CN106827713A - A kind of ripple square tube core body sandwich and preparation method thereof - Google Patents
A kind of ripple square tube core body sandwich and preparation method thereof Download PDFInfo
- Publication number
- CN106827713A CN106827713A CN201710042624.3A CN201710042624A CN106827713A CN 106827713 A CN106827713 A CN 106827713A CN 201710042624 A CN201710042624 A CN 201710042624A CN 106827713 A CN106827713 A CN 106827713A
- Authority
- CN
- China
- Prior art keywords
- square tube
- core body
- ripple
- tube core
- ripple square
- 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.)
- Granted
Links
- 238000002360 preparation method Methods 0.000 title claims abstract description 13
- 238000005520 cutting process Methods 0.000 claims abstract description 9
- 238000005452 bending Methods 0.000 claims description 7
- 238000005219 brazing Methods 0.000 claims description 6
- 238000004140 cleaning Methods 0.000 claims description 6
- 238000010583 slow cooling Methods 0.000 claims description 6
- 229910000838 Al alloy Inorganic materials 0.000 claims description 5
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 5
- 239000000956 alloy Substances 0.000 claims description 3
- 239000010935 stainless steel Substances 0.000 claims description 3
- 229910001220 stainless steel Inorganic materials 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 2
- 238000005516 engineering process Methods 0.000 abstract description 9
- 238000012546 transfer Methods 0.000 abstract description 5
- 238000010276 construction Methods 0.000 abstract description 4
- 238000012545 processing Methods 0.000 abstract description 3
- 230000002708 enhancing effect Effects 0.000 abstract description 2
- 230000007704 transition Effects 0.000 abstract 1
- 239000011162 core material Substances 0.000 description 49
- 239000000463 material Substances 0.000 description 7
- 238000001035 drying Methods 0.000 description 5
- 238000005476 soldering Methods 0.000 description 5
- 238000009413 insulation Methods 0.000 description 4
- 238000003466 welding Methods 0.000 description 4
- 230000033228 biological regulation Effects 0.000 description 3
- 239000002131 composite material Substances 0.000 description 3
- 239000010963 304 stainless steel Substances 0.000 description 2
- 229910000589 SAE 304 stainless steel Inorganic materials 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 239000006261 foam material Substances 0.000 description 2
- 239000011229 interlayer Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 229910000679 solder Inorganic materials 0.000 description 2
- 239000004411 aluminium Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000006071 cream Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 230000035800 maturation Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/18—Layered products comprising a layer of metal comprising iron or steel
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/18—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by an internal layer formed of separate pieces of material which are juxtaposed side-by-side
- B32B3/20—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by an internal layer formed of separate pieces of material which are juxtaposed side-by-side of hollow pieces, e.g. tubes; of pieces with channels or cavities
Landscapes
- Laminated Bodies (AREA)
Abstract
The invention discloses a kind of ripple square tube core body sandwich and preparation method thereof.The present invention relates to sandwich technical field.The ripple square tube core body sandwich is made up of top panel, ripple square tube core body and lower panel.The present invention replaces straight square tube core body with ripple square tube core body, the structure is that the mechanical characteristics such as its specific strength, specific stiffness are further improved on the basis of straight tube core, and make it be leading passage flowing coefficient of heat conduction enhancing more than 50% in transition flow, simultaneously because square tube type core body can need to be designed with the contact area of upper and lower panel according to cutting performance, special jig need not be processed on core body, so as to simplify processing technology.Structure of the invention has high specific strength, high specific stiffness and excellent thermal conduction characteristic, has wide application prospect in space flight and aviation, ship, automobile, machinery and field of civil engineering, is especially had a extensive future in the load-carrying construction required with heat transfer.
Description
【Technical field】
The invention belongs to technical field of composite materials, and in particular to a kind of ripple square tube core body sandwich and its preparation side
Method, particularly a kind of composite with multi-functional characteristic.
【Background technology】
Ultra light porous metal material is in the last few years as prepared by material and mechanical manufacturing technology is developed rapidly
An existing class Multifunction material.This kind of material has high porosity, and its corresponding micro-structural can be divided into unordered by regular degree
With orderly two major class, the former includes closed-cell foam material and open-cell foam materials, and the latter includes two-dimensional lattice material (such as ripple
Structure, honeycomb etc.) and three-dimensional truss structure (such as pyramid structure, X-type structure).
In recent years, the light dot matrix structure with multi-functional characteristic is applied to engineering design increasingly by engineering circles
Favor, such as heat-conductive characteristic, shock resistance, detonation energy.For in the research of the lattice structure capability of antidetonance, Fu Jini
Sub- university Wadley professors team proposes a kind of to be horizontally staggered the straight square tube of arrangement as the sandwich of core body, structure tool
The characteristics of having preparation process is simple, but because rhs-structure tube wall is susceptible to Euler's buckling, cause its load-carrying properties and energy-absorbing
It is less efficient.Based on above reason, on the basis of Nogata tubular construction, the present invention replaces straight square tube using ripple square tube, both may be used
The characteristics of succession straight tube structure prepares simple, can improve its load-carrying properties and energy absorbing efficiency, while can further strengthen the knot again
The heat transfer property of structure.
【The content of the invention】
The technical problems to be solved by the invention are to be directed to above-mentioned deficiency of the prior art, there is provided one kind has mechanics concurrently
The multifunctional composite of load-carrying properties (specific strength, specific stiffness, than energy-absorbing) and heat management function.Replace by with ripple square tube
Straight square tube and obtain the ripple square tube core body sandwich with multi-functional characteristic.
The present invention uses following technical scheme：
A kind of ripple square tube core body sandwich, including top panel and lower panel, set between the top panel and lower panel
Ripple square tube core body is equipped with, the wavy channel core body is arranged parallel to each other by multiple hollow ripple square tubes and constituted.
Further, the bellows-shaped of the ripple square tube is sine bellows.
Further, the top panel is different with the thickness of lower panel.
Further, the top panel, lower panel and ripple square tube are by stainless steel, aluminium alloy or titanium alloy material
Any one is made.
A kind of preparation method of ripple square tube core body sandwich, comprises the following steps：
S1, straight square tube bending is made ripple square tube by sine bellows；
S2, by the plate cutting of smooth mistake into top panel and lower panel；
S3, the cleaning top panel, lower panel and ripple square tube, are put into dry for standby in dryer；
S4, be parallel to each other multiple ripple square tubes the corrugated square tube core body of assembling, and fixation is standby；
S5, ripple square tube core body described in step S4 is connected with top panel, lower panel described in step S3 it is made ripple square tube
Core body sandwich.
Further, in step S1, the ripple Box Section is square section or rectangular cross-sectional.
Further, in step S4, the ripple square tube is ripple square tube core body by 1~2 times of tube wall spacing assembled parallel.
Further, in step S4, phase difference is 0 °~180 ° between the adjacent ripple square tube.
Further, in the step S5, vacuum 10-2~10-3Pa is kept, is risen to from room temperature with 1 DEG C/min speed
550~1200 DEG C, the top panel, ripple square tube core body and lower panel are made by the ripple square tube core body using high temperature brazing
Sandwich, is incubated 10min~60min, slow cooling to room temperature.
Compared with prior art, the present invention at least has the advantages that：
The present invention provides a kind of ripple square tube core body sandwich, is made up of top panel, ripple square tube core body and lower panel,
Straight square tube is replaced by using ripple square tube and the ripple square tube core body sandwich with multi-functional characteristic is obtained, makes it in mistake
It is leading passage flowing coefficient of heat conduction enhancing more than 50% to cross stream, and the structure is further carried on the basis of Nogata tubular construction
High specific strength, specific stiffness and compare energy absorption characteristics.
Further, sine bellows square tube can be improved while the flowing heat transfer characteristic of ripple square tube core body is improved
The resistance to compression stability of sandwich.
Further, certain special occasions, such as shock resistance or antiknock situation, using upper and lower panel not uniform thickness design are being considered
The mechanical characteristic of ripple square tube core body sandwich can further be improved.
The present invention also provides a kind of ripple square tube core body sandwich preparation method, by sine bellows by straight square tube bending system
Corrugated square tube, by plate, lower panel and ripple square tube above cutting by after drying and processing, according to a determining deviation and phase difference
Connection is made sandwich, replaces straight square tube by using ripple square tube and obtains the ripple square tube core body with multi-functional characteristic
Sandwich, because square tube type core body can need to be designed with the contact area of upper and lower panel according to cutting performance, it is not necessary to
Special jig is processed on core body, so as to simplify processing technology, the structure is further on the basis of Nogata tubular construction
Improve specific strength, specific stiffness and compare energy absorption characteristics.
Further, the flow regime of different fluid can be controlled by changing ripple lath phase difference, is optimal stream
Dynamic heat transfer coefficient, wavy channel core body relative density can be changed by adjusting ripple square tube spacing, and structure is improved to greatest extent
Mechanical property.
Further, the present invention carries out the welding of upper and lower panel and core body, the method operation letter using Vacuum Soldering Technology
Just, technology maturation, panel is high with core body bonding strength.
In sum, structure of the invention has high specific strength, high specific stiffness and excellent thermal conduction characteristic, in space flight boat
Sky, ship, automobile, machinery and field of civil engineering have wide application prospect, especially in the load knot required with heat transfer
Had a extensive future in structure.
Below by drawings and Examples, technical scheme is described in further detail.
【Brief description of the drawings】
Fig. 1 is the structural representation of ripple square tube core body sandwich of the present invention；
Fig. 2 is ripple rhs-structure schematic diagram of the present invention.
Wherein：1. top panel；2. ripple square tube；3. ripple square tube core body；4. lower panel.
【Specific embodiment】
In the description of the invention, it is necessary to illustrate, unless otherwise clearly defined and limited, term " installation ", " phase
Company ", " connection " should be interpreted broadly, for example, it may be being fixedly connected, or being detachably connected, or be integrally connected；Can
Being to mechanically connect, or electrically connect；Can be joined directly together, it is also possible to be indirectly connected to by intermediary, Ke Yishi
Two connections of element internal.For the ordinary skill in the art, with concrete condition above-mentioned term can be understood at this
Concrete meaning in invention.
Refer to shown in Fig. 1 and Fig. 2, the invention discloses a kind of ripple square tube core body sandwich, including the He of top panel 1
Lower panel 4, is provided with ripple square tube core body 3 between the top panel 1 and lower panel 4, the wavy channel core body 3 is by multiple ripples
Line square tube 2 is parallel to each other composition.
Wherein, the bellows-shaped of the ripple square tube is sine bellows, the thickness of top panel 1 and lower panel 4 can with identical,
Can also differ, preferred thickness is different.Top panel 1, lower panel 4 and ripple square tube 2 are by stainless steel, aluminium alloy or titanium alloy material
Material is made.
Invention additionally discloses a kind of ripple square tube core body sandwich preparation method, comprise the following steps：
S1, straight square tube bending is made ripple square tube by sine bellows；
The ripple Box Section is square section or rectangular cross-sectional；
S2, by the plate cutting of smooth mistake into top panel and lower panel；
S3, the cleaning top panel, lower panel and ripple square tube, are put into dry for standby in dryer；
S4, be parallel to each other multiple ripple square tubes the corrugated square tube core body of assembling, and fixation is standby；
The ripple square tube is ripple square tube core body by 1~2 times of tube wall spacing assembled parallel；Between the adjacent ripple square tube
Phase difference is 0 °~180 °；
S5, ripple square tube core body described in step S4 is connected with top panel, lower panel described in step S3 it is made ripple square tube
Core body sandwich.
Keep vacuum 10-2~10-3Pa, rises to 550~1200 DEG C, using high temperature brazing with 1 DEG C/min speed from room temperature
The top panel, ripple square tube core body and lower panel are made the ripple square tube core body sandwich, insulation 10min~
60min, slow cooling to room temperature.
Embodiment one：
1) 1060 aluminium alloy straight square tubes are made sine bellows square tube by regulation requirement first by bending machine；
2) 1060 aluminum alloy plate materials of smooth mistake are cut into top panel and lower panel using line cutting technology；
3) go to degrease and rusty stain after cleaning top panel, lower panel and ripple square tube, be put into dry for standby in dryer；
4) ripple square tube is assembled to be formed ripple square tube core body in parallel to each other by 1 times of tube wall spacing and 90 ° of phase differences, and
Fix standby with frock；
5) by uniform commercially available aluminium soldering cream at ripple square tube core body and upper and lower panel binding site, in an oven 40~50
DEG C drying, be then charged into being welded in high temperature brazing stove, slow cooling to room temperature is come out of the stove and obtains ripple square tube core body after the completion of welding
Sandwich plate.
The soldering：Vacuum degree control is 10-3Pa, 550~620 DEG C of insulation 10min are risen to 1 DEG C/min speed from room temperature
~1h.
Embodiment two：
1) TC4 titanium alloys straight square tube is made semicircle ripple square tube by regulation requirement first by bending machine；
2) the TC4 titanium alloy plates of smooth mistake are cut into top panel and lower panel using line cutting technology；
3) go to degrease and rusty stain after cleaning top panel, lower panel and ripple square tube, be put into dry for standby in dryer；
4) ripple square tube is assembled to be formed ripple square tube core body in parallel to each other by 2 times of tube wall spacing and 180 ° of phase differences,
And fix standby with frock；
5) by the face uniform application Ag base solder pastes that ripple square tube core body is parallel with top panel and lower panel, in an oven
80 DEG C of drying, are then charged into being welded in high temperature brazing stove, and slow cooling to room temperature is come out of the stove and obtains ripple square tube core after the completion of welding
Interlayer body plate.
The soldering：Vacuum degree control is 10-2More than Pa, 830-900 DEG C of insulation is risen to 1 DEG C/min speed from room temperature
10min, then furnace cooling.
Embodiment three：
1) 304 stainless steel straight square tubes are made semicircle ripple square tube by regulation requirement first by bending machine；
2) 304 stainless steel materials of smooth mistake are cut into top panel and lower panel using line cutting technology；
3) go to degrease and rusty stain after cleaning top panel, lower panel and ripple square tube, be put into dry for standby in dryer；
4) ripple square tube is assembled to be formed ripple square tube core body in parallel to each other by 2 times of tube wall spacing and 180 ° of phase differences,
And fix standby with frock；
5) by the face uniform application Ni-Zr-P solder pastes that ripple square tube core body is parallel with top panel and lower panel, drying
80 DEG C of drying, are then charged into being welded in high temperature brazing stove in case, and slow cooling is come out of the stove to room temperature and obtains ripple side after the completion of welding
Tube core interlayer body plate.
The soldering：Vacuum degree control is 10-3More than Pa, 1000-1200 DEG C of insulation is risen to 1 DEG C/min speed from room temperature
1 hour, then furnace cooling.
Be according to thin plate stable theory, the characteristics of ripple rhs-structure by straight tube compression while be divided into many it is sub- while, each
Sub- side is constrained by the prism of stabilization, the stability of thin plate is greatly strengthen, so as to improve the utilization rate of core material.Based on
Upper theory, the relatively straight tube core body of ripple rhs-structure has stronger specific strength.
Above content is only explanation technological thought of the invention, it is impossible to limit protection scope of the present invention with this, every to press
According to technological thought proposed by the present invention, any change done on the basis of technical scheme each falls within claims of the present invention
Protection domain within.
Claims (9)
1. a kind of ripple square tube core body sandwich, it is characterised in that：Including top panel (1) and lower panel (4), the top panel
(1) ripple square tube core body (3) is provided with and lower panel (4) between, the wavy channel core body (3) is by multiple hollow ripple sides
Pipe (2) is arranged parallel to each other composition.
2. a kind of ripple square tube core body sandwich according to claim 1, it is characterised in that：The ripple square tube (2)
Bellows-shaped be sine bellows.
3. a kind of ripple square tube core body sandwich according to claim 1, it is characterised in that the top panel (1) and
The thickness of lower panel (4) is different.
4. a kind of ripple square tube core body sandwich according to claim 1, it is characterised in that the top panel (1), under
Panel (4) and ripple square tube (2) are made by any one in stainless steel, aluminium alloy or titanium alloy material.
5. a kind of preparation method of ripple square tube core body sandwich as any one of Claims 1-4, its feature exists
In comprising the following steps：
S1, straight square tube bending is made ripple square tube by sine bellows；
S2, by the plate cutting of smooth mistake into top panel and lower panel；
S3, the cleaning top panel, lower panel and ripple square tube, are put into dry for standby in dryer；
S4, be parallel to each other multiple ripple square tubes the corrugated square tube core body of assembling, and fixation is standby；
S5, ripple square tube core body described in step S4 is connected with top panel, lower panel described in step S3 it is made ripple square tube core body
Sandwich.
6. a kind of ripple square tube core body sandwich preparation method according to claim 4, it is characterised in that：Step S1
In, the ripple Box Section is square section or rectangular cross-sectional.
7. a kind of ripple square tube core body sandwich preparation method according to claim 4, it is characterised in that：Step S4
In, the ripple square tube is ripple square tube core body by 1~2 times of tube wall spacing assembled parallel.
8. a kind of ripple square tube core body sandwich preparation method according to claim 4, it is characterised in that：Step S4
In, phase difference is 0 °~180 ° between the adjacent ripple square tube.
9. a kind of ripple square tube core body sandwich preparation method according to claim 4, it is characterised in that：The step
In S5, vacuum 10 is kept-2~10-3Pa, 550~1200 DEG C are risen to 1 DEG C/min speed from room temperature, will using high temperature brazing
The top panel, ripple square tube core body and lower panel are made the ripple square tube core body sandwich, are incubated 10min~60min,
Slow cooling is to room temperature.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710042624.3A CN106827713B (en) | 2017-01-20 | 2017-01-20 | A kind of ripple square tube core sandwich and preparation method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710042624.3A CN106827713B (en) | 2017-01-20 | 2017-01-20 | A kind of ripple square tube core sandwich and preparation method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106827713A true CN106827713A (en) | 2017-06-13 |
| CN106827713B CN106827713B (en) | 2019-03-01 |
Family
ID=59120692
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710042624.3A Active CN106827713B (en) | 2017-01-20 | 2017-01-20 | A kind of ripple square tube core sandwich and preparation method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106827713B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109483981A (en) * | 2018-11-22 | 2019-03-19 | 华侨大学 | A kind of honeycomb sandwich plate of embedded multi-level structure |
| CN110435256A (en) * | 2019-08-30 | 2019-11-12 | 哈尔滨工程大学 | A kind of absolute Poisson's ratio honeycomb sandwich structure of rectangular tube unit cell and preparation method thereof |
| CN110560875A (en) * | 2019-09-23 | 2019-12-13 | 南昌航空大学 | double-layer plate with channel structure and vacuum electron beam processing method thereof |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104527144A (en) * | 2014-11-26 | 2015-04-22 | 上海复合材料科技有限公司 | Lightweight multi-functionalization interlayer-structure plate and manufacture method thereof |
-
2017
- 2017-01-20 CN CN201710042624.3A patent/CN106827713B/en active Active
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104527144A (en) * | 2014-11-26 | 2015-04-22 | 上海复合材料科技有限公司 | Lightweight multi-functionalization interlayer-structure plate and manufacture method thereof |
Non-Patent Citations (2)
| Title |
|---|
| X.M.XIANG等: "Blast response of sandwich beams with thin-walled tubes as core", 《ENGINEERING STRUCTURES》 * |
| 郝文乾: "轴向冲击载荷下薄壁折纹管和波纹管的屈曲与能量吸收", 《中国优秀硕士学位论文全文数据库 基础科学辑》 * |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109483981A (en) * | 2018-11-22 | 2019-03-19 | 华侨大学 | A kind of honeycomb sandwich plate of embedded multi-level structure |
| CN109483981B (en) * | 2018-11-22 | 2020-11-06 | 华侨大学 | Honeycomb sandwich plate with embedded multi-level structure |
| CN110435256A (en) * | 2019-08-30 | 2019-11-12 | 哈尔滨工程大学 | A kind of absolute Poisson's ratio honeycomb sandwich structure of rectangular tube unit cell and preparation method thereof |
| CN110435256B (en) * | 2019-08-30 | 2021-03-30 | 哈尔滨工程大学 | Rectangular tube unit cell absolute poisson ratio honeycomb sandwich structure and preparation method thereof |
| CN110560875A (en) * | 2019-09-23 | 2019-12-13 | 南昌航空大学 | double-layer plate with channel structure and vacuum electron beam processing method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106827713B (en) | 2019-03-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107498948B (en) | Multilayer gradient lattice sandwich board and preparation method thereof | |
| CN103009013B (en) | Method for preparing metal honeycomb core and honeycomb sandwich board | |
| CN106827713A (en) | A kind of ripple square tube core body sandwich and preparation method thereof | |
| Shah | Advances in science and technology of compact heat exchangers | |
| CN106891598B (en) | A kind of wavy channel core sandwich and preparation method thereof | |
| US20160271674A1 (en) | Method for preparing metal composite plate strip by rolling | |
| CN105436741A (en) | Silver-copper-indium-titanium middle-temperature brazing filler metal | |
| CN103612007B (en) | A kind of preparation method of high-temperature alloy three-dimensional lattice sandwich structure | |
| CN205027181U (en) | Industrial grade microchannel heat exchanger | |
| CN110260697B (en) | Aluminum-based soaking plate | |
| CN108656641A (en) | A kind of ripple-four directions honeycomb composite sandwich structure and preparation method thereof | |
| CN108161346A (en) | A kind of Ti2The preparation method of AlNb/TA15 bimetallic titanium alloy composite hollow structures | |
| CN103331513B (en) | A kind of manufacture method of superplasticity two phase stainless steel sandwich | |
| CN106839831B (en) | A kind of compact efficient heat exchanger core body and its welding tooling | |
| CN102765227A (en) | Corrugated-honeycombed composite sandwich material in porous structure and method for preparing same | |
| US20120175095A1 (en) | Heat exchanger manifold and method of manufacture | |
| Li et al. | Deformation behavior and mechanical properties of periodic topological Ti structures fabricated by superplastic forming/diffusion bonding | |
| CN107344431A (en) | A kind of honeycomb ripple composite lattice sandwich cylindrical shell and preparation method thereof | |
| CN105478474A (en) | Method for compounding aluminum alloy composite board used for machining automobile oil cooler bottom board | |
| CN102909907A (en) | Multilayer diamond lattice metal-foam aluminum compound sandwich board and production method thereof | |
| CN108397680B (en) | Sandwich metal plate | |
| CN111715961A (en) | Metal rubber honeycomb composite soft sandwich component preparation structure and method thereof | |
| US20120132407A1 (en) | Heat exchanger manifold and method of manufacture | |
| CN113148108A (en) | Double-layer corrugated sandwich heat-insulation/bearing integrated heat protection structure | |
| CN201575276U (en) | Light-weight multi-layer thermal protection material structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220817 Address after: 401420 Chongqing Qijiang Industrial Park Patentee after: Chongqing Gongbang Industry (Group) Co.,Ltd. Address before: Room 502, building 1, No. 40, xiayuangang East Street, Tianhe District, Guangzhou City, Guangdong Province Patentee before: Guangzhou Boyi Intellectual Property Operation Co.,Ltd. Effective date of registration: 20220817 Address after: Room 502, building 1, No. 40, xiayuangang East Street, Tianhe District, Guangzhou City, Guangdong Province Patentee after: Guangzhou Boyi Intellectual Property Operation Co.,Ltd. Address before: Beilin District Xianning West Road 710049, Shaanxi city of Xi'an province No. 28 Patentee before: XI'AN JIAOTONG University |
|
| TR01 | Transfer of patent right |