EP0043566B1 - Appareil éjecteur - Google Patents
Appareil éjecteur Download PDFInfo
- Publication number
- EP0043566B1 EP0043566B1 EP81105170A EP81105170A EP0043566B1 EP 0043566 B1 EP0043566 B1 EP 0043566B1 EP 81105170 A EP81105170 A EP 81105170A EP 81105170 A EP81105170 A EP 81105170A EP 0043566 B1 EP0043566 B1 EP 0043566B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- ejector device
- sections
- another
- housing
- chambers
- 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.)
- Expired
Links
- 238000010276 construction Methods 0.000 claims description 7
- 210000002445 nipple Anatomy 0.000 claims description 7
- 230000002093 peripheral effect Effects 0.000 claims description 2
- 230000008878 coupling Effects 0.000 claims 1
- 238000010168 coupling process Methods 0.000 claims 1
- 238000005859 coupling reaction Methods 0.000 claims 1
- 238000013016 damping Methods 0.000 claims 1
- 239000012530 fluid Substances 0.000 abstract 1
- 239000007789 gas Substances 0.000 description 18
- 239000003380 propellant Substances 0.000 description 10
- 238000007789 sealing Methods 0.000 description 5
- 238000009826 distribution Methods 0.000 description 4
- 230000006978 adaptation Effects 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000005086 pumping Methods 0.000 description 2
- 238000004026 adhesive bonding Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
- F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
- F04F5/44—Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
- F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
- F04F5/14—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being elastic fluid
- F04F5/16—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being elastic fluid displacing elastic fluids
- F04F5/20—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being elastic fluid displacing elastic fluids for evacuating
- F04F5/22—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being elastic fluid displacing elastic fluids for evacuating of multi-stage type
Definitions
- the invention relates to an ejector device which consists of at least two ejectors formed by a corresponding number of axially successive jet nozzles of increasing size within a common elongate housing which is subdivided by transverse walls containing the jet nozzles into chambers separated from one another by check valves.
- Ejector devices of this type in which the nozzles located between the first and the last nozzle are both driving and catching nozzles, are known in principle.
- their use has hitherto been restricted to the generation of negative pressure for pumping empty containers and the like, with first all chambers with the exception of the chambers following the last nozzle being connected to the container and providing for the extraction of relatively large amounts of air which by gradually closing the check valves with increasing vacuum, until the end only the ejector formed by the first two jet nozzles generates the final vacuum.
- the design of such ejector devices is associated with considerable effort and requires a largely individual adaptation to the individual application.
- the invention is therefore based on the object of creating an ejector device of the type mentioned which, while taking advantage of the economic advantages of mass production, allows easy adaptation to a wide variety of applications without any special processing effort and thereby increases the possible uses of the ejector device.
- the housing in the modular system consists of a plurality of sections which adjoin one another in the longitudinal direction and can be combined with one another as desired, at least some of which each contain one of the said transverse walls.
- the invention is based on the consideration that the number of successive ejectors is different for different applications, and creates in the way of the modular system the possibility of an individual compilation of modular elements designed as sections for an ejector device corresponding to the respective purpose.
- the combination of sections that can be combined with one another in any order enables the individual sections to be produced in large numbers without restricting the possible combinations.
- the production costs are thereby reduced, and the respective suitable ejector device can be put together individually from a limited number of prefabricated sections in the shortest possible time.
- the sections can be assembled in different ways.
- the sections are held together by common connecting means such as continuous tie rods.
- special connecting means can also be provided for connecting two adjacent sections.
- the housing has a circular cross section and the sections are provided with a screw thread.
- the sections can then be screwed together directly.
- the individual sections can each consist of a transverse wall and an adjoining jacket wall.
- the distance between the nozzles is determined by the length of the jacket wall sections.
- a special design feature of the invention provides that the transverse walls on the one hand and the Sheath walls of the chambers on the other hand form separate sections. For these measures, it is sufficient to provide only the sections forming the peripheral walls of the chambers in different lengths in order to be able to take any nozzle spacing into account.
- each transverse wall can contain a jet nozzle, preferably inserted in its center, or also several jet nozzles in any distribution, provided that corresponding transverse walls with a matching nozzle distribution are only available for each nozzle size. It is of course also possible to provide the transverse walls with a corresponding number and distribution of bores from case to case, in which the nozzles are only subsequently inserted in a suitable manner.
- the nozzles can also be formed directly in the transverse walls by appropriately shaped bores.
- the transverse walls each contain one or more through-openings provided with check valves, which at the beginning of the generation of negative pressure allow large amounts of air to be extracted with the aid of all nozzles located one behind the other and then automatically with increasing negative pressure Switch off chambers whose negative pressure is limited due to the increasing nozzle size.
- Yet another design feature of the invention provides that the sections in the region of the jacket walls of the chambers are provided with connection openings into which hose connections, valves or sealing plugs can be screwed.
- a section for forming a pressure chamber following the last jet nozzle is pot-shaped and provided with one or more front and / or radial blow-out openings.
- the blow-out openings can be provided with a thread for screwing in connection nipples or sealing plugs, and finally the cup-shaped section can contain an insert for sound insulation.
- a transverse wall containing the first nozzle has at least one additional opening for connecting a pressure accumulator via a shuttle valve, which can be charged via the latter from a pressure medium source feeding the ejector device.
- the ejector device according to the invention enables a wide variety of uses and thus offers a multitude of advantages over the known ejector devices with a plurality of ejectors.
- the ejector device according to the invention can be used in a known manner for vacuum generation by means of a pressurized gas, for example compressed air, the extracted gas being a multiple of the amount of propellant gas due to the series connection of several ejectors.
- a pressurized gas for example compressed air
- the extracted gas being a multiple of the amount of propellant gas due to the series connection of several ejectors.
- the ejector device according to the invention also enables the simultaneous generation of overpressure and underpressure, as is required, for example, for the mechanical movement of sheets of paper in printers.
- overpressure and underpressure as is required, for example, for the mechanical movement of sheets of paper in printers.
- the special arrangement of the additional opening in the transverse wall containing the first nozzle for connecting a pressure accumulator via a shuttle valve also enables an abrupt cancellation of the negative pressure and generation of excess pressure when the propellant gas is switched off in this type of application, in that case the shuttle valve changes itself and so far connecting chamber under vacuum, to which the suction devices of the machine are connected, connects to the pressure accumulator. The paper sheets sucked in are released immediately.
- gases can also be mixed in a simple manner, a pressurized first gas being used as the propellant gas and further gases being sucked into the intermediate chambers between the individual jet nozzles and being mixed with one another in the process.
- the mixing of gases with liquids and / or powdered or granulated solid substances is also possible in the same way.
- the ejector device enables the amount of gas used as the propellant gas to be multiplied with a corresponding reduction in its pressure, with the lowest energy expenditure. For example, if five ejectors are connected in series, this results in a blow-out amount of gas which is at least (eight times the amount of propellant gas used with a corresponding reduction in pressure).
- 1-5 denotes five jet nozzles increasing in size in the order of the designation numbers, which in the example form a single nozzle set located in the central axis of the ejector device.
- the jet nozzles 1-5 are used in receiving bores within transverse walls 6-10 by pressing, gluing or screwing or can also be part of these walls.
- the construction A provides that the transverse walls, as in the example the transverse wall 10, each form a section and are received by a recess delimited by a shoulder within a section 11 forming the jacket wall of a subsequent chamber, in which they are held by a further jacket wall section 12 are held and sealed, which are provided with an external thread and are screwed into the subsequent jacket wall section 11 provided with an internal thread within the recess.
- This construction is particularly suitable in the event that the transverse wall contains a plurality of eccentric nozzles (not shown) which must be aligned with one another from transverse wall to transverse wall.
- Construction B provides that the transverse walls, such as walls 6-9 in the example, connect in one piece to a jacket section and thereby form a continuous segment with this, which is directly connected to the ends by means of internal and external threads adjacent section can be screwed. It is obvious that this construction can only be used in connection with a central jet nozzle.
- the chambers 13-16 created between the individual jet nozzles by the segment design described above are connected to one another by bores 17-20 in the transverse walls, which have non-return flaps 21-24 which close as soon as the negative pressure in one chamber becomes greater than in the subsequent chamber .
- the last chamber 25 is under pressure during operation.
- the individual chambers 13-16 contain radial connection openings 26-29, which are provided with threads and, depending on the intended use, enable the attachment of connecting nipples or sealing plugs.
- the segment 11 which is designed to seal off the device and is cup-shaped, is provided with radial connection openings 30a and an axial connection opening 30b, into which connection nipples or sealing plugs 31a, 31b can be inserted.
- the first transverse wall 6 contains a pressure distribution chamber 32 in front of the jet nozzle 1 or possibly several such jet nozzles used therein, to which a connecting nipple 34 inserted into a bore 33 leads for the supply of the propellant gas to the ejector device.
- the chamber 13 located between the first and second jet nozzles 1 and 2 is also connected via a connection opening 35 in the transverse wall 6 to the one connection of a shuttle valve 36, the other connection of which is connected to the propellant gas supply line leading to the connection nipple 34 and to the third one Connection is a pressure accumulator 37.
- This arrangement ensures that when the propellant gas supply to the nozzle 1 is switched off via the connecting nipple 34, the negative pressure in the chamber 13 immediately breaks down as a result of the changeover valve 36 being switched over, and instead an excess pressure builds up in the chamber 13 from the pressure accumulator 37.
- a regulator 38 in the propellant gas supply line enables the pressure and quantity of the propellant gas to be regulated continuously.
- a muffler 39 projecting into the last chamber 25 can be arranged on the segment 11.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Jet Pumps And Other Pumps (AREA)
Claims (14)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT81105170T ATE7244T1 (de) | 1980-07-05 | 1981-07-03 | Ejektorvorrichtung. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3025525 | 1980-07-05 | ||
DE19803025525 DE3025525A1 (de) | 1980-07-05 | 1980-07-05 | Ejektorvorrichtung |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0043566A1 EP0043566A1 (fr) | 1982-01-13 |
EP0043566B1 true EP0043566B1 (fr) | 1984-04-25 |
Family
ID=6106489
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP81105170A Expired EP0043566B1 (fr) | 1980-07-05 | 1981-07-03 | Appareil éjecteur |
Country Status (5)
Country | Link |
---|---|
US (1) | US4466778A (fr) |
EP (1) | EP0043566B1 (fr) |
JP (1) | JPS5783699A (fr) |
AT (1) | ATE7244T1 (fr) |
DE (1) | DE3025525A1 (fr) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE427954B (sv) * | 1979-06-15 | 1983-05-24 | Piab Ab | Ejektor |
IL70239A (en) * | 1983-11-15 | 1988-03-31 | Dan Greenberg | Multichamber ejector |
DE3431240A1 (de) * | 1984-08-24 | 1986-03-06 | Michael 4150 Krefeld Laumen | Kaeltemaschine bzw. waermepumpe sowie strahlpumpe hierfuer |
IL74282A0 (en) * | 1985-02-08 | 1985-05-31 | Dan Greenberg | Multishaft jet suction device |
US4790054A (en) * | 1985-07-12 | 1988-12-13 | Nichols William O | Multi-stage venturi ejector and method of manufacture thereof |
US4759691A (en) * | 1987-03-19 | 1988-07-26 | Kroupa Larry G | Compressed air driven vacuum pump assembly |
ATE111569T1 (de) * | 1987-06-29 | 1994-09-15 | Thilo Volkmann | Strahlpumpe. |
JPH0247618U (fr) * | 1988-09-24 | 1990-03-30 | ||
AU628595B2 (en) * | 1989-07-10 | 1992-09-17 | John Stanley Melbourne | Improved vacuum pump device |
JP2878385B2 (ja) * | 1990-04-20 | 1999-04-05 | エスエムシー株式会社 | エゼクタ装置 |
DE4032857C1 (en) * | 1990-10-12 | 1992-01-23 | Noell Gmbh, 8700 Wuerzburg, De | Bendable grab unit for remote searching - has illumination member and flexible coating unit |
JPH0467618U (fr) * | 1990-10-18 | 1992-06-16 | ||
US5228839A (en) * | 1991-05-24 | 1993-07-20 | Gast Manufacturing Corporation | Multistage ejector pump |
SE469291B (sv) * | 1991-10-31 | 1993-06-14 | Piab Ab | Ejektorarrangemang innefattande minst tvaa tryckluftsdrivna ejektorer samt foerfarande foer att med minst tvaa tryckluftsdrivna ejektorer aastadkomma ett oenskat undertryck paa kortast moejliga tid och med minsta energifoerbrukning |
US5683227A (en) * | 1993-03-31 | 1997-11-04 | Smc Corporation | Multistage ejector assembly |
DE4430574C2 (de) * | 1994-08-18 | 1996-07-18 | Mannesmann Ag | Strahlpumpe mit zwei Überschalldüsen |
DE4432441A1 (de) * | 1994-09-12 | 1996-03-14 | Sellmaier Horst | Mischdüse |
SE511716E5 (sv) * | 1998-03-20 | 2009-01-28 | Piab Ab | Ejektorpump |
IL125791A (en) * | 1998-08-13 | 2004-05-12 | Dan Greenberg | Vacuum pump |
DE29916531U1 (de) * | 1999-09-20 | 2001-02-08 | Volkmann Thilo | Ejektorpumpe |
DE20011839U1 (de) | 2000-07-07 | 2000-12-14 | Festo Ag & Co | Vakuumerzeugervorrichtung |
KR20030077349A (ko) * | 2002-03-26 | 2003-10-01 | 삼조쎌텍 주식회사 | 이소플라본을 함유하는 기능성 츄잉 껌 |
SE0201335L (sv) * | 2002-05-03 | 2003-03-25 | Piab Ab | Vakuumpump och sätt att tillhandahålla undertryck |
KR100629994B1 (ko) * | 2005-12-30 | 2006-10-02 | 한국뉴매틱(주) | 진공 이젝터 펌프 |
KR100730323B1 (ko) * | 2007-03-15 | 2007-06-19 | 한국뉴매틱(주) | 필터 카트리지를 이용한 진공 시스템 |
AU2009291925B2 (en) * | 2008-09-09 | 2015-11-19 | Dresser-Rand Company | Supersonic ejector package |
US20100150743A1 (en) * | 2008-12-12 | 2010-06-17 | Norgren Automotive, Inc. | Single Line Venturi Apparatus |
GB2509184A (en) | 2012-12-21 | 2014-06-25 | Xerex Ab | Multi-stage vacuum ejector with moulded nozzle having integral valve elements |
GB2509182A (en) | 2012-12-21 | 2014-06-25 | Xerex Ab | Vacuum ejector with multi-nozzle drive stage and booster |
US10753373B2 (en) * | 2012-12-21 | 2020-08-25 | Piab Aktiebolag | Vacuum ejector nozzle with elliptical diverging section |
GB2509183A (en) | 2012-12-21 | 2014-06-25 | Xerex Ab | Vacuum ejector with tripped diverging exit flow nozzle |
KR101424959B1 (ko) | 2014-04-08 | 2014-08-01 | 한국뉴매틱(주) | 진공펌프 |
GB201418117D0 (en) | 2014-10-13 | 2014-11-26 | Xerex Ab | Handling device for foodstuff |
CN105156787A (zh) * | 2015-08-12 | 2015-12-16 | 安徽亿能机械有限公司 | 一种双腔室增压接头 |
CN108290297B (zh) | 2015-09-08 | 2021-12-03 | 伯克希尔格雷股份有限公司 | 用于在自动系统中提供高流量真空采集的系统和方法 |
KR101699721B1 (ko) | 2016-09-01 | 2017-02-13 | (주)브이텍 | 진공 펌프 및 그 어레이 |
CN107859658B (zh) * | 2017-10-27 | 2019-02-19 | 江苏大学 | 一种可调节开度的射流自吸系统 |
EP3706966A2 (fr) | 2017-11-07 | 2020-09-16 | Berkshire Grey, Inc. | Systèmes et procédés permettant de fournir une pression de vide dynamique au niveau d'un effecteur d'extrémité à l'aide d'une source de vide unique |
KR102194572B1 (ko) * | 2019-01-08 | 2020-12-23 | 이효길 | 진공펌프 |
WO2020145628A1 (fr) * | 2019-01-08 | 2020-07-16 | 이효길 | Pompe à vide et récipient sous vide comportant une telle pompe |
KR102344214B1 (ko) * | 2021-05-18 | 2021-12-28 | (주)브이텍 | 진공 이젝터 펌프 |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB339402A (fr) * | 1900-01-01 | |||
US1423198A (en) * | 1922-07-18 | Vacuum jet and system of operating the same | ||
FR361049A (fr) * | 1905-11-27 | 1906-05-14 | Westinghouse Electric Corp | Système de diffuseur perfectionné pour éjecteur |
AT30001B (de) * | 1905-12-07 | 1907-09-25 | Westinghouse Sa | Ejektor für zusammendrückbare Flüssigkeiten. |
CH101872A (fr) * | 1921-12-12 | 1923-11-01 | Eugene Caron Virgile | Procédé et appareil pour l'aspiration et la compression d'un fluide gazeux. |
US2000762A (en) * | 1933-10-26 | 1935-05-07 | Gen Electric | Fluid jet pump |
FR842373A (fr) * | 1938-02-11 | 1939-06-12 | Robinetterie S A J Soc D | Hydro-éjecteur à multiple effet |
US2378425A (en) * | 1938-02-22 | 1945-06-19 | Murray Henry Lamont | Ejector-condenser |
US2211795A (en) * | 1938-07-06 | 1940-08-20 | Harry R Levy | Attachment for internal combustion engines |
US2275627A (en) * | 1939-04-03 | 1942-03-10 | Milford W Hartmann | Pumping system |
FR933502A (fr) * | 1946-09-03 | 1948-04-23 | Procédé de fabrication d'éjecteurs et éjecteurs obtenus selon ce procédé | |
BE532754A (fr) * | 1953-10-23 | |||
DE953280C (de) * | 1954-04-08 | 1956-11-29 | Carl Metz Feuerwehrgeraetefabr | Mehrstufiger Strahlapparat zum Entlueften von Pumpen, Behaeltern u. dgl. |
US3445335A (en) * | 1965-05-28 | 1969-05-20 | Gen Electric | Nuclear reactor system with jet pump flow means |
DE1503706C3 (de) * | 1965-06-19 | 1971-09-02 | Siemens Ag | Einer vakuumpumpe vorschaltbare strahlsaugeraggregate |
RO55562A2 (fr) * | 1971-05-28 | 1973-09-20 | ||
SE370765B (fr) * | 1973-12-05 | 1974-10-28 | Piab Ab | |
CA1080121A (fr) * | 1977-12-19 | 1980-06-24 | Edward A. Kempton | Procede d'evacuation de l'eau des puits de gaz |
SE427954B (sv) * | 1979-06-15 | 1983-05-24 | Piab Ab | Ejektor |
-
1980
- 1980-07-05 DE DE19803025525 patent/DE3025525A1/de active Granted
-
1981
- 1981-07-03 JP JP56103447A patent/JPS5783699A/ja active Granted
- 1981-07-03 EP EP81105170A patent/EP0043566B1/fr not_active Expired
- 1981-07-03 AT AT81105170T patent/ATE7244T1/de not_active IP Right Cessation
- 1981-11-20 US US06/323,375 patent/US4466778A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US4466778A (en) | 1984-08-21 |
EP0043566A1 (fr) | 1982-01-13 |
DE3025525C2 (fr) | 1987-05-21 |
DE3025525A1 (de) | 1982-01-28 |
JPS5783699A (en) | 1982-05-25 |
ATE7244T1 (de) | 1984-05-15 |
JPS6329120B2 (fr) | 1988-06-10 |
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