CN221022659U - Novel aluminum honeycomb plate - Google Patents
Novel aluminum honeycomb plate Download PDFInfo
- Publication number
- CN221022659U CN221022659U CN202322747342.7U CN202322747342U CN221022659U CN 221022659 U CN221022659 U CN 221022659U CN 202322747342 U CN202322747342 U CN 202322747342U CN 221022659 U CN221022659 U CN 221022659U
- Authority
- CN
- China
- Prior art keywords
- aluminum
- honeycomb
- titanium substrate
- plate
- connecting frame
- 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.)
- Active
Links
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims abstract description 41
- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 40
- -1 aluminum magnesium titanium Chemical compound 0.000 claims abstract description 40
- 239000000758 substrate Substances 0.000 claims abstract description 39
- 230000007246 mechanism Effects 0.000 claims abstract description 33
- 239000011248 coating agent Substances 0.000 claims abstract description 5
- 238000000576 coating method Methods 0.000 claims abstract description 5
- 238000005260 corrosion Methods 0.000 claims abstract description 5
- 239000004411 aluminium Substances 0.000 claims 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 abstract description 13
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 abstract description 13
- 229910052749 magnesium Inorganic materials 0.000 abstract description 13
- 239000011777 magnesium Substances 0.000 abstract description 13
- 229910052719 titanium Inorganic materials 0.000 abstract description 13
- 239000010936 titanium Substances 0.000 abstract description 13
- 239000000463 material Substances 0.000 abstract description 7
- 230000005484 gravity Effects 0.000 abstract description 5
- 238000000034 method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000011825 aerospace material Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000005034 decoration Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Landscapes
- Laminated Bodies (AREA)
Abstract
The utility model discloses a novel aluminum honeycomb plate, which is characterized in that a plate body mechanism comprises an aluminum magnesium titanium substrate, wherein a multilayer structure is fixedly arranged at the inner end of the aluminum magnesium titanium substrate, a clamping groove is fixedly arranged at the inner end of the multilayer structure, a wear-resistant layer is fixedly arranged at the outer end of the aluminum magnesium titanium substrate, an anti-corrosion coating is fixedly arranged at the outer end of the wear-resistant layer, the aluminum magnesium titanium substrate is an aluminum plate manufactured by three elements of aluminum magnesium titanium, wherein magnesium enables the plate to have better flexibility, titanium enables the plate to have better firmness on the basis of higher flexibility, so that the service life of the outer end of the device is longer, meanwhile, the material of the multilayer structure and the aluminum magnesium titanium substrate are the same, and are compressed together through 20 ten thousand tons of gravity, so that the inner end of the device has better firmness when stressed, the deformation probability is reduced, and the aluminum magnesium titanium substrate is of a frame structure, the plate core mechanism is wrapped inside, and the plate core mechanism is protected in all directions.
Description
Technical Field
The utility model relates to the field of aluminum honeycomb plates, in particular to a novel aluminum honeycomb plate.
Background
The aluminum honeycomb plate is a plate made of aluminum metal elements, is mainly suitable for civil buildings, vehicle and ship decorations and the like, is an application of aviation and aerospace materials in the field of civil buildings, is completely finished in modern factories in the processing process, adopts a hot press molding technology, and is characterized in that the expansion and contraction of heat of an aluminum skin and a honeycomb are synchronous due to the high heat conduction value between the aluminum skin and the honeycomb, and the honeycomb aluminum skin is provided with small holes, so that gas in the plate can freely flow, and a slidable mounting buckle system can not cause structural deformation when expanding with heat and contracting with cold;
The existing aluminum honeycomb plate has the problems that the aluminum skin and the honeycomb are not reinforced and protected, after the aluminum honeycomb plate is stressed, the aluminum skin is deformed and cannot protect the internal honeycomb structure, so that the internal honeycomb structure is deformed, the stability of the aluminum honeycomb plate is low, the stress is limited, and therefore, the novel aluminum honeycomb plate is provided.
Disclosure of utility model
In order to overcome the defects of the prior art, the utility model aims to provide a novel aluminum honeycomb plate, wherein an aluminum-magnesium-titanium substrate is an aluminum plate manufactured by three elements of aluminum, magnesium and titanium, wherein magnesium enables the plate to have better flexibility, titanium enables the plate to have good firmness on the basis of higher flexibility, meanwhile, honeycomb pipe fittings are arranged in an array, the whole plate core mechanism forms a honeycomb structure, and through the arrangement of a first connecting frame and a second connecting frame, the honeycomb pipe fittings are kept equidistant, and the change of the distance between the honeycomb pipe fittings during stress is avoided, so that the honeycomb pipe fittings have better traction force in use.
The technical aim of the utility model is realized by the following technical scheme:
The novel aluminum honeycomb panel comprises a panel body mechanism, wherein a panel core mechanism is fixedly assembled in the panel body mechanism.
The plate body mechanism comprises an aluminum magnesium titanium substrate, wherein a multilayer structure is fixedly arranged at the inner end of the aluminum magnesium titanium substrate, a clamping groove is fixedly arranged at the inner end of the multilayer structure, a wear-resistant layer is fixedly assembled at the outer end of the aluminum magnesium titanium substrate, and an anti-corrosion coating is fixedly arranged at the outer end of the aluminum magnesium titanium substrate, which is positioned at the wear-resistant layer.
The aluminum-magnesium-titanium substrate is an aluminum plate manufactured by three elements of aluminum, magnesium and titanium, wherein magnesium enables the plate to have good flexibility, titanium enables the plate to be good and firm on the basis of high flexibility, therefore the service life of the outer end of the device is longer, a wear-resistant layer is added at the outer end, the surface of the wear-resistant layer is uneven, and large-area stressed friction of the surface of the device during use can be avoided.
Further, the plate core mechanism comprises a honeycomb pipe, a first connecting frame is fixedly arranged on the front side and the rear side of the lower portion of the outer end of the honeycomb pipe, and a second connecting frame is fixedly arranged on the left side and the right side of the lower portion of the outer end of the honeycomb pipe.
The honeycomb pipe fittings arranged in an array form a honeycomb structure integrally, and the first connecting frame and the second connecting frame keep equal distance, so that the distance between the honeycomb pipe fittings is prevented from changing when the honeycomb pipe fittings are stressed, and the honeycomb pipe fittings have better traction force in use.
Further, the aluminum-magnesium-titanium substrate is of a frame structure, and the number of layers of the multilayer structure is four.
The material of multilayer structure and aluminium magnesium titanium base plate are the same material, compress together through 20 ten thousand tons of gravity, make the inner of device have better fastness when the atress from this, reduce deformation probability, and aluminium magnesium titanium base plate is frame structure, wraps up board core mechanism in, makes the omnibearing protection of board core mechanism.
Further, the clamping grooves are of annular structures and are distributed on the upper side and the lower side of the inner end of the multilayer structure in an array mode.
The clamping grooves are arranged on the upper side and the lower side of the inner end of the multilayer structure in an array mode, the clamping grooves are matched with the honeycomb pipe fitting, and the clamping grooves are connected through the pouring structure, so that the honeycomb pipe fitting is stably connected with the aluminum-magnesium-titanium substrate, and the bearing capacity of the honeycomb pipe fitting is increased.
Further, the honeycomb pipe fittings are vertically connected through the first connecting frame, and the honeycomb pipe fittings are transversely connected through the second connecting frame.
Further, the honeycomb pipe fittings are distributed in an array manner in the aluminum-magnesium-titanium substrate.
Further, the upper end and the lower end of the honeycomb pipe fitting are matched with the clamping grooves.
Furthermore, the first connecting frame and the second connecting frame are of the same structure, the first connecting frame is symmetrically distributed at the front end and the rear end of the honeycomb pipe fitting, and the second connecting frame is symmetrically distributed at the left end and the right end of the honeycomb pipe fitting.
In summary, the utility model has the following beneficial effects:
1. The aluminum-magnesium-titanium substrate is an aluminum plate manufactured by three elements of aluminum, magnesium and titanium, wherein magnesium enables the plate to have good flexibility, titanium enables the plate to be good and firm on the basis of high flexibility, so that the service life of the outer end of the device is longer, a wear-resistant layer is added at the outer end, the surface of the wear-resistant layer is uneven, and large-area stressed friction of the surface of the device during use can be avoided;
2. The material of the multilayer structure is the same as that of the aluminum-magnesium-titanium substrate, and the multilayer structure and the aluminum-magnesium-titanium substrate are compressed together through 20 ten thousand tons of gravity, so that the inner end of the device has better firmness when being stressed, the deformation probability is reduced, the aluminum-magnesium-titanium substrate is of a frame structure, and the plate core mechanism is wrapped in the frame structure, so that the plate core mechanism is protected in all directions;
3. The clamping grooves are arranged on the upper side and the lower side of the inner end of the multilayer structure in an array mode, the clamping grooves are matched with the honeycomb pipe fitting, and the clamping grooves are connected through a pouring structure, so that the honeycomb pipe fitting is stably connected with the aluminum-magnesium-titanium substrate, and the bearing force of the honeycomb pipe fitting is increased;
4. The honeycomb pipe fittings arranged in an array form a honeycomb structure integrally, and the first connecting frame and the second connecting frame keep equal distance, so that the distance between the honeycomb pipe fittings is prevented from changing when the honeycomb pipe fittings are stressed, and the honeycomb pipe fittings have better traction force in use.
Drawings
Fig. 1 is a schematic perspective view of the present embodiment;
FIG. 2 is a schematic perspective view of a plate core mechanism in the present embodiment;
FIG. 3 is a schematic cross-sectional view of a plate mechanism in the present embodiment;
Fig. 4 is an enlarged schematic view of fig. 3 a in the present embodiment.
In the figure, 1, a plate body mechanism; 101. an aluminum-magnesium-titanium substrate; 102. a multi-layer structure; 103. a clamping groove; 104. a wear-resistant layer; 105. an anti-corrosion coating; 2. a board core mechanism; 201. honeycomb pipe fittings; 202. a first connecting frame; 203. and a second connecting frame.
Detailed Description
The present utility model will be described in further detail with reference to the accompanying drawings.
Wherein like parts are designated by like reference numerals. It should be noted that the words "front", "back", "left", "right", "upper" and "lower" used in the following description refer to directions in the drawings, and the words "bottom" and "top", "inner" and "outer" refer to directions toward or away from, respectively, the geometric center of a particular component.
Referring to fig. 1, a novel aluminum honeycomb panel in a preferred embodiment of the utility model comprises a panel body mechanism 1, wherein a panel core mechanism 2 is fixedly assembled in the panel body mechanism 1.
Referring to fig. 1, the plate body mechanism 1 comprises an aluminum magnesium titanium substrate 101, wherein a multilayer structure 102 is fixedly arranged at the inner end of the aluminum magnesium titanium substrate 101, a clamping groove 103 is fixedly arranged at the inner end of the multilayer structure 102, a wear-resistant layer 104 is fixedly assembled at the outer end of the aluminum magnesium titanium substrate 101, and an anti-corrosion coating 105 is fixedly arranged at the outer end of the wear-resistant layer 104 at the outer end of the aluminum magnesium titanium substrate 101.
The aluminum-magnesium-titanium substrate 101 is an aluminum plate manufactured by three elements of aluminum, magnesium and titanium, wherein magnesium enables the plate to have good flexibility, titanium enables the plate to have good firmness on the basis of high flexibility, therefore the service life of the outer end of the device is longer, the wear-resistant layer 104 is added at the outer end, and the uneven surface of the wear-resistant layer 104 can avoid large-area stressed friction on the surface when the device is used.
The aluminum-magnesium-titanium substrate 101 is a frame structure, and the number of layers of the multilayer structure 102 is four.
The material of the multilayer structure 102 and the aluminum-magnesium-titanium substrate 101 are the same, and are compressed together through 20 ten thousand tons of gravity, so that the inner end of the device has better firmness when being stressed, the deformation probability is reduced, the aluminum-magnesium-titanium substrate 101 is of a frame structure, the plate core mechanism 2 is wrapped in, and the plate core mechanism 2 is protected in all directions.
The clamping grooves 103 are of annular structures, and the clamping grooves 103 are distributed on the upper side and the lower side of the inner end of the multilayer structure 102 in an array mode.
The clamping grooves 103 are arranged on the upper side and the lower side of the inner end of the multilayer structure 102 in an array mode, the clamping grooves 103 are matched with the honeycomb pipe fitting 201, and the clamping grooves 103 are connected with the honeycomb pipe fitting 201 through a pouring structure, so that the honeycomb pipe fitting 201 and the aluminum-magnesium-titanium substrate 101 are stably connected, and the bearing capacity of the honeycomb pipe fitting 201 is increased.
The board core mechanism 2 comprises a honeycomb pipe 201, wherein a first connecting frame 202 is fixedly arranged on the front side and the rear side below the outer end of the honeycomb pipe 201, and a second connecting frame 203 is fixedly arranged on the left side and the right side below the outer end of the honeycomb pipe 201.
The honeycomb pipe fittings 201 are arranged in an array, so that the plate core mechanism 2 integrally forms a honeycomb structure, and the first connecting frame 202 and the second connecting frame 203 are arranged, so that the honeycomb pipe fittings 201 are kept equidistant, the distance between the honeycomb pipe fittings 201 is prevented from changing when stress is applied, and the honeycomb pipe fittings 201 have good traction force in use.
The upper and lower ends of the honeycomb pipe 201 are fitted with the clamping grooves 103.
The first connecting frame 202 and the second connecting frame 203 have the same structure, the first connecting frame 202 is symmetrically distributed at the front end and the rear end of the honeycomb pipe 201, and the second connecting frame 203 is symmetrically distributed at the left end and the right end of the honeycomb pipe 201.
The specific implementation process comprises the following steps: firstly, an aluminum plate made of three elements of aluminum, magnesium and titanium is used as an aluminum plate 101, wherein magnesium enables a plate to have better flexibility, titanium enables the plate to have better firmness on the basis of higher flexibility, therefore, the service life of the outer end of the device is longer, a wear-resistant layer 104 is additionally arranged at the outer end, the surface of the wear-resistant layer 104 is uneven, the large-area stressed friction of the surface of the device can be avoided when the device is used, the material of the multi-layer structure 102 and the aluminum, magnesium and titanium substrate 101 are the same, the materials are compressed together through 20 ten thousand tons of gravity, the inner end of the device has better firmness when being stressed, the deformation probability is reduced, the aluminum, magnesium and titanium substrate 101 is of a frame-type structure, the board core mechanism 2 is wrapped in, and the board core mechanism 2 is protected in all directions.
The clamping grooves 103 are arranged on the upper side and the lower side of the inner end of the multilayer structure 102 in an array mode, the clamping grooves 103 are matched with the honeycomb pipe fitting 201, and the clamping grooves 103 are connected with the honeycomb pipe fitting 201 through a pouring structure, so that the honeycomb pipe fitting 201 and the aluminum-magnesium-titanium substrate 101 are stably connected, and the bearing capacity of the honeycomb pipe fitting 201 is increased.
Finally, the honeycomb pipe fittings 201 are arranged in an array, the plate core mechanism 2 integrally forms a honeycomb structure, and the first connecting frame 202 and the second connecting frame 203 are arranged, so that the honeycomb pipe fittings 201 are kept equidistant, the distance between the honeycomb pipe fittings 201 is prevented from changing when stress is applied, and the honeycomb pipe fittings 201 have good traction force in use.
The foregoing has shown and described the basic principles and main features of the present utility model and the advantages of the present utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present utility model, and various changes and modifications may be made without departing from the spirit and scope of the utility model, which is defined in the appended claims. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (8)
1. The utility model provides a novel aluminium honeycomb panel which characterized in that: comprises a plate body mechanism (1), wherein a plate core mechanism (2) is fixedly assembled in the plate body mechanism (1);
The plate body mechanism (1) comprises an aluminum magnesium titanium substrate (101), wherein a multilayer structure (102) is fixedly arranged at the inner end of the aluminum magnesium titanium substrate (101), a clamping groove (103) is fixedly arranged at the inner end of the multilayer structure (102), a wear-resistant layer (104) is fixedly assembled at the outer end of the aluminum magnesium titanium substrate (101), and an anti-corrosion coating (105) is fixedly arranged at the outer end of the wear-resistant layer (104) at the outer end of the aluminum magnesium titanium substrate (101).
2. The novel aluminum honeycomb panel as recited in claim 1, wherein: the plate core mechanism (2) comprises a honeycomb pipe fitting (201), a first connecting frame (202) is fixedly arranged on the front side and the rear side below the outer end of the honeycomb pipe fitting (201), and a second connecting frame (203) is fixedly arranged on the left side and the right side below the outer end of the honeycomb pipe fitting (201).
3. The novel aluminum honeycomb panel as recited in claim 1, wherein: the aluminum-magnesium-titanium substrate (101) is of a frame structure, and the number of layers of the multilayer structure (102) is four.
4. The novel aluminum honeycomb panel as recited in claim 2, wherein: the clamping grooves (103) are of annular structures, and the clamping grooves (103) are distributed on the upper side and the lower side of the inner end of the multilayer structure (102) in an array mode.
5. The novel aluminum honeycomb panel as recited in claim 2, wherein: the honeycomb pipe fitting (201) is vertically connected through a first connecting frame (202), and the honeycomb pipe fitting (201) is transversely connected through a second connecting frame (203).
6. The novel aluminum honeycomb panel as recited in claim 2, wherein: the honeycomb pipe fittings (201) are distributed in an array mode inside the aluminum-magnesium-titanium substrate (101).
7. The novel aluminum honeycomb panel as recited in claim 2, wherein: the upper end and the lower end of the honeycomb pipe fitting (201) are matched with the clamping groove (103).
8. The novel aluminum honeycomb panel as recited in claim 4, wherein: the first connecting frame (202) and the second connecting frame (203) are of the same structure, the first connecting frame (202) is symmetrically distributed at the front end and the rear end of the honeycomb pipe fitting (201), and the second connecting frame (203) is symmetrically distributed at the left end and the right end of the honeycomb pipe fitting (201).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322747342.7U CN221022659U (en) | 2023-10-12 | 2023-10-12 | Novel aluminum honeycomb plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322747342.7U CN221022659U (en) | 2023-10-12 | 2023-10-12 | Novel aluminum honeycomb plate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221022659U true CN221022659U (en) | 2024-05-28 |
Family
ID=91135186
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322747342.7U Active CN221022659U (en) | 2023-10-12 | 2023-10-12 | Novel aluminum honeycomb plate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221022659U (en) |
-
2023
- 2023-10-12 CN CN202322747342.7U patent/CN221022659U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110181227B (en) | Method for preparing aluminum/magnesium/aluminum composite board by three-dimensional layer interface | |
| US10239141B2 (en) | Forming a complexly curved metallic sandwich panel | |
| CN104767035A (en) | High-precision carbon fiber auxiliary reflection face forming method | |
| CN221022659U (en) | Novel aluminum honeycomb plate | |
| CN202944564U (en) | Connecting structure for pelvic fin and control cabin | |
| CN112659674A (en) | Lattice topological structure with channel, preparation method of lattice topological structure and cabin section wall plate | |
| CN210115326U (en) | Acid-washing-resistant hot-rolling rubber roller | |
| CN110744872A (en) | Composite material honeycomb sandwich structure and foaming glue filling method used in same | |
| CN103753132B (en) | There is the part preparation method of Ti/TixAly/Ti sandwich construction | |
| CN211616836U (en) | Heat-insulating board | |
| CN214983806U (en) | Fireproof aluminum honeycomb panel | |
| CN212380484U (en) | End plate structure of lightweight battery module | |
| CN209837460U (en) | Composite structure wallboard | |
| CN202079854U (en) | Composite sandwich panel | |
| CN215152629U (en) | Honeycomb panel for building with anti-disengaging structure | |
| CN215858777U (en) | Section bar for 5mm aluminum honeycomb panel fast-assembling flush joint connecting wire | |
| CN214688315U (en) | Non-glue aluminum honeycomb plate | |
| CN221097944U (en) | High-strength compression-resistant aluminum profile | |
| CN215167485U (en) | Anti-betat honeycomb corrosion-resistant plate | |
| CN216993312U (en) | Aluminum honeycomb panel capable of prolonging service life | |
| CN110374257B (en) | Sound-proof and heat-insulation metal composite plate structure | |
| CN215970445U (en) | Composite type nano heat-insulating plate with multiple effects | |
| CN219773426U (en) | Indoor heating building material | |
| CN218205372U (en) | High-performance pre-stretched aluminum plate with heat-insulation interlayer | |
| CN212684892U (en) | Corrosion-resistant high resistant aluminium honeycomb structure of waiting |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |