CN104759799A - Engineering packing box bottom board set assembling and welding method - Google Patents
Engineering packing box bottom board set assembling and welding method Download PDFInfo
- Publication number
- CN104759799A CN104759799A CN201510213963.4A CN201510213963A CN104759799A CN 104759799 A CN104759799 A CN 104759799A CN 201510213963 A CN201510213963 A CN 201510213963A CN 104759799 A CN104759799 A CN 104759799A
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- Prior art keywords
- welding
- reinforcement
- longeron
- welding method
- cargo floor
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- 238000003466 welding Methods 0.000 title claims abstract description 58
- 238000000034 method Methods 0.000 title claims abstract description 30
- 238000012856 packing Methods 0.000 title abstract 4
- 238000009434 installation Methods 0.000 claims abstract description 7
- 230000002787 reinforcement Effects 0.000 claims description 37
- 239000007787 solid Substances 0.000 claims description 10
- 229910000679 solder Inorganic materials 0.000 claims description 7
- 230000003014 reinforcing effect Effects 0.000 abstract 1
- 230000008646 thermal stress Effects 0.000 abstract 1
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K37/00—Auxiliary devices or processes, not specially adapted for a procedure covered by only one of the other main groups of this subclass
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- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Butt Welding And Welding Of Specific Article (AREA)
Abstract
The invention discloses an engineering packing box bottom board set assembling and welding method. The engineering packing box bottom board set assembling and welding method comprises the first step of combination of a frame, the second step of installation of longitudinal beams, the third step of arrangement of reinforcing bars, the fourth step of arrangement of a bottom board, and the fifth step of installation of accessories. The conventional assembly sequence of a packing box bottom board set is changed, and therefore the purposes of creating the space, improving the welding operation environment and then improving the welding quality are achieved. The more effective welding process method is provided, the welding intensity is further ensured, partial concentration of welding thermal stress is effectively prevented, welding deformation is reduced, and the deformation resistance of the whole is improved.
Description
Technical field
The present invention relates to engineering cargo vehicle and manufacture field, be specifically related to a kind of engineering cargo floor general assembly and welding method.
Background technology
Engineering cargo vehicle cargo floor assembly by frame, base plate, longeron, reinforcement and annex four major part form.At present, assembling and the welding method of general engineering cargo vehicle cargo floor assembly are: combination frame → placement base plate → lay longeron → layout reinforcement → pad site weldering → conventional monolithic welding → installation accessories.The processing method of above-mentioned assembling and welding, welding quality not easily ensures, reliability of technology is poor, yielding.And blocking because of base plate during integral solder, make to weld narrow space, easily cause weld defect, especially two-sided welding cannot be implemented to the connecting portion of reinforcement and frame and longeron, affect weld strength, thus Strength Failure cracks in cargo floor lifting operation process, a large amount of welded stress of side are assembled simultaneously, make overall non-deformability poor.
Summary of the invention
Instant invention overcomes the deficiencies in the prior art, engineering cargo floor general assembly and welding method be provided, thus expect to improve cargo floor assembly manufacture craft reliability, improve lifting load-bearing ability, ensure that the structural strength of engineering cargo floor from technique.
For solving above-mentioned technical problem, the present invention by the following technical solutions:
A kind of engineering cargo floor general assembly and welding method, described method comprises the following steps:
The first step, combination frame;
Second step, lays longeron;
3rd step, arranges reinforcement;
4th step, places base plate;
5th step, installation accessories.
Further technical scheme, when laying longeron and layout reinforcement, places gap according to the pre-Cincinnati of base plate thickness.
The solid welding of pad site is implemented fixed when further technical scheme is combination frame.
Further technical scheme implements the solid welding of pad site when laying longeron to determine; The solid welding of pad site is implemented fixed during described layout reinforcement.
Further technical scheme carries out integral solder according to following steps after being layout reinforcement:
A. implement longeron termination to weld with the pad position of bezel contact position;
B. implement reinforcement termination to weld with the pad position of longeron contact position;
C. implement reinforcement termination to weld with the pad position of bezel contact position.
Further technical scheme is step a is implement each longeron two terminations to weld with the pad position of bezel contact position simultaneously.
Further technical scheme is step b is implement reinforcement termination to weld with the pad position of two face contact positions of a longeron with each longeron contact position and reinforcement termination simultaneously.
Further technical scheme is step c is implement reinforcement termination to weld with the pad position of two limit contact positions of frame simultaneously.
Further technical scheme carries out integral solder after being layout reinforcement is two-sided welding, and each welding sequence of described two-sided welding is identical.
Further technical scheme is placement base plate is fill in base plate by sectionally assembled or full slice system.
Compared with prior art, the invention has the beneficial effects as follows: the present invention, by changing the conventional assemble sequence of cargo floor assembly, reaches space for the creativity, improves welding operation environment, and then improve the object of welding quality.The present invention proposes more efficiently welding technique, further ensures the intensity of welding, effectively prevents the concentration of local of welded stress, reduces welding distortion itself, improves overall non-deformability.
Accompanying drawing explanation
Fig. 1 is the assemble sequence schematic diagram of one embodiment of the invention.
Fig. 2 is welding post sequential schematic in one embodiment of the invention.
Detailed description of the invention
All features disclosed in this description, or the step in disclosed all methods or process, except mutually exclusive feature and/or step, all can combine by any way.
Arbitrary feature disclosed in this description (comprising any accessory claim, summary and accompanying drawing), unless specifically stated otherwise, all can be replaced by other equivalences or the alternative features with similar object.That is, unless specifically stated otherwise, each feature is an example in a series of equivalence or similar characteristics.
Below in conjunction with drawings and Examples, the specific embodiment of the present invention is described in detail.
As shown in Figure 1 and Figure 2, according to one embodiment of present invention, the present embodiment discloses a kind of engineering cargo floor general assembly and welding method, the present embodiment is by changing the conventional assemble sequence of cargo floor assembly, reach space for the creativity, improve welding operation environment, and then improve the object of welding quality.Concrete, as shown in Figure 1, the present embodiment engineering cargo floor general assembly and welding method are under assembled tool specification, and lorry engineering cargo floor assembly drops into assembling, the first step successively by the order of 1 ~ 5, combination frame 1; Second step, lays longeron 2; 3rd step, arranges reinforcement 3; 4th step, places base plate 4; 5th step, installation accessories 5.
Wherein, preferably, reserve base plate when laying longeron 2 and arrange reinforcement 3 according to base plate thickness in the present embodiment and place gap.
In the first step, second step, it is fixed that the 3rd step three step implements the solid welding of pad site respectively.Concrete, when self-indulgent beam and layout reinforcement, place gap according to the pre-Cincinnati of base plate thickness.The solid welding of pad site is implemented fixed during combination frame.The solid welding of pad site is implemented fixed when laying longeron; The solid welding of pad site is implemented fixed during described layout reinforcement.
Further preferred embodiment, as shown in Figure 2, in the present embodiment on jig, implement integral solder to the assembly after 1,2,3 step combinations by a → b → c position order, wherein, aa, bb, cc position is double welds simultaneously.
Concrete, after layout reinforcement, carry out integral solder according to following steps in the present embodiment:
A. implement longeron termination to weld with the pad position of bezel contact position;
B. implement reinforcement termination to weld with the pad position of longeron contact position;
C. implement reinforcement termination to weld with the pad position of bezel contact position.
Preferably, as a and a position welding in Fig. 2, be and implement each longeron two terminations simultaneously and weld with the pad position of bezel contact position.When there being two longerons, two longeron terminations that the two ends of two longerons have altogether are welded with corresponding bezel contact position simultaneously.
As b and b position welding in Fig. 2, be enforcement reinforcement termination simultaneously and weld with the pad position of two face contact positions of a longeron with each longeron contact position and reinforcement termination.As having two longerons, the contact site, reinforcement termination that the reinforcement termination contact site corresponding with it, the two sides of one of them longeron is corresponding with it with the two sides of another longeron welds simultaneously.
As c and c position welding in Fig. 2, be enforcement reinforcement termination simultaneously and weld with the pad position of two limit contact positions of frame.As seen from Figure 2, wherein these two limits of frame are two symmetrical limits, and it is parallel with longeron.
After the assembly be assembled into frame, longeron and reinforcement face has been welded, upset assembly, has welded another side by abovementioned steps, mode, has realized the two-sided welding of reinforcement termination and frame and longeron.
As preferred embodiment, the present embodiment, when placing base plate, can adopt and sectionally assembledly fill in base plate, full slice system also can be adopted to fill in base, fill in base plate and adjust equal postpone, weld in the usual way.Weld as installation accessories such as mud guard bearing, profile lamp socket, rope hooks on request again.Thus can improve cargo floor assembly manufacture craft reliability, improve lifting load-bearing ability, ensure that the structural strength of engineering cargo floor from technique.
Spoken of in this manual " embodiment ", " another embodiment ", " embodiment ", etc., refer to the specific features, structure or the feature that describe in conjunction with this embodiment and be included at least one embodiment of the application's generality description.Multiple place occurs that statement of the same race is not necessarily refer to same embodiment in the description.Furthermore, when describing specific features, structure or a feature in conjunction with any one embodiment, what advocate is also fall within the scope of the invention to realize this feature, structure or feature in conjunction with other embodiments.
Although with reference to the multiple explanatory embodiment of inventing, invention has been described here, but, should be appreciated that, those skilled in the art can design a lot of other amendment and embodiment, these amendments and embodiment will drop within spirit disclosed in the present application and spirit.More particularly, in the scope of the open claim of the application, multiple modification and improvement can be carried out to the building block of subject combination layout and/or layout.Except the modification of carrying out building block and/or layout is with except improvement, to those skilled in the art, other purposes also will be obvious.
Claims (10)
1. engineering cargo floor general assembly and a welding method, is characterized in that: described method comprises the following steps:
The first step, combination frame;
Second step, lays longeron;
3rd step, arranges reinforcement;
4th step, places base plate;
5th step, installation accessories.
2. engineering cargo floor general assembly according to claim 1 and welding method, is characterized in that described when laying longeron and arrange reinforcement, places gap according to the pre-Cincinnati of base plate thickness.
3. engineering cargo floor general assembly according to claim 1 and welding method, implements the solid welding of pad site when it is characterized in that described combination frame fixed.
4. engineering cargo floor general assembly according to claim 1 and welding method, is characterized in that described to implement the solid welding of pad site when laying longeron fixed; The solid welding of pad site is implemented fixed during described layout reinforcement.
5. engineering cargo floor general assembly according to claim 1 and welding method, carry out integral solder according to following steps after it is characterized in that described layout reinforcement:
A. implement longeron termination to weld with the pad position of bezel contact position;
B. implement reinforcement termination to weld with the pad position of longeron contact position;
C. implement reinforcement termination to weld with the pad position of bezel contact position.
6. engineering cargo floor general assembly according to claim 5 and welding method, is characterized in that simultaneously described steps A implements each longeron two terminations to weld with the pad position of bezel contact position.
7. engineering cargo floor general assembly according to claim 5 and welding method, is characterized in that described step B implements reinforcement termination to weld with the pad position of two face contact positions of a longeron with each longeron contact position and reinforcement termination simultaneously.
8. engineering cargo floor general assembly according to claim 5 and welding method, is characterized in that described step C implements reinforcement termination to weld with the pad position of two limit contact positions of frame simultaneously.
9. engineering cargo floor general assembly according to claim 5 and welding method, carrying out integral solder after it is characterized in that described layout reinforcement is two-sided welding, and each welding sequence of described two-sided welding is identical.
10. engineering cargo floor general assembly according to claim 1 and welding method, is characterized in that described placement base plate fills in base plate by sectionally assembled or full slice system.
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CN201510213963.4A CN104759799B (en) | 2015-04-29 | 2015-04-29 | Engineering cargo floor general assembly and welding method |
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CN104759799B CN104759799B (en) | 2016-06-29 |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105345322A (en) * | 2015-11-20 | 2016-02-24 | 辽宁忠旺特种车辆制造有限公司 | Welding technology of lateral board of full-loading van |
CN107248556A (en) * | 2017-06-30 | 2017-10-13 | 苏州凯富精密模具有限公司 | A kind of electric automobile battery pack production technology |
CN113828992A (en) * | 2021-10-11 | 2021-12-24 | 安徽工程大学 | Double-shaft-head tail type automatic welding positioner and workpiece welding method |
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CN201672643U (en) * | 2010-05-24 | 2010-12-15 | 刘玉岭 | Combined non-cold-bridge sealing box |
US20110298245A1 (en) * | 2010-06-08 | 2011-12-08 | Ford Global Technologies, Llc | Reduced height pickup truck bed support and method of manufacturing |
CN202279020U (en) * | 2011-05-31 | 2012-06-20 | 三河市新宏昌专用车有限公司 | Self-unloading vehicle container bottom plate structure |
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2015
- 2015-04-29 CN CN201510213963.4A patent/CN104759799B/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201672643U (en) * | 2010-05-24 | 2010-12-15 | 刘玉岭 | Combined non-cold-bridge sealing box |
US20110298245A1 (en) * | 2010-06-08 | 2011-12-08 | Ford Global Technologies, Llc | Reduced height pickup truck bed support and method of manufacturing |
CN202279020U (en) * | 2011-05-31 | 2012-06-20 | 三河市新宏昌专用车有限公司 | Self-unloading vehicle container bottom plate structure |
Non-Patent Citations (2)
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105345322A (en) * | 2015-11-20 | 2016-02-24 | 辽宁忠旺特种车辆制造有限公司 | Welding technology of lateral board of full-loading van |
CN107248556A (en) * | 2017-06-30 | 2017-10-13 | 苏州凯富精密模具有限公司 | A kind of electric automobile battery pack production technology |
CN107248556B (en) * | 2017-06-30 | 2020-10-30 | 苏州凯富精密模具有限公司 | Production process of battery box of electric vehicle |
CN113828992A (en) * | 2021-10-11 | 2021-12-24 | 安徽工程大学 | Double-shaft-head tail type automatic welding positioner and workpiece welding method |
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CN104759799B (en) | 2016-06-29 |
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