CN101067471B - Container in automobile - Google Patents

Container in automobile Download PDF

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Publication number
CN101067471B
CN101067471B CN2007101023848A CN200710102384A CN101067471B CN 101067471 B CN101067471 B CN 101067471B CN 2007101023848 A CN2007101023848 A CN 2007101023848A CN 200710102384 A CN200710102384 A CN 200710102384A CN 101067471 B CN101067471 B CN 101067471B
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CN
China
Prior art keywords
container
edge
halfbody
zone
container halfbody
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Active
Application number
CN2007101023848A
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Chinese (zh)
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CN101067471A (en
Inventor
M·蒂特尔
N·伯格
A·尤贝莱克
T·莫桑迪尔
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MAN Truck and Bus SE
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MAN Truck and Bus SE
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Publication date
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Publication of CN101067471A publication Critical patent/CN101067471A/en
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Publication of CN101067471B publication Critical patent/CN101067471B/en
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01—Shape
    • F17C2201/0104—Shape cylindrical
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/03—Orientation
    • F17C2201/035—Orientation with substantially horizontal main axis
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05—Size
    • F17C2201/056—Small (<1 m3)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634—Materials for walls or layers thereof
    • F17C2203/0636—Metals
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634—Materials for walls or layers thereof
    • F17C2203/0658—Synthetics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00—Vessel construction, in particular methods of manufacturing
    • F17C2209/22—Assembling processes
    • F17C2209/221—Welding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00—Vessel construction, in particular methods of manufacturing
    • F17C2209/22—Assembling processes
    • F17C2209/227—Assembling processes by adhesive means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00—Handled fluid, in particular type of fluid
    • F17C2221/03—Mixtures
    • F17C2221/031—Air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0107—Single phase
    • F17C2223/0123—Single phase gaseous, e.g. CNG, GNC
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/035—High pressure (>10 bar)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/036—Very high pressure (>80 bar)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/01—Improving mechanical properties or manufacturing
    • F17C2260/011—Improving strength
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/01—Improving mechanical properties or manufacturing
    • F17C2260/013—Reducing manufacturing time or effort
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/05—Improving chemical properties
    • F17C2260/053—Reducing corrosion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00—Applications
    • F17C2270/01—Applications for fluid transport or storage
    • F17C2270/0165—Applications for fluid transport or storage on the road
    • F17C2270/0168—Applications for fluid transport or storage on the road by vehicles
    • F17C2270/0171—Trucks
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00—Applications
    • F17C2270/01—Applications for fluid transport or storage
    • F17C2270/0165—Applications for fluid transport or storage on the road
    • F17C2270/0168—Applications for fluid transport or storage on the road by vehicles
    • F17C2270/0176—Buses

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Glass Compositions (AREA)
  • Compressor (AREA)
  • Motor Or Generator Frames (AREA)
  • Details Of Rigid Or Semi-Rigid Containers (AREA)
  • Cartons (AREA)
  • Containers Having Bodies Formed In One Piece (AREA)
  • Body Structure For Vehicles (AREA)
  • Transmission Of Braking Force In Braking Systems (AREA)

Abstract

The invention relates to a container (1) in a vehicle comprising two container half bodies (2, 4) manufactured by molding of sheet steel, whose edges (12, 14) that overlap in an related joint area (16) are contacted together by pasting. The invention provides that the edges (12, 14) of the container half bodies (2, 4) are bent at an acute angle (Alpha) to the areas (8, 10) close to the edges (12, 14); in a way they are parallel to each other at least in the related joint area (16). The invention also provides the adhesive substance for a pasting gap or a joint gap (18) set between the edges.

Description

Container in the automobile
Technical field
The present invention relates to a kind of by the container in claim 1 automobile as described in the preamble, the compressed air container in the load-carrying vehicle particularly, this container comprises the container halfbody of two cup-shapeds of making by steel plate deformed, and the edge in the regional inside lap of overlap joint of this container halfbody interconnects by stickup.
Background technique
Compressed air container in the load-carrying vehicle is used for storing compressed air, this pressurized air is as the operation medium of the compressed air brake of load-carrying vehicle and other device, for example as pressurized air spring, door control equipment or as the operation medium of hoist or lift.In addition, in load-carrying vehicle, use other container, for example fuel container or urea container.
Such compressed air container is disclosed in DE 199 57 855 A1.At this, the edge of container halfbody is not for example by bonding thermal bonding, thereby has avoided the damage to corrosion-inhibiting coating that for example causes by significant high temperature in welding process.In addition, the edge in engaging zones overlaps with the form from the outstanding flanging of shell wall radially outward.Yet the manufacturing of flanging needs certain cost.In addition, can make the dangerous increase of warpage in this case, this warpage is dangerous can to produce negative effect to dimensional stability.
Summary of the invention
Relative therewith, task of the present invention is that further exploitation starts described this container, makes and more easily make this container under the high-intensity situation of the connection that obtains the container halfbody.
By the present invention, this task solves by the feature of claim 1.
The present invention proposes, the edge of container halfbody is carried out bending with acute angle with respect to the zone in abutting connection with this edge, make this edge in the overlap joint zone, just extend in parallel to each other at least, and jointing material is set for being arranged between these edges bonding seam or joint close.
By the edge of container halfbody along its flat curved engaged, produce big adhesive surface on the one hand, guarantee the firm connection of container halfbody thus.In the shell wall of container halfbody, cause more small stress because only the edge is carried out the bend ratio multilayer folding with acute angle, thus when distortion, reduced material warp, and improved dimensional stability.The slope shape of container halfbody in its fringe region engages and makes the jointing material of arranging therebetween when the container halfbody engages can not extrude from bonding seam or joint close especially especially.
Can be implemented in the present invention described in the claim 1 by the measure of listing in the dependent claims advantageously further expands and improves.
Particularly preferably be, the edge of one of them container halfbody is outwards flatly crooked in the overlap joint zone, and the edge of another container halfbody extends from cross section with looking gable shape.Such gable shape edge is made up of smooth section slope shape, that radially outward points to from axially looking, this section connects smooth section same slope-shaped but that radially inwardly point to after surpassing peak, this section while also forms marginal end.Gable shape edge is configured to stiffening rib basically, has increased wall of a container body rigidity by this stiffening rib.
In zone at joining edge, the inside dimension of one of them container halfbody is substantially equal to the inside dimension of another container halfbody and when simultaneously the inside dimension of another container halfbody in the free-ended zone at its edge is more than or equal to the inside dimension in the zone of described container halfbody at joining edge, though when having big manufacturing tolerances, also prevented the edge of container halfbody when axial engagement, slide into each other above and cause not in accordance with regulations along edge join.
Overlap joint in the zone the edge and be preferably located in 2 in abutting connection with the angle between the zone at this edge and spend in the scopes of 15 degree, particularly preferably be about 8 degree.
By other measure, the edge of at least one container halfbody overlap joint can be provided with in the zone at least one along the container circumferential ring around stiffening rib or groove, this stiffening rib or groove are used for holding Sealing to small part, and the sealing part contacts the edge of another container halfbody hermetically.Basically only bear seal action when seeing when additionally Sealing being prepended to the bonding seam that is provided with jointing material or joint close, yet bonding position has alleviated burden thus and has just born the joint of container halfbody by Sealing from the inner chamber of described container.Thus, protect bonding position to avoid the Korrosionsmedium effect in an advantageous manner.
Simultaneously also be that the Sealing of spacing washer that is used for the edge to be joined of container halfbody is responsible for keeping the desirable thickness of bonding seam especially.Before and after a plurality of Sealings, arrange successively, thereby the edge of container halfbody can in mutual support on a plurality of positions and when Bond can not overturn between hardening period relatively, this function can particularly advantageously be implemented.
Described container is particularly preferred for the pneumatic braking device as the compressed air container that is used for storing compressed air in load-carrying vehicle.
From the feature that other dependent claims, illustrates, obtain other advantage.
Description of drawings
Below embodiments of the invention shown in the drawings and in description subsequently, it being elaborated.Accompanying drawing illustrates:
Fig. 1 is the viewgraph of cross-section by the overlap joint zone of the container halfbody of the compressed air container of preferred implementation;
Fig. 2 is the viewgraph of cross-section by the overlap joint zone of the container halfbody of the compressed air container of another kind of mode of execution.
Embodiment
In Fig. 1 only with shown in the interception way and whole container with 1 sign by preferred purposes as the compressed-air actuated compressed air container that stores the pneumatic braking device be used for load-carrying vehicle.Scheme as an alternative, this container can be used for storing and be used for the pressurized air that any pressurized air in the automobile uses device, for example are used for the railcar gate operator, are used for the pressurized air spring or are used for other Pneumatic automobile device or automobile mechanism.
As shown in Figure 1, compressed air container 1 is assembled by the container halfbody 2,4 that preferably has circular cross section of for example two identical sizes, and two container halfbodies pass through the joint connection hermetically mutually of their public join domains 6. Container halfbody 2,4 is preferably made by the steel plate that is provided with corrosion-inhibiting coating at internal surface, and this steel plate for example forms the shape of cup-shaped by deformation process by deep-draw.This means, each in the container halfbody 2,4 all by the bottom that can not see here and thus the shell wall given prominence to of right angle 8,10 with opening with leaving form, opening is respectively by edge 12,14 gauges.In case of necessity, also can also can not use corrosion-inhibiting coating at steel plate arranged outside corrosion-inhibiting coating or steel plate.
For make corrosion-inhibiting coating at high temperature, as not damaging under the high temperature that produces in when welding, the free edge of container halfbody 2,4 12,14 interconnects by stickup.For this reason, the mutual opposed smooth surface at edge 12,14 is provided with Bond in the zone of bonding seam or joint close 18, and passes through the axial pressure mutual extrusion of container halfbody 2,4.Every kind of epoxy resin, thermosol or polyamine fat Bond that is suitable for the jointing material of this purposes, particularly high-intensity suitable collision all is admissible as jointing material as the Bond of single composition or two compositions respectively.The thickness s of the Bond in bonding seam or joint close 18 adjusts as the case may be on request.Be not that container halfbody 2,4 is provided with corrosion-inhibiting coating before bonding, can after bonding, coat this corrosion-inhibiting coating yet.
The salient point of the join domain 6 of container halfbody 2,4 is that its edge 12,14 overlaps in overlap joint zone 16.At this, described edge 12,14 with acute angle with respect in abutting connection with these edges 12,14 zone is crooked, these zones are by cylindrical shell wall 8,10 form, and this edge just extends in overlap joint zone 16 at least in parallel to each other and jointing material is arranged in the bonding seam or joint close 18 between the surface of pointing to toward each other at edge 12,14.Edge 12,14 in overlap joint zone 16 and be preferably located in 2 in abutting connection with the angle α between the zone 8,10 at these edges 12,14 and spend in the scopes of 15 degree particularly preferably is about 8 degree.
This realizes with following method that preferably the smooth edge 12 that is about to one of them container halfbody 2 is outwardly-bent in overlap joint zone 16, and the edge 14 of another container halfbody 4 is extended from cross section with looking into gable shape.The gable shape edge 14 of another container halfbody 4 is formed from axially seeing by smooth section 20 slope shape, that radially outward points to, this smooth section 20 connects smooth section 24 same slope-shaped but that radially inwardly point to surpassing peak 22 backs, and the end of this smooth section 24 is marginal ends 26.In other words, edge 14 is configured to the stiffening rib of radially outward projection.Preferably carry out rounding from the transition portion of the section 20 of shell wall 10 outside pointing to from section 20 to the transition portion that points to interior section 24 with radius R.
The inner diameter d of one of them container halfbody 2 1Basically with the inner diameter d of another container halfbody 4 2Equally big.Simultaneously, the inner diameter d of another container halfbody 4 in free edge acies 26 zones 3Be greater than or equal to the inner diameter d of described container halfbody 2,4 1, d 2Thus, though the edge 12,14 that when having big manufacturing tolerances, also prevents container halfbody 2,4 slide into each other during in axial engagement above and feasiblely 12,14 do not engage along the edge in accordance with regulations.
In of the present invention another kind of embodiment, represent with identical reference character with respect to previous example part identical and same function according to Fig. 2.
With respect to front embodiment different be, for example the edge 14 of the shell wall 10 of another container halfbody 4 be provided with at least one along the container circumference around stiffening rib or groove 28, this stiffening rib or groove are used for holding Sealing 30 to small part, and the sealing part contacts the edge 12 of another container halfbody 2 hermetically.Sealing 30 preferably is made of radial direction seal ring.Be arranged at this stiffening rib or groove 28 and see in the overlap joint zone 16 and from the inner chamber of container 1 and be prepended to bonding seam or joint close 18.Groove or stiffening rib 30 are preferably made by the distortion at edge 14.
Particularly preferably be, other groove or stiffening rib of structure in the edge 14 of the shell wall 10 of another container halfbody 4 for example is so that front and back are arranged a plurality of Sealings 30,36 successively.In pressing the mode of execution of Fig. 2, though other groove or stiffening rib 32 also are arranged in the overlap joint zone 16, see the flex point 34 that is prepended to rounding from the inner chamber of container 1, the edge 12 of one of them container halfbody 2 is with respect to remaining shell wall 8 bendings on this flex point.
According to a kind of replacement scheme, also construct groove or stiffening rib 28 in the edge 12 of a container halfbody 2 therein, 32, alternately constructing a plurality of grooves or stiffening rib 28,32 on the edge 12 of a container halfbody 2 and on the edge 14 of another container halfbody 4 therein under the existing situation in other words.
The Sealing 30,36 of spacing washer that simultaneously also is the edge to be joined 12,14 of container halfbody 2,4 guarantees to keep bonding seam or joint close 18 desirable thickness s.When a plurality of Sealings 30,36 front and back are arranged successively, thereby the edge 12,14 of container halfbody 2,4 can support on a plurality of positions and when Bond can not overturn between hardening period relatively, this function can particularly advantageously be implemented mutually.But for realizing above-mentioned functions, Sealing 30 is 36 just enough basically in other words.
The invention is not restricted to compressed air container 1, but can be used for the container of any kind of, for example be used for the fuel container or the urea container of load-carrying vehicle, wherein also have the described advantage of beginning.

Claims (7)

1. the container in the automobile (1), this container comprises the container halfbody (2 of two cup-shapeds of making by steel plate deformed, 4), the edge (12 that in overlap joint zone (16), overlaps of this container halfbody, 14) interconnect by stickup, wherein said container halfbody (2,4) edge (12,14) with acute angle (α) with respect in abutting connection with this edge (12,14) zone (8,10) bending makes this edge just extend in parallel to each other in overlap joint zone (16) at least, and for bonding seam or the joint close (18) that is arranged between the edge is provided with jointing material
The edge (12) of one of them container halfbody (2) is outwardly-bent in overlap joint zone (16), and the edge (14) of another container halfbody (4) extends internally from cross section with looking into gable shape,
It is characterized in that: in the zone (8,10) of described edge (12,14), the inside dimension (d of one of them container halfbody (2) 1) be substantially equal to the inside dimension (d of another container halfbody (4) 2), and the inside dimension (d in the zone of its free edge acies (26) of described another container halfbody (4) 3) more than or equal to the inside dimension (d of described container halfbody (2,4) in the zone (8,10) at the described edge of adjacency (12,14) 1, d 2).
2. by the described container of claim 1, it is characterized in that: described in overlap joint zone (16) edge (12,14) and be positioned at 2 in abutting connection with the angle (α) between the zone (8,10) of described edge (12,14) and spend to the scope of 15 degree.
3. by claim 1 or 2 described containers, it is characterized in that: described container is the compressed air container (1) in the load-carrying vehicle.
4. by claim 1 or 2 described containers, it is characterized in that: at least one container halfbody (2,4) is provided with erosion-resisting coating.
5. by claim 1 or 2 described containers, it is characterized in that: the edge (14) of at least one container halfbody (4) in overlap joint zone (16), be provided with at least one along the container circumference around stiffening rib or groove (28,32), this stiffening rib or groove are used for holding Sealing (30) to small part, and the sealing part contacts the edge (12) of another one container halfbody (2) hermetically.
6. by the described container of claim 5, it is characterized in that: from the inner chamber of described container (1), described Sealing (30) is prepended to bonding seam or joint close (18).
7. by the described container of claim 5, it is characterized in that: described Sealing (30) is made of at least one radial direction seal ring.
CN2007101023848A 2006-05-05 2007-04-30 Container in automobile Active CN101067471B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006021020A DE102006021020A1 (en) 2006-05-05 2006-05-05 Container in a motor vehicle
DE102006021020.4 2006-05-05

Publications (2)

Publication Number Publication Date
CN101067471A CN101067471A (en) 2007-11-07
CN101067471B true CN101067471B (en) 2011-09-14

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Application Number Title Priority Date Filing Date
CN2007101023848A Active CN101067471B (en) 2006-05-05 2007-04-30 Container in automobile

Country Status (7)

Country Link
EP (1) EP1852647B1 (en)
CN (1) CN101067471B (en)
AT (1) ATE413563T1 (en)
BR (1) BRPI0701687B1 (en)
DE (2) DE102006021020A1 (en)
PL (1) PL1852647T3 (en)
RU (1) RU2426935C2 (en)

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* Cited by examiner, † Cited by third party
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EP2682613B1 (en) * 2011-03-01 2016-12-21 Toyota Jidosha Kabushiki Kaisha Adhesive flange structure
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RU2426935C2 (en) 2011-08-20
ATE413563T1 (en) 2008-11-15
DE502007000214D1 (en) 2008-12-18
PL1852647T3 (en) 2009-04-30
CN101067471A (en) 2007-11-07
DE102006021020A1 (en) 2007-11-08
EP1852647A1 (en) 2007-11-07
EP1852647B1 (en) 2008-11-05
BRPI0701687B1 (en) 2019-11-12
BRPI0701687A (en) 2007-12-26

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