herstellung denkbar, sofern diese die genügend temperaturbeständig und druckfest sind. So ist es auch denkbar, dass das Bypassrohr als eine Schlauchleitung ausgeführt ist, oder eine solche beinhaltet.Furthermore, it is possible that the bypass pipe is provided with cooling fins or cooling fins or is designed in the manner of a finned tube in order to improve the cooling effect, if necessary. The bypass tube can be designed as a casting-produced hollow body, or contain such. In addition to steel and non-metallic materials for production are conceivable, provided that they are sufficiently temperature resistant and pressure resistant. Thus, it is also conceivable that the bypass pipe is designed as a hose line, or includes such.
Gemäß einer anderen, die Erfindung verbessernden Maßnahme ist vorgesehen, dass das Bypassrohr derart relativ zur Kühlereinheit angeordnet ist, dass dieses im Strom der die Kühlereinheit durchströmenden Kühlluft liegt. Hierdurch wird sichergestellt, dass das Bypassrohr auf die hindurchströmende Druckluft eine Mindestkühlwirkung ausübt. Das Bypassrohr kann entweder vertikal oder horizontal relativ zur Kühlereinheit angeordnet sein und gerade verlaufen. Falls die Eigenkühlwirkung des Bypassrohres bei geradem Verlauf nicht ausreichend ist, kann das Bypassrohr alternativ auch nach Art einer Rohrschlange oder dergleichen ausgeführt werden.According to another measure improving the invention, it is provided that the bypass tube is arranged relative to the cooler unit in such a way that it lies in the flow of the cooling air flowing through the cooler unit. This ensures that the bypass tube exerts a minimum cooling effect on the compressed air flowing through it. The bypass tube can be arranged either vertically or horizontally relative to the radiator unit and run straight. If the self-cooling effect of the bypass pipe is not sufficient for a straight course, the bypass pipe can alternatively be designed in the manner of a pipe coil or the like.
Weiterhin ist es denkbar, in die Wandung des Bypassrohres ein Entwässerungsventil oder ein Sicherheitsventil hinzufügen, falls dies sinnvoll ist. Ein Entwässerungsventil wäre an der tiefsten Stelle des Bypassrohres anzuordnen.Furthermore, it is conceivable to add a drain valve or a safety valve in the wall of the bypass pipe, if that makes sense. A drain valve would be located at the lowest point of the bypass tube.
Die erfindungsgemäße Lösung eignet sich zu einem Einsatz sowohl bei einstufigen als auch bei mehrstufigen Verdichtereinheiten. Im Falle einer einstufigen Verdichtereinheit ist die Kühlereinheit als Nachkühler vorgesehen, welche dann mit mindestens einem erfindungsgemäßen Bypassrohr ausgestattet werden kann. Im Falle einer mehrstufigen Verdichtereinheit ist gewöhnlich jede einzelne Verdichterstufe mit nachgeordneter Kühlereinheit in Form eines Zwischen- bzw. Nachkühlers versehen, wobei jeder Kühleinheit mindestens ein Bypassrohr zugeordnet ist.The solution according to the invention is suitable for use in both single-stage and multi-stage compressor units. In the case of a single-stage compressor unit, the cooler unit is provided as an aftercooler, which can then be equipped with at least one bypass pipe according to the invention. In the case of a multi-stage compressor unit usually each individual compressor stage is provided with a downstream cooler unit in the form of an intermediate or aftercooler, wherein each cooling unit is associated with at least one bypass tube.
Unabhängig von der konkreten Ausführungsform der Verdichtereinheit ist das mindestens eine zugeordnete Bypassrohr jedoch vorzugsweise derart auszulegen, dass selbst bei total eingefrorener Kühlereinheit die gesamte Förderleistung der vorgeschalteten Verdichtereinheit über das mindestens eine zugeordnete Bypassrohr leitbar ist.Regardless of the specific embodiment of the compressor unit, however, the at least one associated bypass pipe is preferably designed such that even with a totally frozen cooler unit, the entire capacity of the upstream compressor unit via the at least one associated bypass pipe is conductive.
Weitere, die Erfindung verbessernde Maßnahmen werden nachstehend gemeinsam mit der Beschreibung eines bevorzugten Ausführungsbeispiels der Erfindung anhand der Figuren näher dargestellt. Es zeigt:
- Fig.1
- eine perspektivische Außenansicht einer Kompressoranordnung, und
- Fig.2
- eine schematische Darstellung von Bypassmitteln an der Kühlereinheit der Kompressoranordnung nach
Fig.1 .
- Fig.1
- an external perspective view of a compressor assembly, and
- Fig.2
- a schematic representation of bypass means on the radiator unit of the compressor assembly according to
Fig.1 ,
Gemäß
Gemäß
Das durchgängige, permanent offene Bypassrohr 9 zeichnet sich durch einen Innenquerschnitt aus, welcher derart auf die Förderleistung der Verdichtereinheit 2 sowie die Druckdifferenz zwischen Einlass 5 und Auslass 7 abgestimmt ist, dass das Bypassrohr 9 bei normalen Umgebungstemperaturen einen höheren Strömungswiderstand als die Kühlstruktur 6 verursacht, wogegen bei fortschreitendem Einfrieren der Kühlstruktur 6 in Folge Kristallanlagerung an Wandung und Innenlamellen die Druckluft zunehmend über das Bypassrohr 9 strömt. Es hat sich gezeigt, dass das Bypassrohr 9 bei diesen Bedingungen selbst nicht einfriert, da es zügig aufgeheizt wird durch die Druckluft selbst sowie deren Strömungsreibung im Bypassrohr 9.The continuous, permanently open bypass pipe 9 is characterized by an internal cross-section, which is matched to the capacity of the
Somit wird die Drucklufterzeugung unter minimalem Verlust von Kühl- und Förderleistung aufrechterhalten.Thus, the compressed air generation is maintained with minimal loss of cooling and delivery.
Das Bypassrohr 9 ist hier als eine horizontale gerade Rohrleitung ausgeführt, welche im Strom der die Kühlereinheit 4a durchströmenden Kühlluft liegt, um das Bypassrohr 9 mitzukühlen. Zusätzlich ist in die Wandung des Bypassrohres 9 bei diesem Ausführungsbeispiel ein Sicherheitsventil 10 eingefügt, welches ab einem definierten Druckwert öffnet, um ein Platzen des Bypassrohres 9 zu verhindern. Des weiteren kann das Bypassrohr 9 im Inneren auch Oberflächen- und Querschnittsveränderungen zur Erzielung einer Düsenfunktion haben kann, falls strömungsdynamisch sinnvoll.The bypass pipe 9 is designed here as a horizontal straight pipeline, which lies in the flow of cooling air flowing through the
- 11
- Elektromotorelectric motor
- 22
- Verdichtereinheitcompressor unit
- 33
- Filtereinheitfilter unit
- 44
- Kühlereinheitcooler unit
- 55
- Einlassinlet
- 66
- Kühlstrukturcooling structure
- 77
- Auslassoutlet
- 88th
- Lüfterradfan
- 99
- Bypassrohrbypass pipe
- 1010
- Entwässerungs- und/oder SicherheitsventilDrainage and / or safety valve
Claims (12)
- Compressor arrangement for generating compressed air by means of a motor-driven compressor unit (2), downstream of which is positioned at least one cooler unit (4a, 4b) for cooling the generated compressed air, which compressed air enters into the cooler unit (4a, 4b) via at least one inlet (5), flows through a cooling structure (6) around which cooling air flows and which is composed of a plurality of parallel cooling ducts, and leaves the cooler unit (4a, 4b) via at least one outlet (7), with bypass means being provided between the inlet (5) and the outlet (7) of the cooler unit (4a, 4b) in order to prevent freezing of the cooler unit (4a, 4b) at low ambient temperatures,
characterised in that a continuous and permanently open bypass pipe (9) is provided as a bypass means between the region of the inlet (5) and the region of the outlet (7), the inner cross section of which is matched to the delivery capacity of the compressor unit (2) and to the pressure difference between the inlet (5) and the outlet (7) in such a way that the bypass pipe (9) generates a higher flow resistance than the cooling structure (6) at normal ambient temperatures, whereas with progressive freezing of the cooling structure (6), the compressed air flows to an increasing extent via the bypass pipe (9), the ratio between the inner cross-section [mm2] of the bypass pipe (9) and the output [l/min] at an operating pressure of 10 bar being in the range between 0.8 and 1.2, and in that the bypass pipe (9) is further arranged relative to cooler unit (4a, 4b) in such a way that it lies in the flow of the cooling air passing through cooler unit (4a, 4b). - Compressor arrangement according to claim 1,
characterised in that the pressure difference between the inlet and the outlet of the bypass pipe (9) into / out of the cooler unit (4a; 4b) is a maximum of 0.5 bar. - Compressor arrangement according to claim 1,
characterised in that the bypass pipe (9) has screw connections at both ends, by means of which screw connections a detachable fastening to the cooling unit (4a, 4b) takes place. - Compressor arrangement according to any of the preceding claims,
characterised in that the bypass pipe (9) is embodied either as a vertically or horizontally aligned straight pipe line or in the manner of a hose pipe. - Compressor arrangement according to any of the preceding claims,
characterised in that a dewatering and/or safety valve (10) is inserted into the wall of the bypass pipe (9). - Compressor arrangement according to claim 1,
characterised in that the compressor unit (2) is of single-stage construction with a cooler unit positioned downstream as a post-cooler, which is assigned at least one bypass pipe (9). - Compressor arrangement according to claim 1,
characterised in that the compressor unit (2) is of multi-stage construction with a cooler unit (4a and 4b) positioned downstream of each compressor stage as an intermediate cooler and post-cooler, with each cooler unit (4a and 4b) being assigned at least one bypass pipe (9). - Compressor arrangement according to any of the preceding claims,
characterised in that, in the event of the cooler unit (4a, 4b) being completely frozen up, the entire output of the compressor unit (2) positioned upstream can be conducted via the associated bypass pipe (9), and in that after the freezing has been eliminated, the initial state before the freezing is automatically re-established. - Compressor arrangement according to claim 1,
characterised in that the bypass pipe (9) is integrated into the cooler unit (4a and 4b). - Compressor arrangement according to claim 1,
characterised in that the bypass pipe (9) is provided with cooling ribs or cooling fins or is embodied in the manner of a finned pipe. - Compressor arrangement according to claim 1,
characterised in that the bypass pipe (9) is embodied as or comprises a hollow body mass-produced by casting. - Compressor arrangement according to claim 1,
characterised in that the bypass pipe (9) is embodied as or contains a hose line.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200510053949 DE102005053949B3 (en) | 2005-11-11 | 2005-11-11 | Compressor, for the delivery of compressed air, has a cooling unit for the compressed air with an open bypass tube between the inflow and outflow to prevent freezing |
PCT/EP2006/010780 WO2007054328A1 (en) | 2005-11-11 | 2006-11-10 | Compressor arrangement having bypass means for avoiding freezing of the cooler unit |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1948930A1 EP1948930A1 (en) | 2008-07-30 |
EP1948930B1 true EP1948930B1 (en) | 2016-07-06 |
Family
ID=37111720
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP06818455.5A Not-in-force EP1948930B1 (en) | 2005-11-11 | 2006-11-10 | Compressor arrangement having bypass means for avoiding freezing of the cooler unit |
Country Status (4)
Country | Link |
---|---|
US (1) | US9022068B2 (en) |
EP (1) | EP1948930B1 (en) |
DE (1) | DE102005053949B3 (en) |
WO (1) | WO2007054328A1 (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102013007186A1 (en) * | 2013-04-25 | 2014-10-30 | Man Truck & Bus Ag | Line system for a motor vehicle |
DE102014113598A1 (en) | 2014-09-19 | 2016-03-24 | Knorr-Bremse Systeme für Schienenfahrzeuge GmbH | Multi-stage piston compressor with an external cooling air duct |
DE102016011032B4 (en) | 2016-09-13 | 2023-12-28 | Zf Cv Systems Hannover Gmbh | Pressure supply unit of a motor vehicle |
JP2019108811A (en) * | 2017-12-15 | 2019-07-04 | 工機ホールディングス株式会社 | Gas compressor |
US11681309B2 (en) * | 2019-01-03 | 2023-06-20 | Westinghouse Air Brake Technologies Corporation | Thermal management system and method |
CN112412789B (en) * | 2019-08-23 | 2022-09-06 | 广东美芝制冷设备有限公司 | Compressor and refrigeration cycle device |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3232340A (en) * | 1963-03-26 | 1966-02-01 | Schramm Inc | Air supply system |
DE3307064A1 (en) * | 1983-03-01 | 1984-09-06 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Pneumatic compressor with at least one compressor stage, particularly for high voltage output switches |
GB9324723D0 (en) * | 1993-12-02 | 1994-01-19 | Amot Controls Ltd | Turbocharger control apparatus |
US5623834A (en) * | 1995-05-03 | 1997-04-29 | Copeland Corporation | Diagnostics for a heating and cooling system |
DE19600377B4 (en) * | 1995-12-14 | 2005-10-27 | Wabco Gmbh & Co.Ohg | Compressed gas system with a gas dryer |
US6283725B1 (en) * | 1997-07-21 | 2001-09-04 | Westinghouse Air Brake Company | Aftercooler bypass means for a locomotive compressed air system |
US6027311A (en) * | 1997-10-07 | 2000-02-22 | General Electric Company | Orifice controlled bypass system for a high pressure air compressor system |
US6167956B1 (en) * | 1999-08-24 | 2001-01-02 | Westinghouse Air Brake Company | Aftercooler having bypass passage integrally formed therewith |
US6604515B2 (en) * | 2001-06-20 | 2003-08-12 | General Electric Company | Temperature control for turbocharged engine |
-
2005
- 2005-11-11 DE DE200510053949 patent/DE102005053949B3/en not_active Expired - Fee Related
-
2006
- 2006-11-10 US US12/093,156 patent/US9022068B2/en active Active
- 2006-11-10 WO PCT/EP2006/010780 patent/WO2007054328A1/en active Application Filing
- 2006-11-10 EP EP06818455.5A patent/EP1948930B1/en not_active Not-in-force
Also Published As
Publication number | Publication date |
---|---|
WO2007054328A1 (en) | 2007-05-18 |
DE102005053949B3 (en) | 2006-11-09 |
EP1948930A1 (en) | 2008-07-30 |
US20090151794A1 (en) | 2009-06-18 |
US9022068B2 (en) | 2015-05-05 |
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