CN202132324U - Transition joint assembly for connecting dissimilar material - Google Patents
Transition joint assembly for connecting dissimilar material Download PDFInfo
- Publication number
- CN202132324U CN202132324U CN2011200400839U CN201120040083U CN202132324U CN 202132324 U CN202132324 U CN 202132324U CN 2011200400839 U CN2011200400839 U CN 2011200400839U CN 201120040083 U CN201120040083 U CN 201120040083U CN 202132324 U CN202132324 U CN 202132324U
- Authority
- CN
- China
- Prior art keywords
- structural element
- flange
- joint assembly
- transit joint
- foreign material
- 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 - Fee Related
Links
- 239000000463 material Substances 0.000 title claims abstract description 47
- 230000007704 transition Effects 0.000 title abstract description 3
- 238000003466 welding Methods 0.000 claims description 34
- 238000001125 extrusion Methods 0.000 claims description 22
- 150000001875 compounds Chemical class 0.000 claims description 5
- 238000007789 sealing Methods 0.000 claims description 3
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 abstract description 4
- 229910052782 aluminium Inorganic materials 0.000 abstract description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 4
- 229910052749 magnesium Inorganic materials 0.000 abstract description 4
- 239000011777 magnesium Substances 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 9
- 229910000831 Steel Inorganic materials 0.000 description 5
- 239000002131 composite material Substances 0.000 description 5
- 239000010959 steel Substances 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 4
- 210000001503 joint Anatomy 0.000 description 4
- 239000004411 aluminium Substances 0.000 description 3
- 239000003795 chemical substances by application Substances 0.000 description 3
- 238000003756 stirring Methods 0.000 description 3
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 230000009977 dual effect Effects 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 230000004927 fusion Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 229910001094 6061 aluminium alloy Inorganic materials 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 238000007778 shielded metal arc welding Methods 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B2/00—Friction-grip releasable fastenings
- F16B2/02—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening
- F16B2/06—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening external, i.e. with contracting action
- F16B2/065—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening external, i.e. with contracting action using screw-thread elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B7/00—Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections
- F16B7/04—Clamping or clipping connections
- F16B7/0433—Clamping or clipping connections for rods or tubes being in parallel relationship
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Connection Of Plates (AREA)
- Arc Welding In General (AREA)
Abstract
The utility model provides a transition joint assembly for connecting dissimilar materials, which comprises a first structural member made of a first material such as aluminum and equipped with a first flange and a second flange; a second structural member made of a second material such as magnesium and equipped with a first flange and a second flange; a third structural member and a fourth structural member. The third structural member and the fourth structural member are made of the first material and are respectively equipped with a first flange and a second flange in contact with the flanges of the first and second structural members. Therefore, the first structural member and the second structural member are locked together through the third structural member and the fourth structural member.
Description
Technical field
The utility model relates to and is used to connect the constitutional detail processed by foreign material and the transit joint assembly of mechanical component.
Background technique
Two problems compatibility that is materials and the applicability that is connected technology that connect foreign material.Especially, when using known connection technology that aluminium is connected in magnesium, is connected in steel or is connected in composite, have problems, these known connection technologies for example are melting welding (for example, shielded metal arc welding) and solid-state welding (for example, friction rabbling welding).These problems comprise: metallurgical incompatibility, this causes weld seam uncontrollable break and/or brittle metal between the formation of compound; The rapid difference of electromotive force, this can cause electro erosion when having salt and/or humidity; And the incompatibility of thermal expansion coefficient, this can cause forming in the joint strong residual stress, thereby causes the inefficacy of under the particular load condition (for example stress corrosion).
The model utility content
The utility model relates to transit joint, and it can be used for being connected with same material but the tratitional technology of the material that can not be connected with foreign material forever connects material different through generally being used to connect those.This new-type transit joint provides more flexibility to the transition design; Therefore each material (for example; Steel and aluminium) can be through more be prone to adapting to the element size tolerance difference, more easy to control and can make joint have the sliding-type joint of excellent mechanical property (for example, fatigue and intensity) and be welded to connect and/or bolt links together.This new-type transit joint also allows to select to make joint and will use the structure of joint to make respectively, also allows to select to be fabricated to sub-component to joint so that follow-up the connection through welding or bolt is attached to one than in the macrostructure.
In one embodiment, the utility model provides a kind of assembly, comprising: by first structural element that first material is processed, said first structural element has flange; By second structural element that second material is processed, said second structural element has flange; The 3rd structural element of processing by said first material; Said the 3rd structural element has first flange and second flange; Wherein, The flange of first structural element contacts first flange of the 3rd structural element, and the flange of second structural element contacts second flange of the 3rd structural element, so that first structural element and second structural element are locked at together; And wherein, first structural element and the 3rd structural element are connected to each other directly.
In another embodiment, the utility model provides a kind of assembly, comprising: by first structural element that first material is processed, said first structural element has first flange and second flange; By second structural element that second material is processed, said second structural element has first flange and second flange; By the 3rd structural element that said first material is processed, said the 3rd structural element has first flange and second flange; By the 4th structural element that said first material is processed, said the 4th structural element has first flange and second flange; Wherein, First flange of first structural element contacts first flange of the 3rd structural element; Second flange of first structural element contacts first flange of the 4th structural element; First flange of second structural element contacts second flange of the 3rd structural element, and second flange of second structural element contacts second flange of the 4th structural element, so that first structural element and second structural element are locked at together; And wherein, first structural element and the 3rd structural element are connected to each other directly, and first structural element and the 4th structural element are connected to each other directly.
The structural element of these assemblies of being processed by same or similar material can be connected to each other directly through the welding procedure of related domain any known, and these welding procedures comprise melting welding, submerged arc welding, laser beam welding or gas metal buried arc welding.In an other embodiment, assembly may further include and makes at least two structural element one or more tackiness agents connected to one another.Assembly also may further include and makes at least two structural element one or more fastening pieces connected to one another, and fastening piece comprises bolt or rivet.
The utility model provides a kind of transit joint assembly that is used to connect foreign material, comprising: by first structural element that first material is processed, said first structural element has first flange and second flange; By second structural element that second material is processed, said second structural element has first flange and second flange; By the 3rd structural element that said first material is processed, said the 3rd structural element has first flange and second flange; By the 4th structural element that said first material is processed, said the 4th structural element has first flange and second flange; It is characterized in that; First flange of first structural element contacts first flange of the 3rd structural element; Second flange of first structural element contacts first flange of the 4th structural element; First flange of second structural element contacts second flange of the 3rd structural element, and second flange of second structural element contacts second flange of the 4th structural element; And wherein; First structural element and the 3rd structural element are connected to each other directly at first flange of the 3rd structural element and the point of contact place between first structural element; And first structural element and the 4th structural element are connected to each other directly at first flange of the 4th structural element and the point of contact place between first structural element, so that first structural element and second structural element are locked at together.
In one embodiment; First flange and the welding of the point of contact place between first structural element through at the 3rd structural element are connected to each other directly first structural element and the 3rd structural element, and through first flange and the welding of the point of contact place between first structural element at the 4th structural element first structural element and the 4th structural element are connected to each other directly.
In one embodiment, first structural element is top latch or " T " shape extrusion.
In one embodiment, from cross section, second structural element is " T " shape.
In one embodiment, the point of contact between first structural element and the 3rd structural element comprises local rotary type joint.
In one embodiment, first and second structural elements contact with each other.
In one embodiment, when cross section was seen assembly, third and fourth structural element conformed to the external frame of first structural element with second structural element basically.
In one embodiment, this assembly also comprises and makes at least two interconnected one or more sealing compounds of structural element or tackiness agent.
In one embodiment, this assembly also comprises and makes at least two interconnected one or more fastening pieces of structural element.
In one embodiment, said one or more fastening piece comprises bolt or rivet.
The utility model also provides the method that is used to assemble transit joint disclosed herein.
After the detailed description of having read the utility model embodiment, the further feature and the advantage of the utility model will be more clear, will only provide with reference to the mode of accompanying drawing with example below the utility model embodiment's detailed description.
Description of drawings
In order the utility model there to be better understanding, referring to the detailed description of considering below in conjunction with accompanying drawing, wherein to embodiment:
Accompanying drawing 1A is the sectional view of a transit joint assembly among the embodiment;
Accompanying drawing 1B is the top perspective sectional view of the transit joint assembly among the accompanying drawing 1A;
Accompanying drawing 2A is the sectional view that includes the transit joint assembly of fastening piece among another embodiment;
Accompanying drawing 2B is the top perspective sectional view of the transit joint assembly among the accompanying drawing 2A;
Accompanying drawing 3 is the sectional views that adopted the transit joint assembly of local rotary type joint among another embodiment;
Accompanying drawing 4A is the sectional view of the transit joint assembly among another embodiment, and this transit joint assembly is through dual the taking on the web that angle joint is welded in beam that be slidingly matched;
Accompanying drawing 4B is the top perspective sectional view of the transit joint assembly among the accompanying drawing 4A;
Accompanying drawing 5A is the sectional view of the transit joint that will intersect with the second transit joint assembly among another embodiment;
Accompanying drawing 5B is the side view of the transit joint assembly among the accompanying drawing 5A;
Accompanying drawing 5C be among the accompanying drawing 5A the transit joint assembly and will with the top perspective sectional view of its second transit joint assembly that intersects;
Accompanying drawing 6A is the side view of the transit joint assembly that intersects each other among another embodiment;
Accompanying drawing 6B is the plan view of the transit joint assembly that intersects each other among the accompanying drawing 6A.
Embodiment
With reference to accompanying drawing 1A and 1B; The utility model one embodiment's transit joint assembly 10 comprises first structural element, second structural element and third and fourth structural element; In the present embodiment, first structural element is top latch or " T " shape extrusion, comprise have flange 18 first material (for example; Steel, magnesium, composite etc.) 12; Second structural element comprises second material 14 with flange 24, and third and fourth structural element is side locking extrusion in the present embodiment, comprises first material 16 with flange 20 and 22.In the present embodiment, see that second structural element has " T " shape from cross section.Structural element 12; 14; 16 can be processed by any material of transit joint that is applicable to, comprise aluminium, T6 state 6061 aluminum alloys, aluminium alloy compound thing, steel, magnesium, based on organic composite (graphite fiber that for example combines) with based on the composite (steel fiber that for example weaves and be glued together) of inorganic matter or similar composite.The flange 20 of side locking extrusion should fully contact with the flange 18 of top latch or " T " shape extrusion and the flange 24 of second structural element with 22; So that make the mechanically interlocking of these structural elements; In case and locking extrusion 16 in side is soldered on top latch or " T " shape extrusion 12, can stop first structural element 12 to separate with second structural element 14.In the present embodiment, from cross section, third and fourth structural element 16 is suitable for matching with the external frame of first structural element 12 and second structural element 14 when coupling together.The flange 20 of side locking extrusion forms butt joint with top latch or " T " shape extrusion 28, and top latch or " T " shape extrusion 28 can be soldered along its length direction.In another embodiment, sealing compound or tackiness agent 26 can place between structural element 12,14 or 16, so that these structural elements mutually combine and/or reduce the wearing and tearing and the corrosion of these structural elements.
With reference to accompanying drawing 2A and 2B; The weld seam 30 of another embodiment's of the utility model transit joint assembly can be obtained by any welding manner well known in the art, for example based on the welding (for example gas metal-arc welding (GMAW), gas tungsten arc welding (GTAW), laser beam welding (LBW), vertical masonry joint submerged arc welding (LSBW) etc.) of fusion mode or based on the welding of solid-state mode (for example friction stir welding (FSW), embed friction welding (FW plunge) etc.).Selectively, not to comprise weld seam 30, said welding method also can be guaranteed that mechanical interlocked unseparated any other between the structural element connects and the technique for fixing replacement by well known in the art.Transit joint can comprise: by the add ons 33 that first material makes, it can be soldered on first structural element 12; And the add ons 36 that makes by second material, it is soldered on second structural element 14.Accompanying drawing 2A and 2B also show the purposes of the optional fastening piece 40 of transit joint, and it can be used for preventing that the flange 22 of side locking extrusion 16 from separating from second structural element 14.
Another embodiment of the utility model is shown in accompanying drawing 3, shows a kind of transit joint, and it has adopted the local swivel coupling 44 between the flange 20 that is positioned at top latch or " T " shape extrusion 14 and side locking extrusion 18.In the present embodiment; The local rotary type joint 44 that employing has radius of curvature can allow to lean against side locking extrusion 18 dresses on the edge 46 of top latch or " T " shape extrusion; So that they can be welded together each other; Simultaneously, when using support anvil when (as during friction stir welding), allowing has reliable point of contact 48 between the flange of conical surface and side locking extrusion of flange of second structural element.Locking extrusion 18 in side also can optionally comprise the lower surface 50 of thickening, to improve and the contacting of support anvil.
Accompanying drawing 4A and 4B show the transit joint assembly 10 of the utility model, and it is through dual the taking on the web 60 that angle joint 62 is welded in beam that be slidingly matched.
Accompanying drawing 5A and 5B show the first transit joint assembly 80 of the utility model, and it will intersect and be connected with the second transit joint assembly.Accompanying drawing 5B is the side view that is shown in the transit joint assembly 80 among the accompanying drawing 5A.In the side locking extrusion 16 of transit joint assembly 80 recess 82 is arranged.
First transit joint assembly that accompanying drawing 5C shows accompanying drawing 5A and 5B and the second transit joint assembly 90 that will intersect and be connected with it.In the side locking extrusion 16 of the second transit joint assembly 90 recess 92 is arranged.Recess 92 mechanically cooperates with recess 82, so that the flange 24 of second structural element 14 of the flange 18 of first structural element 12 of the side locking extrusion 16 of the side of the first transit joint assembly 80 locking extrusion 16 contacts second transit joint assembly 92, the second transit joint assembly 92 and the second transit joint assembly 92.
Accompanying drawing 6A show cooperate fully each other be shown in first and second transit joints 80 and 90 among the accompanying drawing 5C respectively. Transit joint 80 and 90 can be welded to each other at any point of contact place between them.Weld seam can be formed by any welding procedure well known in the art; For example (for example based on the welding of fusion mode; Gas metal-arc welding (GMAW), gas tungsten arc welding (GTAW), laser beam welding (LBW), vertical masonry joint submerged arc welding (LSBW) or the like) or based on the welding of solid-state mode (for example, friction stir welding (FSW), embed friction weldering (FW plunge) etc.).Alternatively, not to comprise weld seam, said welding method also can be connected with any well known in the art other that the first and second transit joint assemblies 80 that can guarantee to intersect and 90 can not separate with technique for fixing and replace.
Accompanying drawing 6B show cooperate fully each other be shown in first and second transit joints 80 and 90 the plan view among the accompanying drawing 5C respectively.Should be understood that first and second transit joints 80 and 90 needn't that kind intersect each other with meeting at right angles shown in accompanying drawing 6A and 6B.
Should be understood that embodiment described here only is exemplary, those skilled in the art can make various variations and the correction that does not break away from the utility model spirit and scope.Therefore, all such variations and correction will be included in and like enclosed within the scope of embodiments described herein that limits in the claim.
Claims (10)
1. transit joint assembly that is used to connect foreign material comprises:
By first structural element that first material is processed, said first structural element has first flange and second flange;
By second structural element that second material is processed, said second structural element has first flange and second flange;
By the 3rd structural element that said first material is processed, said the 3rd structural element has first flange and second flange;
By the 4th structural element that said first material is processed, said the 4th structural element has first flange and second flange;
It is characterized in that; First flange of first structural element contacts first flange of the 3rd structural element; Second flange of first structural element contacts first flange of the 4th structural element; First flange of second structural element contacts second flange of the 3rd structural element, and second flange of second structural element contacts second flange of the 4th structural element; And
Wherein, First structural element and the 3rd structural element are connected to each other directly at first flange of the 3rd structural element and the point of contact place between first structural element; And first structural element and the 4th structural element are connected to each other directly at first flange of the 4th structural element and the point of contact place between first structural element, so that first structural element and second structural element are locked at together.
2. the transit joint assembly that is used to connect foreign material as claimed in claim 1; It is characterized in that; First flange and the welding of the point of contact place between first structural element through at the 3rd structural element are connected to each other directly first structural element and the 3rd structural element, and through first flange and the welding of the point of contact place between first structural element at the 4th structural element first structural element and the 4th structural element are connected to each other directly.
3. the transit joint assembly that is used to connect foreign material as claimed in claim 1 is characterized in that, first structural element is top latch or " T " shape extrusion.
4. the transit joint assembly that is used to connect foreign material as claimed in claim 1 is characterized in that, from cross section, second structural element is " T " shape.
5. the transit joint assembly that is used to connect foreign material as claimed in claim 2 is characterized in that the point of contact between first structural element and the 3rd structural element comprises local rotary type joint.
6. the transit joint assembly that is used to connect foreign material as claimed in claim 1 is characterized in that first and second structural elements contact with each other.
7. the transit joint assembly that is used to connect foreign material as claimed in claim 6 is characterized in that, when cross section was seen assembly, third and fourth structural element conformed to the external frame of first structural element with second structural element basically.
8. the transit joint assembly that is used to connect foreign material as claimed in claim 1 is characterized in that, this assembly also comprises makes at least two interconnected one or more sealing compounds of structural element or tackiness agent.
9. the transit joint assembly that is used to connect foreign material as claimed in claim 1 is characterized in that, this assembly also comprises makes at least two interconnected one or more fastening pieces of structural element.
10. the transit joint assembly that is used to connect foreign material as claimed in claim 9 is characterized in that said one or more fastening pieces comprise bolt or rivet.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/721,376 | 2010-03-10 | ||
| US12/721,376 US20110219719A1 (en) | 2010-03-10 | 2010-03-10 | Transition-joints for joining dissimilar materials |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202132324U true CN202132324U (en) | 2012-02-01 |
Family
ID=43752135
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011200400839U Expired - Fee Related CN202132324U (en) | 2010-03-10 | 2011-01-07 | Transition joint assembly for connecting dissimilar material |
| CN2011100394809A Pending CN102189357A (en) | 2010-03-10 | 2011-01-07 | Transition-joints for joining dissimilar materials |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011100394809A Pending CN102189357A (en) | 2010-03-10 | 2011-01-07 | Transition-joints for joining dissimilar materials |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20110219719A1 (en) |
| CN (2) | CN202132324U (en) |
| WO (1) | WO2011112271A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105984510A (en) * | 2015-03-23 | 2016-10-05 | 福特全球技术公司 | Vehicle body structure |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8341917B2 (en) * | 2009-06-03 | 2013-01-01 | Garland Industries, Inc. | Anchoring system for a roof panel system |
| CA2762860C (en) | 2011-02-18 | 2019-03-12 | Laydon Composites Ltd. | Clamp assembly for mounting panels to i-beams |
| JP5496946B2 (en) * | 2011-05-26 | 2014-05-21 | 三菱重工交通機器エンジニアリング株式会社 | Platform door equipment |
| US9279531B2 (en) | 2012-12-17 | 2016-03-08 | United Technologies Corporation | Composite ducts and methods |
| CN204209275U (en) * | 2013-06-26 | 2015-03-18 | 美铝公司 | A kind of laminar structure |
| CN103647162A (en) * | 2013-12-17 | 2014-03-19 | 西南铝业（集团）有限责任公司 | Wiring lug for large extrusion container and manufacture method thereof |
| CN105889742A (en) * | 2016-05-25 | 2016-08-24 | 福建省南铝板带加工有限公司 | Aluminum profile connecting structure and corner brace for connecting structure |
| US10220888B2 (en) | 2016-10-19 | 2019-03-05 | Laydon Composites Ltd. | Angled clamp assembly for mounting panels to I-beams |
| DE102016223875A1 (en) | 2016-11-30 | 2018-05-30 | Volkswagen Aktiengesellschaft | Method for joining components made of different materials |
| CN111456312A (en) * | 2019-11-22 | 2020-07-28 | 浙江精工钢结构集团有限公司 | Steel-aluminum combined movable roof |
| USD1018270S1 (en) * | 2021-06-07 | 2024-03-19 | Guixia Su | Beam clamp |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2448362A (en) * | 1945-09-26 | 1948-08-31 | Beech Aircraft Corp | Aircraft beam chord construction |
| US3319983A (en) * | 1960-12-27 | 1967-05-16 | Georgia Marble Co | Anchoring system for the installation of slabs on vertical and overhead surfaces |
| US4248025A (en) * | 1979-08-08 | 1981-02-03 | Unarco Industries, Inc. | Knock down pole construction |
| DE3166530D1 (en) * | 1980-01-07 | 1984-11-15 | Masaya Nagashima | Method and means for releasably rigidly fastening together beams and like profiles |
| EP0166035A1 (en) * | 1984-06-21 | 1986-01-02 | Intra-Profiel Staalbouwtechniek B.V. | Rack clamp for securing supporting arms to uprights of cantilever racks |
| US5864998A (en) * | 1989-12-26 | 1999-02-02 | Weston R. Loomer | Modular structural members |
| US6094881A (en) * | 1998-04-30 | 2000-08-01 | Con/Span Bridge Systems Inc. | Box shaped structural member with pultruded flanges and connecting webs |
| US6374570B1 (en) * | 2000-08-25 | 2002-04-23 | Lockheed Martin Corporation | Apparatus and method for joining dissimilar materials to form a structural support member |
| US6598923B2 (en) * | 2000-11-22 | 2003-07-29 | Alcoa Inc. | Joint structure and method for making a joint structure |
| DK1412642T3 (en) * | 2001-08-03 | 2008-02-11 | Norbert Basler | System, clamping element and counter element for connecting profile elements |
| US7115324B1 (en) * | 2003-08-29 | 2006-10-03 | Alcoa Inc. | Method of combining welding and adhesive bonding for joining metal components |
| US7464512B1 (en) * | 2004-03-10 | 2008-12-16 | Perina Mark J | Hollow structural member |
| US7258828B2 (en) * | 2004-09-03 | 2007-08-21 | Lockheed Martin Corporation | Infusion joining of composite structures |
| US20090188206A1 (en) * | 2008-01-24 | 2009-07-30 | Israel Stol | System and method for joining dissimilar materials |
-
2010
- 2010-03-10 US US12/721,376 patent/US20110219719A1/en not_active Abandoned
-
2011
- 2011-01-07 CN CN2011200400839U patent/CN202132324U/en not_active Expired - Fee Related
- 2011-01-07 CN CN2011100394809A patent/CN102189357A/en active Pending
- 2011-01-07 WO PCT/US2011/020450 patent/WO2011112271A1/en active Application Filing
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105984510A (en) * | 2015-03-23 | 2016-10-05 | 福特全球技术公司 | Vehicle body structure |
| CN105984510B (en) * | 2015-03-23 | 2021-05-07 | 福特全球技术公司 | Vehicle body structure |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102189357A (en) | 2011-09-21 |
| US20110219719A1 (en) | 2011-09-15 |
| WO2011112271A1 (en) | 2011-09-15 |
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