CN112861252A - Self-defined lattice standard unit and lattice structure - Google Patents

Self-defined lattice standard unit and lattice structure Download PDF

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CN112861252A
CN112861252A CN202011556003.5A CN202011556003A CN112861252A CN 112861252 A CN112861252 A CN 112861252A CN 202011556003 A CN202011556003 A CN 202011556003A CN 112861252 A CN112861252 A CN 112861252A
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lattice
cube
standard
sandwich structure
points
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CN112861252B (en
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吉芬
廖宝华
柏林
蒋睿哲
侯志辉
许少峰
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AVIC Chengdu Aircraft Design and Research Institute
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    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/15Vehicle, aircraft or watercraft design
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
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    • G06F30/17Mechanical parametric or variational design
    • GPHYSICS
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    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F2113/00Details relating to the application field
    • G06F2113/10Additive manufacturing, e.g. 3D printing
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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Abstract

The invention has proposed a self-defining lattice standard cell and lattice structure, self-defining lattice standard cell at first, the geometric definition of this standard cell is to define 8 special nods of the cube with 8 vertexes of the cube, 6 central points of six faces; formed by connection in a specific way. And a sandwich structure formed by self-defined lattice standard units according to a zero-period array at intervals is adopted. The sandwich structure has isotropy, light weight and excellent mechanical property. Meanwhile, by changing the parameters, the structure diversification can be realized, and the structures with different weights and mechanical properties can be obtained so as to meet the design requirements of different structures.

Description

Self-defined lattice standard unit and lattice structure
Technical Field
The invention belongs to the field of structural design, and particularly relates to a user-defined dot matrix standard unit and a dot matrix structure.
Background
The lattice structure is a grid-shaped structure similar to a honeycomb interlayer and is hollow inside, the characteristic is that three-dimensional periodic ordered porous is taken as a characteristic, as shown in figure 1, the lattice structure has excellent strength, rigidity and lighter mass characteristic, the lattice structure is a novel structural form which cannot be realized by the traditional process, and the lattice structure is widely applied to various aspects in the fields of aviation and aerospace along with the rapid development of selective melting additive manufacturing technology in recent years.
All lattice structures are formed by lattice standard cells according to a certain arrangement rule, as shown in fig. 2, the lattice standard cells are basic elements constituting the lattice structure, and the structural form and the arrangement mode of the lattice cells must be defined first for designing and manufacturing the lattice structure.
In the design and manufacture process of the lattice structure, standard cells in a software cell library are generally adopted and stacked in a certain manner to form a lattice structure model, as shown in fig. 3. However, the lattice units are generally complex in shape, variable in cross section and large in data volume, as shown in fig. 4, the data volume of the formed lattice model is far greater than that of a conventional structure digital model, the time for constructing the lattice model is several times longer than that of the general model, the structure stress characteristics brought by different lattice units are different, and the selection of the lattice units is constrained by a software unit library. Occasionally, designers adopt self-designed units to design the lattice structure, but the lattice unit stress characteristics and the model data volume influence cause that a satisfactory effect cannot be achieved.
Although the dot matrix structure is widely applied at home and abroad, software for designing the dot matrix structure is not developed at home at present, a dot matrix unit library of the dot matrix structure is not available, the actual dot matrix structure needs to be applied by means of foreign software, the 3-matic software of Materialise, the added work bench of GE, Netfab issued by Autodesk, 3Dsimd of Ansys and the like, the latest version of CATIA released by a V6 platform also has the dot matrix design capability, the foreign software is expensive in price, has higher requirements on computer configuration, is somewhat immature, and most design units are not introduced. On the premise of a large localization trend, a designer system urgently needs to develop a custom lattice standard unit suitable for structural design, the unit data volume is relatively small, a design model can be quickly formed through conventional software, the unit has good stress characteristics, the requirements of structure strength, rigidity and the like can be met, and the unit is suitable for selective area melting process manufacturing.
Disclosure of Invention
(1) The purpose of the invention is as follows: a novel lattice standard unit is set up in a user-defined mode so as to obtain the model data volume which has excellent stress characteristics, lighter unit body weight and smaller model data volume, and the method is suitable for structural design and modeling of aircrafts and the like.
(2) Technical solution of the invention
The invention provides a self-defined lattice standard unit on one hand, wherein the geometric definition of the standard unit is formed by connecting 8 vertexes of a cube, 6 central points of six faces and 8 special intersection points of the cube by the following method;
a) constructing a cube line frame, and finding out 8 vertexes and 6 central points of six surfaces, wherein the total number of the points is 14;
b) connecting the 6 central points of the six surfaces with four vertexes of the vertical surface (namely the parallel surface) of the surface respectively to obtain 24 straight lines;
c) sequentially connecting 8 non-coplanar vertexes in the cube to obtain 8 straight lines, and sharing 8 special intersection points with the 24 straight lines in the step b);
d) the 8 special intersection points are respectively connected with the central points of three faces closest to the point in the cube to obtain 24 line segments, the 8 special intersection points are respectively connected with the vertex of the cube closest to the point to obtain 8 line segments, and the 8 line segments can effectively increase the boundary area of the unit bodies so that the adjacent unit bodies can be better connected together when the selected area is manufactured in a melting mode; the 32 line segments obtained in total form a line frame structure of the lattice standard cell.
Preferably, 32 line segments in the standard unit body line frame structure are cylinders with the same diameter, and each cylinder is also called a rib small rod to form the custom dot matrix standard micro unit body.
Preferably, 8 small bars of the ribs passing through the top points are trimmed by using six boundary surfaces of the cube respectively, and the ribs converged at the center points of 6 surfaces of the cube are trimmed, so that all the ribs are in the same outline of the cube, and the ends of the ribs are planes and flush with the boundary surfaces of the cube; the resulting standard unit cells are in a regular, monolithic form so that adjacent unit cells can better meet together during selective zone melt fabrication.
Preferably, the diameter of the small bar of the rib is 0.5mm or 0.3 mm.
The invention provides a lattice sandwich structure, and the sandwich layer of the sandwich structure is formed by arranging lattice standard microcell bodies in a periodic array.
Preferably, in the lattice sandwich structure, the lattice standard microcells are arranged in a single-layer array arrangement or a double-layer staggered array arrangement.
Preferably, in the lattice sandwich structure, a lattice standard microcell gradient is added in a specific area to realize the rigidity gradual transition of the solid structure and the sandwich structure.
Preferably, the lattice sandwich structure is integrally formed by 3D printing.
The beneficial technical effects are as follows: by adopting the micro-unit structure provided by the invention, the micro-unit structure has excellent stress characteristic, lighter unit body weight and relatively smaller model data volume, is suitable for structural design and modeling of aircrafts and the like, enables designers to get rid of the limitation of an imported software unit library, can utilize a self-defined lattice standard unit to design a lattice structure through conventional software, reduces the weight of the structure, increases the strength and the rigidity, and realizes data transmission between design and manufacture.
Drawings
Fig. 1, a typical structure diagram of a lattice,
FIG. 2 is a schematic view showing the formation of a lattice structure,
FIG. 3 is a schematic diagram of the lattice structure of different cells,
fig. 4. several lattice elements commonly used in software libraries,
FIG. 5. center points of the cube, cube vertices and faces,
FIG. 6 is a view showing a line connecting a center point of one face of a cube and a vertex of a parallel face thereof,
fig. 7. the vertices of the other four vertical planes are connected in a staggered manner,
fig. 8, the intersection point (the intersection point of the lines of fig. 5 and 6),
FIG. 9. intersection points (all intersection points for each plane in the manner of FIG. 7),
FIG. 10 is a view showing a line connecting the vertex, the center point of the plane and the intersection point,
fig. 11, a standard cell structure diagram,
FIG. 12 is a schematic diagram of the geometric definition and parameters of a standard lattice microcell,
FIG. 13 is a schematic diagram of two typical specifications of standard microcells of a lattice,
FIG. 14. lattice standard microcell arrays form a lattice structure,
FIG. 15 is a schematic view of a lattice sandwich structure formed by lattice standard microcells.
Detailed Description
The invention is described in detail with reference to the accompanying drawings of the specification, firstly, a lattice structure standard unit is defined by user, and the geometric definition of the standard unit defines 8 special intersection points of a cube by 8 vertexes of the cube and 6 central points of six faces; formed by joining in the following manner.
Step 1, constructing a millimeter-scale cube line frame, and finding out 8 vertexes and the central points of six surfaces, wherein the total number of the vertexes and the central points is 14, as shown in fig. 5;
step 2, connecting lines from the central point of one surface to the vertexes of the opposite surface (i.e. parallel surface) of the surface, wherein the total number of lines is 4, as shown in fig. 6, the vertexes of the four surfaces perpendicular to the surface are connected in a staggered manner, and the total number of lines is 4, as shown in fig. 7, and the intersection point of the lines in fig. 5 and 6 is found out, as shown in fig. 8;
step 3, operating each surface according to the step 2, overlapping most of the intersection points, and totally having 8 intersection points, as shown in fig. 9;
step 4, the 8 intersection points shown in fig. 8 are respectively connected with the central point of the nearest one of the two parallel surfaces of the square, 24 lines are used, the 8 intersection points are respectively connected with the vertex of the nearest square, 8 lines are used, and the 8 lines can effectively increase the boundary area of the unit bodies, so that the adjacent unit bodies can be better connected together when the selected area is manufactured by melting; a total of 32 wires make up the geometrically defined bobbin structure of the standard cell body, as shown in fig. 10.
Forming a standard unit body structure by the method, forming mm-level cylinders with the same diameter by using 32 lines, wherein each cylinder is also called a rib small rod; thereby forming the standard microcell body of the custom lattice.
Respectively trimming 8 small bars of the ribs passing through the top points by using six boundary surfaces of the cube, trimming the ribs gathered at the center points of 6 surfaces of the cube, ensuring that all the ribs are in the square outline, and the end heads are planes and are flush with the boundary surfaces of the cube; the resulting standard unit cell is in a regular, monolithic form so that adjacent unit cells can better meet together when the selected area is melt fabricated, as shown in fig. 11.
The constructed isotropic lattice unit is named as a lattice standard micro unit and consists of 32 cylindrical rib small bars with the same diameter, the number, the section shape, the direction and the length of ribs of a unit body in three X \ Y \ Z directions are completely consistent, a fully-enclosed cube with a mm level as a unit can be used for description, and the design elements are cube side length a, and rib small bar diameters d, a and d are parameters, as shown in figure 12. By adjusting the design element parameters, lattice standard microcells with various specifications can be formed. Two lattice standard microcell specifications are commonly used in the design, a is 5mm, the diameter d of the small rib bar is 0.5mm, or a is 3mm, the diameter d of the small rib bar is 0.3mm, as shown in fig. 13.
The lattice standard micro-unit constructed in the above manner has the same projection and characteristics of the physical structure in the three directions of X \ Y \ Z, is an isotropic lattice unit, can be arrayed, and forms a lattice structure suitable for selective area melting process manufacturing, as shown in fig. 14.
The standard cells can construct a lattice sandwich structure formed by the standard cells in a zero-pitch array, as shown in fig. 15. The sandwich structure has isotropy, light weight and excellent mechanical property. Meanwhile, by changing the parameters, the structure diversification can be realized, and the structures with different weights and mechanical properties can be obtained so as to meet the design requirements of different structures.
According to the designed lattice sandwich structure, the standard units can be arranged in a staggered periodic array, and the density gradient of the standard units can be increased in a specific area, so that the rigidity gradual transition of a solid structure and a sandwich structure is realized, and the rigidity mutation of the structure is reduced.
Example 1:
1.1 geometric construction: constructing a lattice standard microcell according to a geometric relationship, and defining the side length a of a design element cube and the diameter d of a rib small rod;
2, process verification: taking a typical lattice standard micro unit with a being 5mm and d being 0.5mm, forming a lattice structure with the same specification and size by an array similar to a lattice unit of a certain software library commonly used in engineering, carrying out a laser selective melting manufacturing test, and verifying process feasibility;
3, in the mechanical property test, a typical lattice standard micro unit with a being 5mm and d being 0.5mm is selected, similar lattice units are formed with a lattice structure with the same specification and size through an array with a certain software library commonly used in engineering, and mechanical property examination and comparison tests such as element-level and typical-level stretching, compression, shearing, bending and the like are carried out to verify the mechanical property;
4 other feature alignment: compared with the similar lattice unit, the lattice unit has lighter structural weight and smaller model data volume.
By adopting the lattice standard unit provided by the invention, through manufacturing of laser selective melting lattice parts and mechanical property tests, the self-constructed lattice standard micro unit is verified to be capable of better forming a lattice structure, through process verification and mechanical property tests, the engineering feasibility is strong, the problem that the micro unit cannot be formed because of being a suspension structure is solved, and the lattice standard unit has good manufacturability, excellent stress characteristic, light structural weight and small model data volume.

Claims (9)

1. A self-defined lattice standard cell is characterized in that the geometric definition of the standard cell is formed by connecting 8 vertexes of a cube, 6 central points of six faces and 8 special intersection points of the cube by the following method;
step S1, constructing a cube line frame, and finding out 8 vertexes and 6 central points of six surfaces, wherein the total number of the points is 14;
step S2, connecting 6 central points of the six surfaces with four vertexes of the facing vertical surface respectively to obtain 24 straight lines;
step S3, sequentially connecting 8 non-coplanar vertexes in the cube to obtain 8 straight lines, wherein the 8 straight lines and the 24 straight lines in the step S2 have 8 special intersection points in total;
step S4, respectively connecting 8 special intersection points to central points of three faces nearest to the point in the cube to obtain 24 line segments, respectively connecting the 8 special intersection points to a vertex of the cube nearest to the point to obtain 8 line segments, wherein the 8 line segments can effectively increase the boundary area of the unit bodies so that adjacent unit bodies can be better connected together when the selected area is manufactured by melting; the 32 line segments obtained in total form a line frame structure of the lattice standard cell.
2. The lattice standard cell of claim 1, wherein 32 line segments in the line frame structure of the lattice standard cell are cylinders with the same diameter, each cylinder is a rib small rod, and a custom lattice standard microcell body is formed.
3. The lattice standard cell of claim 2, wherein the resulting lattice standard microcell body is trimmed by: respectively trimming 8 small rib bars passing through the top points by using six boundary surfaces of the cube, and trimming the small rib bars gathered at the center points of 6 surfaces of the cube to ensure that all ribs are in the same cube outline, and the end heads are planes and flush with the boundary surfaces of the cube; the obtained standard unit body is in a regular and integral form.
4. The lattice standard cell of claim 3, wherein the rib bars have a diameter of 0.5mm or 0.3 mm.
5. A lattice sandwich structure using the lattice standard microcells according to claim 3 as a sandwich layer, wherein the sandwich layer is formed by arranging the lattice standard microcells in a periodic array.
6. The lattice sandwich structure of claim 5, wherein said sandwich structure has lattice standard microcells arranged in a single layer array arrangement or a double layer staggered periodic array arrangement.
7. The lattice sandwich structure of claim 6, wherein said sandwich structure has zero spacing between lattice standard microcells.
8. The lattice sandwich structure of claim 7, wherein in said sandwich structure, lattice standard microcell gradient is added to specific area to realize rigidity gradual transition between solid structure and sandwich structure.
9. The dot matrix sandwich structure according to any one of claims 5 to 8 wherein said sandwich structure is integrally formed by 3D printing.
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115206558A (en) * 2022-07-07 2022-10-18 中国核动力研究设计院 Fuel assembly lower tube seat based on multilayer staggered lattice structure, filter body and application

Citations (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5296923A (en) * 1991-01-09 1994-03-22 Konica Corporation Color image reproducing device and method
CN102303427A (en) * 2011-07-12 2012-01-04 北京航空航天大学 Dual-interlayer symmetrical multi-pyramid configuration three-dimensional integrally-braid lattice composite material and preparation method thereof
CN103324783A (en) * 2013-05-30 2013-09-25 国家电网公司 LOD model real-time generation method based on side folding
CN103345064A (en) * 2013-07-16 2013-10-09 卫荣杰 Cap integrated with 3D identifying and 3D identifying method of cap
US20140149085A1 (en) * 2012-11-24 2014-05-29 Dennis John Newland Correlated Hyperbolic Paraboloid Structural Members
CN106599420A (en) * 2016-12-02 2017-04-26 北京空间飞行器总体设计部 Zero-expansion dot matrix cylindrical shell structure used for spacecraft and design method thereof
CN106650085A (en) * 2016-12-20 2017-05-10 清华大学 Finite element mesh-based method for generating hollow model by entity model
CN106694884A (en) * 2016-12-29 2017-05-24 西安铂力特激光成形技术有限公司 Hollowed-out lattice sandwich layer with gradient functionality and manufacturing method of hollowed-out lattice sandwich layer
CN107038164A (en) * 2016-02-03 2017-08-11 幸福在线(北京)网络技术有限公司 A kind of method for sharing virtual reality image, apparatus and system
CN107679334A (en) * 2017-10-19 2018-02-09 中国航空工业集团公司西安飞机设计研究所 A kind of Varying-thickness composite material laminated board finite element modeling method
CN107742014A (en) * 2017-09-29 2018-02-27 北京空间飞行器总体设计部 The design method of phase-change energy storage device dot matrix sandwich based on increasing material manufacturing
CN107843136A (en) * 2017-09-29 2018-03-27 北京空间飞行器总体设计部 A kind of phase-change energy storage device dot matrix sandwich based on increasing material manufacturing
US20180089348A1 (en) * 2015-04-16 2018-03-29 Hitachi, Ltd. Whole Integrated Analysis Model Assist Device and Whole Integrated Analysis Model Assist Method
CN108038293A (en) * 2017-12-06 2018-05-15 首都航天机械公司 A kind of light multifunction lattice structure and its laser gain material manufacture method
CN108170947A (en) * 2017-12-27 2018-06-15 重庆大学 A kind of method that novel lattice structure is obtained based on glowworm swarm algorithm
CN108953443A (en) * 2018-07-17 2018-12-07 中国人民解放军海军工程大学 Indent octagon cubic lattice Sandwich Plates
CN109084169A (en) * 2018-09-17 2018-12-25 中南大学 A kind of lattice structure and dot matrix part
CN109635320A (en) * 2018-11-02 2019-04-16 北京理工大学 A kind of lattice structure of the high energy dissipation ability based on laser gain material manufacture
CN109885971A (en) * 2019-03-20 2019-06-14 北京空间飞行器总体设计部 Design of satellite construction method based on three-dimensional lattice material
CN110570526A (en) * 2019-09-06 2019-12-13 南京航空航天大学 Topological information guided three-dimensional lattice structural member internal geometric data acquisition method
CN110674614A (en) * 2019-09-12 2020-01-10 无锡江南计算技术研究所 Signal eye diagram analysis method based on RX MASK central dot matrix
CN110705093A (en) * 2019-09-29 2020-01-17 北京星航机电装备有限公司 Lightweight lattice structure parametric modeling and data lightweight processing method
CN111186140A (en) * 2020-01-20 2020-05-22 浙江大学 Method for generating mask printing path with distributed force lines
US20200210629A1 (en) * 2016-02-10 2020-07-02 Autodesk, Inc. Designing objects using lattice structure optimization
CN111425543A (en) * 2020-03-30 2020-07-17 华中科技大学 Enhanced type superposed hollow lattice structure and application thereof
CN211028252U (en) * 2019-10-31 2020-07-17 上海船舶工艺研究所(中国船舶工业集团公司第十一研究所) Device for processing free edge of ship component
CN111723438A (en) * 2020-06-12 2020-09-29 哈尔滨工程大学 Method for eliminating thermal buckling of dot matrix sandwich plate structure and inhibiting nonlinear flutter
CN111967089A (en) * 2020-08-04 2020-11-20 南京理工大学 Irregular three-dimensional lattice structure heat insulation performance optimization design method based on gradual change cell size

Patent Citations (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5296923A (en) * 1991-01-09 1994-03-22 Konica Corporation Color image reproducing device and method
CN102303427A (en) * 2011-07-12 2012-01-04 北京航空航天大学 Dual-interlayer symmetrical multi-pyramid configuration three-dimensional integrally-braid lattice composite material and preparation method thereof
US20140149085A1 (en) * 2012-11-24 2014-05-29 Dennis John Newland Correlated Hyperbolic Paraboloid Structural Members
CN103324783A (en) * 2013-05-30 2013-09-25 国家电网公司 LOD model real-time generation method based on side folding
CN103345064A (en) * 2013-07-16 2013-10-09 卫荣杰 Cap integrated with 3D identifying and 3D identifying method of cap
US20180089348A1 (en) * 2015-04-16 2018-03-29 Hitachi, Ltd. Whole Integrated Analysis Model Assist Device and Whole Integrated Analysis Model Assist Method
CN107038164A (en) * 2016-02-03 2017-08-11 幸福在线(北京)网络技术有限公司 A kind of method for sharing virtual reality image, apparatus and system
US20200210629A1 (en) * 2016-02-10 2020-07-02 Autodesk, Inc. Designing objects using lattice structure optimization
CN106599420A (en) * 2016-12-02 2017-04-26 北京空间飞行器总体设计部 Zero-expansion dot matrix cylindrical shell structure used for spacecraft and design method thereof
CN106650085A (en) * 2016-12-20 2017-05-10 清华大学 Finite element mesh-based method for generating hollow model by entity model
CN106694884A (en) * 2016-12-29 2017-05-24 西安铂力特激光成形技术有限公司 Hollowed-out lattice sandwich layer with gradient functionality and manufacturing method of hollowed-out lattice sandwich layer
CN107742014A (en) * 2017-09-29 2018-02-27 北京空间飞行器总体设计部 The design method of phase-change energy storage device dot matrix sandwich based on increasing material manufacturing
CN107843136A (en) * 2017-09-29 2018-03-27 北京空间飞行器总体设计部 A kind of phase-change energy storage device dot matrix sandwich based on increasing material manufacturing
CN107679334A (en) * 2017-10-19 2018-02-09 中国航空工业集团公司西安飞机设计研究所 A kind of Varying-thickness composite material laminated board finite element modeling method
CN108038293A (en) * 2017-12-06 2018-05-15 首都航天机械公司 A kind of light multifunction lattice structure and its laser gain material manufacture method
CN108170947A (en) * 2017-12-27 2018-06-15 重庆大学 A kind of method that novel lattice structure is obtained based on glowworm swarm algorithm
CN108953443A (en) * 2018-07-17 2018-12-07 中国人民解放军海军工程大学 Indent octagon cubic lattice Sandwich Plates
CN109084169A (en) * 2018-09-17 2018-12-25 中南大学 A kind of lattice structure and dot matrix part
CN109635320A (en) * 2018-11-02 2019-04-16 北京理工大学 A kind of lattice structure of the high energy dissipation ability based on laser gain material manufacture
CN109885971A (en) * 2019-03-20 2019-06-14 北京空间飞行器总体设计部 Design of satellite construction method based on three-dimensional lattice material
CN110570526A (en) * 2019-09-06 2019-12-13 南京航空航天大学 Topological information guided three-dimensional lattice structural member internal geometric data acquisition method
CN110674614A (en) * 2019-09-12 2020-01-10 无锡江南计算技术研究所 Signal eye diagram analysis method based on RX MASK central dot matrix
CN110705093A (en) * 2019-09-29 2020-01-17 北京星航机电装备有限公司 Lightweight lattice structure parametric modeling and data lightweight processing method
CN211028252U (en) * 2019-10-31 2020-07-17 上海船舶工艺研究所(中国船舶工业集团公司第十一研究所) Device for processing free edge of ship component
CN111186140A (en) * 2020-01-20 2020-05-22 浙江大学 Method for generating mask printing path with distributed force lines
CN111425543A (en) * 2020-03-30 2020-07-17 华中科技大学 Enhanced type superposed hollow lattice structure and application thereof
CN111723438A (en) * 2020-06-12 2020-09-29 哈尔滨工程大学 Method for eliminating thermal buckling of dot matrix sandwich plate structure and inhibiting nonlinear flutter
CN111967089A (en) * 2020-08-04 2020-11-20 南京理工大学 Irregular three-dimensional lattice structure heat insulation performance optimization design method based on gradual change cell size

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
XIN JIN ET AL.: "Optimal design and modeling of 3D variable-density lattice structures", 《2017 8TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ICMAE)》 *
朱健峰: "点阵结构机械性能分析与应用", 《中国优秀博硕士学位论文全文数据库(硕士)信息科技辑》 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115206558A (en) * 2022-07-07 2022-10-18 中国核动力研究设计院 Fuel assembly lower tube seat based on multilayer staggered lattice structure, filter body and application
CN115206558B (en) * 2022-07-07 2024-04-19 中国核动力研究设计院 Fuel assembly lower tube seat based on multilayer staggered lattice structure, filter body and application

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