DK178324B1 - TANKS, PARTICULARLY FOR USE AS A BUFFER TANK IN AIR PRESSURE - Google Patents

TANKS, PARTICULARLY FOR USE AS A BUFFER TANK IN AIR PRESSURE Download PDF

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Publication number
DK178324B1
DK178324B1 DK201400495A DKPA201400495A DK178324B1 DK 178324 B1 DK178324 B1 DK 178324B1 DK 201400495 A DK201400495 A DK 201400495A DK PA201400495 A DKPA201400495 A DK PA201400495A DK 178324 B1 DK178324 B1 DK 178324B1
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DK
Denmark
Prior art keywords
tank
tank according
shell parts
sections
shell
Prior art date
Application number
DK201400495A
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Danish (da)
Inventor
Kim Villadsen
Original Assignee
Hbn Teknik As
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Publication date
Application filed by Hbn Teknik As filed Critical Hbn Teknik As
Priority to DK201400495A priority Critical patent/DK178324B1/en
Application granted granted Critical
Publication of DK178324B1 publication Critical patent/DK178324B1/en

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  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

By preparing a buffer tank of the two tank halves (1 and 2), and the interior of the tank space (11) to place the damping plates (4) respectively by tillednings- and the discharge end, there will be achieved an attenuation without compromising the buffer effect. Furthermore, there will between the tank halves (1 and 2) would be inserted one or more additional damping means in the form of the attenuation sections (20), said sections comprising a plate member (21) with through openings (22) for further attenuation.

Description

TANK, ESPECIALLY FOR USE AS A BUFFER TANK IN AIR SYSTEMS
OejikendteteMh
The invention relates to a tank, in particular II! fe back as a buffer tank in the compressed air load, which tank comprises an outer tank should to form an inner cavity, and with pipe connections for the air inlet and outlet, and wherein the tank consists of two tanks have to share with each one tiislutningssfuds which must portions are dimensioned to sammeh ^ efses ten formation of the internal cavity.
Shells of this kind is preferably used in compressed air systems, where there are pressure variations in that the air by passing through such a tank is equalized trykvabatonefne, i.e. udjævnef trykvanatiorieroe on the discharge side. To which, the idea opmagasinerer desn excess trykluiSxkåpaeiteh when air consumption periods are reduced relative file compressor kapapitaf.
It includes such bufferlanke in all systems with varying air demand.
From US 2010/0075200 Eel <Ende an example of eft tank for storing gas under high pressure, which tank comprises a iankskal teh, forming an internal lumen and including pipe connections for the gas inlet and discharge, which tank be made up of two shell portions, each a connecting stub ,, and wherein skaldeten is sized hl saromensvejses TLI to form the cavity.
The disadvantage of the known thought is the not the sufficiently dampens sound that occurs when pulsating air tightens through the tank, then the parts will be set to vibrate, thus producing a rowers or less vigorous and generiode noise.
The purpose of the invention
The invention aims to remedy this deficiency and improve the possibilities of adapting tanks conditions, thus ensuring the best possible attenuation Oden that it changes the buffer function.
Pete is achieved according to the invention, by a tank in which, in connection to the studs within the cavity are mounted baffles, which forms the bottom in the way with pass-through openings formed to guide tongue partition the lot file striking the piespladerne.
In this way, the sound will be muted upon impact against prelplsdeo, respectively by supply and discharge. Tank Space will also act as the known buffer tanks. For further reduction can be one tank compartment hospitalized absorbing material behold like a sponge or the like;
As disclosed in claim 2, inserting one or Liere sections with damping properties between the shell parts will be in a surprisingly simple way to dimension thought banquets conditions, and thus achieve a tank, etc. will give the opfimåle: noise reduction.
As disclosed in claim 3 s, leveling passages in each of the damping plates symmetrically to the plate center, we! at tanks with several: sections could be attenuated by shifting the maximum of the holes relative to each other by rotating the individual plates such that the air is forced to a centrifuging which will incorporate sfømftlhgåBhefgl. This will ensure m rfiakphiaj soundproofing.
Do you know the meaning of claim 4 of designing one shell part and damping section with an outer rim that can enclose the adjacent shell portion and at the same time provide the other shell part and dimming sections with: m inner rim, and jade these circles run in a spaced, will form an abutment surface.
: Hereby, the parts could be a kit which allows for construction of a buffer tank with a dæmpniogseffekt adapted imi conditions *
When, as in ombandfet. S claim that dlmertelønere and shaping skaldetene and attenuation sections with circular installation surfaces of the same diameter, the parts could be assembled to form the finished tank.
As disclosed in claim 6 that produced ice parts in plastic, the parts can be partly carried out in a vibration damping material could partly assembled by sammensvejsnlng ai the parts.
At that address! in claim 7, to provide the bearing surface with a tongue and a cooperating groove, will be referred to f claim 8, sømmensvefse to those portions and thus Upon spin welding.
Finally, we know that deal! In claim 9, to design the air flows in the tank so as to extend around the center line of the tank room, achieve effective and a komoaKt tyddærøpniog design, the respiratory tract will meander through the openings dg consume energy.
Bipligia
Udførelseseksempter of the invention will get what due time be further described with referring to Fig drawing, in which Fig. 1 shows a tank without attenuation section inserted, viewed frå side rich. 2 shows the tank seen i- a deisnli, Fig .. 3 shows fanken Shown in an enlarged partial section, equal. 4 shows a tank with two inserted dæmpningssekhoner side view,% S vieer ie individual parts 1 disassembled state and FIG. 6 Displays this tank seen in a partial section.
Description sf udføreiseseksemofeme That first Udførelseseksemp! L nail will felive besteveti is at% 1-3 tank.
This tank is constructed of two parts to be halvkugleforroede 1 and 2 which are assembled to form an enclosed inner cavity 11 "
Each shell 1 and 2 is provided with either an inlet or an outlet, which is done via the connecting pieces S, a: Preferably, the shells are mounted on the apex
Each of these connection pieces 3: W, as shown peftg, 2 and 3 are formed as outwardly projecting connecting pieces, which can be provided with a not shown internal thread for saMrrie ^ rønfcg with trykiurtsanlæggei inside skaldelens cavity 11, the spigot is provided with a dividing wall 14 which at the end is closed by a plate 4. Furthermore, hulier 5 formed through the partition wall 10 with a view to the air passage
Purpose: to this arrangement, by forming both a damping of the connecting stub to 3, tllledes compressed air, whose flow path is indicated by the 'broken line 12.
By air inlet ten! 3 spigot air will flow against the inner side of the plate 4, which will act as a preiplade and thus dampen the air velocity and the recording energy from the air and thus dampen the pulsation.
After the air in the suppressed state pass across through the openings S and Into the cavity 11th
In tankrummeis opposite end which is at the top in the drawing, the air will abut against the one mounted prelpla.de 4 that will further attenuate the pulsation. After that air movement across gennemskiHevæggens 1G openings 5 ​​and out through the outlet 3. The air will thus be attenuated while the tank space 11 to act as a buffer chamber.
This will resulere in a dampening of luftpulsationen and thus a significant reduction in noise emissions as the energy in the air will be reduced through these attenuation and afbopingsmidler.
The parts; is preferably produced by casting in one kunststot édfn per åelv will constitute err damping factors may be due to the material's insignificant egensvmgning which iuftpuisationen VJI have on the relatively soft material.
The assembly of the two shell portions 1 oak 2 will now be described
Each shell part are provided at their open end of the circular increment of the same diameter so as to we! able to bear against each other, with their end faces will be the bearing surface 13. In order to ensure that the parts are not displaced or deformed during use, there is a pi outside of the one shell part 1 formed an outer rim 6; which extends about the second shell portion 2 shown in fig..2 sorn.
In order to weld these elements and 2, there may, as shown in rig. 2 and 3, be designed in one fjerlsgnende maieriaiefprøgelse S of the one shell part 1 and, if a groove 8 on the second shell 2 such that by a rotation welding will occur © s melting tjsfen § and thus a welding together of the two parts 1 and 2
To further strengthen the joint, may be made, as shown in Fig. 2 and 3, on the supports © shell portion 2 may be formed an inner peripheral% which may be either m against the upper shell portion 1 inside surface.
Pi this way, there is formed an enclosed tank, as prepared 1 will be weldable plastic, stretch © g with a high attenuation rate due to the inner dæmpningsforanstaitninger. If required, can be observed in the damping material ianktummei for further attenuation. This d ^ mpdingsef ^ kt is obtained ydéh to bufféregenskaberne is affected.
Then we! it tig. 4 * 8 in the example shown, a buffer tank will be described.
Also this tank is built in shell parts 1 and 2, which is identical with the pi tig. 1-3 tank. Between these must share 1 and 2, in the example shown inserted two damping sections 20th
Each of these: sections 20 consisting of fen circular plådedel 21, as shown in ft g. 5 and Sv Along piadedetens 21 penfen is cer-shaped peripheral portion 8 by 1 its shape is identical to the opposite party on the upper shell part 1, in pladedeten 21 there are formed openings 22, which preferably extends at the same distance from the plate center. In this way, the individual sections 20 prior to the welding, are rotated relative to each other eg ;, thereby extending the air flow path 12 through iankrummef 11.
The manufacture and assembly of the parts 2 and 20 are similar to dies on Fig. 1-3-described tank.
The purpose of the insertion of the attenuation sections 20 is to dampen yderigere and by choosing the number of sections to produce a buffer tank with a specified attenuation rate.
Hereby it is in a surprisingly simple rnåde possible to adjust the damping level is filled as needed, while maintaining the desired buffarefekt.
The flow of air through the tank with two damping sections 20 will. as indicated by dotted: line 12 of FIG. 6, be dampened partly affected by attacks against preipladen 4 at iuMlednlngen know spigot 3 at anslåg against dam plate 21, the deflection then at ports 22:01 additional plate 21 with openings and finally with preipladen 4 (after which the air will leave the tank through efgangssfudsen third
This combination of 'pulsation and changing sfromnfngsv ^ one will effectively smooth the air being pulsation and thus dampen the noise, fdeftil comes the material's ability ten! are to absorb vibrations due to its relative resilience.
manufacture of plastic has the obvious advantage that the tank is not particularly susceptible to transmissible external influences dg tédenmåjlæ down for wrestling.
in the shown example there are shown two damping sections 20, but this is merely to illustrate the principle in the tank. There will naturally be able to be inserted from one or more sections to obtain a specific dærnpnlngseffekt.

Claims (6)

  1. 2, Tank according to claim 1, characterized in that between the shell parts (1,2} additional erlndsåt and weld together? For the shell parts (1,2) one or more damping sections (20), which section consists of a plate member (21) with passage openings ( 22), and having a rim portion (i) which corresponds to skaldelenes (1) such that portions (1,2 and 20) can be welded together.
  2. 3, tank according to claims 1 and 2, know β egneived in that the openings (22) are spaced substantially the same distance from each other and the same distance S fa rim; partlet: (i):;
  3. 4 Tank according to claims 1-3, ke ri defeg π etved that the border portion (6) on one of the shell parts (1), eg each of dærnpningssekfioneme (20) is formed: rne4 an outer rim (6), while the second shell portion ( 2) and each of the attenuation sections (20) is formed with an inner rim (7), said edges (6,7) extend respectively outside and inside with one intermediate anlægsfiade (13) which constitutes samroensvejsningsfladen,
  4. 5, TånkIfølge (to claims 1-4, c vc one acterised in that the shell parts (1,2) and dæmpnmgssektionen (20) each have arkulær anlægsfiade (13) of the same diameter. S, Tank according to claims 1-5 .kendetegnet in that that both shell parts (1.2) as damping sect one (20) is made of plastic,
  5. 7, A tank according to claim 4-6, know 'tegneived that the intermediate abutment surface (13) are respectively provided with a tongue (9) dg samvirkeridé one groove (B) on opposite flattened !, which the feathers (9) and groove ( 6) Kah welded together.
  6. 8. Tank according to claim 1, ktneif tegnelved, the shell parts (1,2} and oæmpn ngssektlonen (20) sammensvejsøs in the abutment surfaces (13) by spin welding. In. Hd eteg networks ve 4 that each connector (3): s pladeret ' "trust! y $ * -Skaldelen (1,2) such that tuftstrsmningen (12) tlhkmhimet: § 1): fdriødsr around the cavity døhtørlnje · dg across the baffle plates (4) and oæmpningssekilonens pladedei (21),
DK201400495A 2014-09-02 2014-09-02 TANKS, PARTICULARLY FOR USE AS A BUFFER TANK IN AIR PRESSURE DK178324B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DK201400495A DK178324B1 (en) 2014-09-02 2014-09-02 TANKS, PARTICULARLY FOR USE AS A BUFFER TANK IN AIR PRESSURE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DK201400495A DK178324B1 (en) 2014-09-02 2014-09-02 TANKS, PARTICULARLY FOR USE AS A BUFFER TANK IN AIR PRESSURE
DK201400495 2014-09-02

Publications (1)

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DK178324B1 true DK178324B1 (en) 2015-12-07

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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040026431A1 (en) * 2002-01-18 2004-02-12 Jones Brian H Low weight high performance composite vessel and method of making same
US20100075200A1 (en) * 2008-09-22 2010-03-25 Ken Hatta High-pressure tank, method of manufacturing high-pressure tank, and manufacturing equipment of high-pressure tank
WO2013026140A1 (en) * 2011-08-22 2013-02-28 Tranzgaz Inc. Method of fabricating type 4 cylinders and arranging in transportation housings for transport of gaseous fluids

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040026431A1 (en) * 2002-01-18 2004-02-12 Jones Brian H Low weight high performance composite vessel and method of making same
US20100075200A1 (en) * 2008-09-22 2010-03-25 Ken Hatta High-pressure tank, method of manufacturing high-pressure tank, and manufacturing equipment of high-pressure tank
WO2013026140A1 (en) * 2011-08-22 2013-02-28 Tranzgaz Inc. Method of fabricating type 4 cylinders and arranging in transportation housings for transport of gaseous fluids

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Effective date: 20200902