CN104318009A - Method for designing personalized interbody fusion cage - Google Patents

Method for designing personalized interbody fusion cage Download PDF

Info

Publication number
CN104318009A
CN104318009A CN201410558933.2A CN201410558933A CN104318009A CN 104318009 A CN104318009 A CN 104318009A CN 201410558933 A CN201410558933 A CN 201410558933A CN 104318009 A CN104318009 A CN 104318009A
Authority
CN
China
Prior art keywords
centrum
fusion device
model
invasive lumbar
lumbar fusion
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
Application number
CN201410558933.2A
Other languages
Chinese (zh)
Other versions
CN104318009B (en
Inventor
李淑宇
蒲放
梁航
张明峥
李德玉
樊瑜波
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Beihang University
Original Assignee
Beihang University
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Beihang University filed Critical Beihang University
Priority to CN201410558933.2A priority Critical patent/CN104318009B/en
Publication of CN104318009A publication Critical patent/CN104318009A/en
Application granted granted Critical
Publication of CN104318009B publication Critical patent/CN104318009B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The invention relates to a method for designing a personalized interbody fusion cage. The metod comprises the following steps of performing CT (computed tomography) scanning on a vertebral body; performing three-dimensional model reconstruction on CT continuous section image data; measuring a vertebral body model, namely measuring the sagittal diameter of the vertebral body, the transverse diameter of the vertebral body, the height of vertebrae interval and the like; performing personalized design and implantation on the interbody fusion cage on the basis of the measured parameters; meshing and smoothening; performing material assignment, boundary condition setting and the like to establish a finite element model; solving and analyzing the finite element model. The method provides a basis for the optimization and the improvement of the interbody fusion cage and the personalized interbody fusion cage is designed by considering geometric matching and function matching.

Description

A kind of personalized Invasive lumbar fusion device method for designing
Technical field
The present invention relates to a kind of personalized Invasive lumbar fusion device method for designing, more particularly relate to a kind of method of based on CT 3-dimensional reconstruction and measuring technique, finite element analysis technology, Invasive lumbar fusion device being carried out to personalized design.
Background technology
In clinical interbody fusion, implantation, size, spatial form and the neurotrosis of Invasive lumbar fusion device, implant stability, intervertebral bone graft amount is closely related.But, because differing greatly of physiological parameter and internal milieu individualized feature, standardization, mass, the Invasive lumbar fusion device of serializing production and the interaction of human body are difficult to optimization, cause some Invasive lumbar fusion devices to enter after in body, excessive wear, fatigue failure etc. occur.Therefore, the design of Invasive lumbar fusion device must be personalized.Invasive lumbar fusion device faces complicated ambient stress in vivo, these stress both can affect the reliability of Invasive lumbar fusion device self structure, the normal performance that also can affect Invasive lumbar fusion device function and surrounding host tissue change reconstruction, be one of key factor of Invasive lumbar fusion device success or failure.Therefore, the performance of Invasive lumbar fusion device not only will consider its material type selecting, preparation and surface modification, also should take into full account that it becomes the Configuration Design of medicine equipment, and the interaction between it and surrounding host tissue.At present, the design of most Invasive lumbar fusion device, based on geometric match demand, does not realize designing based on function match.
Summary of the invention
In order to overcome the design of current most Invasive lumbar fusion device based on geometric match demand, do not have to realize the problem based on function match design, the invention discloses a kind of personalized Invasive lumbar fusion device method for designing, described method is by utilizing CT three-dimensional reconstruction, under digital virtual environment, go back the anatomical structure feature of prevertebrate and carry out three-dimensional measurement, carry out personalized design and the implantation of Invasive lumbar fusion device on this basis, use personalized finite element analysis technology to carry out analyzing and studying to designed Invasive lumbar fusion device.
The present invention according to actual needs, the view data such as CT/MRI are imported in developed software CageDesigner, automatically carry out the segmentation of spinal vertebral, set up the geometric model of backbone, automatically carry out the stress and strain model of model, and backbone intervertebral fusion surgical procedure can be simulated and carry out finite element analysis, for the personalized design of Invasive lumbar fusion device provides reference.
The invention discloses a kind of personalized Invasive lumbar fusion device method for designing, specifically comprise the following steps:
1) image acquisition and pre-service: vertebra is carried out Spiral CT scan, the raw data of the vertebra then CT scanner obtained to import in software and carries out auto-sequencing and judgement according to the numbering of image to image.Then medium filtering, gaussian filtering and binary conversion treatment are carried out to the CT image imported.
2) foundation of centrum Iamge Segmentation and three-dimensional model: first manually select an initial lamella to start cutting procedure at software level face view area, the centrum general profile of the initial lamella of manual drawing, then adopts Level Set Method to obtain the centrum precise boundary of initial lamella through iteration.After this cutting procedure will be that starting point carries out cutting operation from upper and lower both direction to all lamellas with reference layer.Because the amplitude of variation of centrum CT image adjacent sheets target is less, thus can the segmentation result gained profile of handy processed lamella as the initial profile of adjacent sheets, then use Level Set Method to obtain the precise boundary of all centrums.Finally, manual method can be adopted to revise obtained profile.For the result of segmentation, adopt object plotting method to draw, and show in the window.
3) vertebral model is measured: centrum sagittal diameter and centrum horizontal shape footpath obtain in the upper soleplate plane of vertebral model.Adopt the cutting function of software, the three-dimensional vertebral model of cutting, obtains soleplate plane on vertebral model.Soleplate plane finds and divides the anterior-posterior axle that vertebral model becomes left and right two halves equally, measure the distance between anterior-posterior axle and vertebral model edge two intersection point, this distance is centrum sagittal diameter.Measure and distance between perpendicular straight line vertebral model edge two intersection point of anterior-posterior axle, what its middle distance was maximum is the horizontal shape footpath of centrum.The height of intervertenral space is measured at vertebral model median sagittal plane.Median sagittal plane manually obtains front and back marginal point and the soleplate central point of terminal plate of vertebral body.The distance measuring upper and lower terminal plate of vertebral body leading edge point is intervertenral space leading edge height, and the distance of 2 terminal plate of vertebral body trailing edge points is intervertenral space trailing edge height, and the distance of two soleplate central points is intervertenral space centre-height.
4) design of Invasive lumbar fusion device and implantation: in existing Invasive lumbar fusion device model bank, according to the upper limb anatomic form (curve of centrum, platform), select the geometric configuration (radian) of fusion device, according to the height of disc height determination Invasive lumbar fusion device, according to centrum transverse diameter, the length of centrum radius vector determination Invasive lumbar fusion device and width.The principle of design makes Invasive lumbar fusion device laminating anatomical structure, reaches larger contact area, meet mechanical strength, promote to merge.For two pieces of Invasive lumbar fusion devices, its symmetry is implanted in centrum latter half of.For single fusion cage, it is tiltedly implanted centrum center.
5) FEM meshing and level and smooth: adopt the Meshing Method based on voxel to carry out stress and strain model to centrum.First by the different coded representation of the pixel of each several part; Then adjacent for levels 8 pixels are connected into 1 voxel as node, remove the voxel of redundancy, using the hexahedral element of remaining voxel as eight nodes.The pixel coder of eight nodes of the unit in model surface and different materials interface is different, now adopt the method for mirror image subdivision that each border hexahedral element is decomposed into 5 tetrahedron elements, then carry out the level and smooth of interface by the node of these tetrahedron elements mobile; In order to reduce calculated amount, some unit consistent for material will merge as required.Adopt the method mapped to be mapped on designed personalized Invasive lumbar fusion device by the finite element grid of the Modular Intervertebral fusion device model in existing Invasive lumbar fusion device model bank, realize the stress and strain model of Invasive lumbar fusion device.
6) assignment of material and boundary condition are arranged: the elastic modulus of range site node densitometer calculated unit, model thickness of cortex of bone and Minor articulus friction factor are set, suppose that cancellous bony material is isotropy, between Invasive lumbar fusion device with centrum, adopt face-face to contact.The all degree of freedom of lower soleplate of hypocentrum are all fixed, and choose the upper soleplate central point R of centrum, by applying downward pressure simulation centrum load-bearing on R, apply torque simulation anteflexion, after stretch, lateral bending, torsion.By above-mentioned steps, complete the foundation of the centrum finite element model being implanted with Invasive lumbar fusion device.
7) the solving and analyzing of finite element model: adopt voxel finite element model derivation algorithm to solve centrum finite element model, obtain major principal stress, equivalent stress, sink and displacement, be used for evaluating stress distribution situation and the misalignment of centrum and Invasive lumbar fusion device, thus determine whether design is reasonable.For irrational design, turn back to step 4 and design is modified, and final realization was not only considered geometric match but also considered the design of personalized Invasive lumbar fusion device of function match.The personalized Invasive lumbar fusion device of final design is with STL formatted output.
The present invention's personalized Invasive lumbar fusion device method for designing advantage comprises:
1, consider geometric match and function match in the design comprehensively, personalized finite element analysis technology is incorporated in the design of Invasive lumbar fusion device.
2, visual display vertebra shape can measure the parameter shape footpath as horizontal in centrum of reacting vertebral body structure feature, centrum sagittal diameter, disc height etc. comprehensively;
3, method for designing is easy, and the running time is short, is easy to clinical expansion.
Accompanying drawing explanation
Fig. 1 is that personalized Invasive lumbar fusion device according to an embodiment of the invention designs concrete implementing procedure figure;
Fig. 2 be according to an embodiment of the invention on centrum soleplate plane carry out parameter measurement schematic diagram;
Fig. 3 according to an embodiment of the inventionly carries out parameter measurement schematic diagram at centrum median plane;
Fig. 4 is two piece Invasive lumbar fusion device implantation position schematic diagram of the present invention;
Fig. 5 is single fusion cage implantation position schematic diagram of the present invention;
Fig. 6 is the centrum stress and strain model result figure of one embodiment of the present of invention;
Fig. 7 is the personalized Invasive lumbar fusion device designed by one embodiment of the present of invention.
Embodiment
As shown in Figure 1, be that personalized Invasive lumbar fusion device according to an embodiment of the invention designs concrete implementing procedure figure, comprise the following steps:
Step 101: image acquisition and pre-service.
Spiral CT scan is carried out to vertebra, obtains vertebra CT image.The raw image data of the vertebra of acquisition to be imported in software and according to the numbering of image, auto-sequencing and judgement to be carried out to image.Then medium filtering, gaussian filtering and binary conversion treatment are carried out to the CT image imported.
Step 102: the foundation of centrum Iamge Segmentation and three-dimensional model.
First manually select an initial lamella to start cutting procedure at software level face view area, the centrum general profile of the initial lamella of manual drawing, then adopt Level Set Method to obtain the centrum precise boundary of initial lamella through iteration.After this cutting procedure will be that starting point carries out cutting operation from upper and lower both direction to all lamellas with reference layer.Because the amplitude of variation of centrum CT image adjacent sheets target is less, thus can the segmentation result gained profile of handy processed lamella as the initial profile of adjacent sheets, then use Level Set Method to obtain the precise boundary of all centrums.Finally, manual method can be adopted to revise obtained profile.For the result of segmentation, adopt object plotting method to draw, and show in the window.
Step 103: vertebral model is measured.
Centrum sagittal diameter and horizontal shape footpath obtain in the upper soleplate plane of vertebral model.Adopt the cutting function of software, the three-dimensional vertebral model of cutting, obtain the upper soleplate plane (Fig. 2) of centrum.Soleplate plane finds and divides the anterior-posterior axle L (Fig. 2) that vertebral model becomes left and right two halves equally, measure the distance between anterior-posterior axle L and vertebral model edge two intersection point C, D (Fig. 2), this distance is the sagittal diameter of centrum.Measure and distance between the perpendicular straight line of anterior-posterior axle L and vertebral model edge two intersection point, the maximum distance between 2 A, B (Fig. 2) of its middle distance is the horizontal shape footpath of centrum.The height of intervertenral space is measured at vertebral model median sagittal plane (Fig. 3).Median sagittal plane manually obtains front and back marginal point E, F, G, H (Fig. 3) and soleplate central point I, J (Fig. 3) of terminal plate of vertebral body.Measure upper and lower terminal plate of vertebral body leading edge point F, the distance of H (Fig. 3) is intervertenral space leading edge height, the distance of 2 terminal plate of vertebral body trailing edge points E, G (Fig. 3) is intervertenral space trailing edge height, and the distance of two soleplate central point I, J (Fig. 3) is intervertenral space centre-height.
Step 104: the design of Invasive lumbar fusion device and implantation.
In existing Invasive lumbar fusion device model bank, according to the upper limb anatomic form (curve of centrum, platform), select the geometric configuration (radian) of fusion device, according to the height of disc height determination Invasive lumbar fusion device, according to centrum transverse diameter, the length of centrum radius vector determination Invasive lumbar fusion device and width.The principle of design makes Invasive lumbar fusion device laminating anatomical structure, reaches larger contact area, meet mechanical strength, promote to merge.For two pieces of Invasive lumbar fusion devices, its symmetry is implanted in centrum latter half of (Fig. 4).First vertebral rim is inside contracted 1/3rd, obtain the gray area shown in Fig. 4, Invasive lumbar fusion device can not implant this part.One piece of Invasive lumbar fusion device is alignd with some D (Fig. 4), moves to the right, until it contacts with gray area, complete the determination of the implantation position of this piece of Invasive lumbar fusion device, then place another piece of Invasive lumbar fusion device symmetrically.For single fusion cage, it is tiltedly implanted centrum center (Fig. 5).First 45 degree are become to place with centrum sagittal diameter in Invasive lumbar fusion device major axis h direction, Invasive lumbar fusion device trailing edge is overlapped with some D (Fig. 5), then Invasive lumbar fusion device is moved in parallel to side, until Invasive lumbar fusion device major axis h is by centrum center O (Fig. 5), complete the implantation of single fusion cage.
Step 105: FEM meshing and level and smooth.
The Meshing Method based on voxel is adopted to carry out stress and strain model to centrum.First by the different coded representation of the pixel of each several part; Then adjacent for levels 8 pixels are connected into 1 voxel as node, remove the voxel of redundancy, using the hexahedral element of remaining voxel as eight nodes.The pixel coder of eight nodes of the unit in model surface and different materials interface is different, now adopt the method for mirror image subdivision that each border hexahedral element is decomposed into 5 tetrahedron elements, then carry out the level and smooth of interface by the node of these tetrahedron elements mobile; In order to reduce calculated amount, some unit consistent for material will merge as required.Adopt the method mapped to be mapped on designed personalized Invasive lumbar fusion device by the finite element grid of the Modular Intervertebral fusion device model in existing Invasive lumbar fusion device model bank, realize the stress and strain model of Invasive lumbar fusion device.A fructufy of FEM meshing is such as shown in Fig. 6.
Step 106: the assignment of material and boundary condition are arranged.
The elastic modulus of range site node densitometer calculated unit, arranges model thickness of cortex of bone and Minor articulus friction factor, supposes that cancellous bony material is isotropy, adopts face-face to contact between Invasive lumbar fusion device with centrum.The all degree of freedom of lower soleplate of hypocentrum are all fixed, and choose the upper soleplate central point R of centrum, by applying downward pressure simulation centrum load-bearing on R, apply torque simulation anteflexion, after stretch, lateral bending, torsion.By above-mentioned steps, complete the foundation of the centrum finite element model being implanted with Invasive lumbar fusion device.
Step 107: the solving and analyzing of finite element model.
Adopt voxel finite element model to solve conventional algorithm EBE-PCG (element by element precon-ditioned conjugate gradient) algorithm to solve, obtain major principal stress, equivalent stress, sink and displacement, be used for evaluating stress distribution situation and the misalignment of centrum and Invasive lumbar fusion device, thus determine whether design is reasonable.For irrational design, turn back to step 4 and design is modified, and final realization was not only considered geometric match but also considered the design of personalized Invasive lumbar fusion device of function match.The personalized Invasive lumbar fusion device of final design is with STL formatted output (Fig. 7).
The design of the personalized lumbar intervertebral fusion device of embodiment
L3-L4 lumbar vertebrae is carried out Spiral CT scan, sweep parameter: thickness 0.63mm, layer is apart from 0.63mm, bulb voltage 120kV, and electric current 225mAs, resolution 512*512pxl, obtain 150 lumbar vertebrae CT images.Medium filtering, gaussian filtering and binary conversion treatment is carried out by these 150 CT data importing softwares.
First a picture with centrum and vertebral arch is manually selected as initial lamella to start cutting procedure at software level face view area, the centrum general profile of the initial lamella of manual drawing, then adopts Level Set Method to obtain the centrum precise boundary of initial lamella through iteration.After this cutting procedure will be that starting point carries out cutting operation from upper and lower both direction to all lamellas with reference layer.
Adopt the cutting function of software, the three-dimensional vertebral model of cutting, obtain the upper soleplate plane (Fig. 2) of centrum.Soleplate plane finds and divides the anterior-posterior axle L (Fig. 2) that vertebral model becomes left and right two halves equally, measure the distance between anterior-posterior axle L and vertebral model edge two intersection point C, D (Fig. 2), obtain centrum sagittal diameter.Measure and distance between the perpendicular straight line of anterior-posterior axle L and vertebral rim two intersection point, the maximum distance between 2 A, B (Fig. 2) of its middle distance is the horizontal shape footpath of centrum.Median sagittal plane manually obtains front and back marginal point E, F, G, H (Fig. 3) and soleplate central point I, J (Fig. 3) of terminal plate of vertebral body.Measure upper and lower terminal plate of vertebral body leading edge point F, the distance of H (Fig. 3) obtains intervertenral space leading edge height, the distance of 2 terminal plate of vertebral body trailing edge points E, G (Fig. 3) obtains intervertenral space trailing edge height, and the distance of two soleplate central point I, J (Fig. 3) obtains intervertenral space centre-height.
Choose JAGUAR tMlUMBAR I/F CAGE (size: height=9mm, wide=9mm, length=25mm, elastic modulus: 3600MPa, Poisson ratio: 0.25) as reference model, design the length of new Invasive lumbar fusion device according to measured centrum horizontal shape footpath, the height of new Invasive lumbar fusion device is set according to disc height.
Two pieces of Invasive lumbar fusion devices are implanted in centrum latter half of.Stress and strain model and level and smooth is carried out to model.Arranging Minor articulus friction factor is 0.1, supposes that cancellous bony material is isotropy, adopts face-face to contact between Invasive lumbar fusion device with centrum.The all degree of freedom of lower soleplate of L4 centrum are all fixed, and choose the upper soleplate central point R of L3 centrum, by applying 400N downward pressure simulation centrum load-bearing on R, apply 10N-m torque simulation anteflexion, after stretch, lateral bending, torsion.
Adopt voxel finite element model to solve conventional algorithm EBE-PCG (element by element precon-ditioned conjugate gradient) algorithm to solve, obtain major principal stress, equivalent stress, sink and displacement, be used for evaluating stress distribution situation and the misalignment of centrum and Invasive lumbar fusion device, thus determine whether design is reasonable.For irrational design, turn back to step 4 and design is modified, and final realization was not only considered geometric match but also considered the design of personalized Invasive lumbar fusion device of function match.The personalized Invasive lumbar fusion device of final design is with STL formatted output (Fig. 7).
Should be understood that, just to illustrate but not determinate in the above description described and carry out the present invention in illustrating, and do not depart from as appended claims under the prerequisite of the present invention that limits, can various change, distortion be carried out to above-described embodiment and/or revise.
drawing reference numeral explanation
The foundation of 101, image acquisition and pre-service 102, centrum Iamge Segmentation and three-dimensional model
103, vertebral model measure 104, the design of Invasive lumbar fusion device and implantation
105, the assignment of FEM meshing and level and smooth 106, material and boundary condition are arranged
107, the solving and analyzing of finite element model.

Claims (5)

1. a method for designing for personalized Invasive lumbar fusion device model, is characterized in that comprising the following steps:
1) image acquisition and pre-service: vertebra is carried out Spiral CT scan, then carries out Image semantic classification by the vertebra raw data that CT scanner obtains, thus obtains centrum image;
2) foundation of centrum Iamge Segmentation and three-dimensional model: the segmentation being realized centrum image by automatic or manual segmentation, adopts object plotting method to complete reconstruction and the display of centrum three-dimensional model;
3) centrum three-dimensional model is measured: the sagittal diameter of centrum and horizontal shape footpath obtain in the upper soleplate plane of centrum three-dimensional model, and the height of intervertenral space is measured at the median sagittal plane of centrum three-dimensional model;
4) design of Invasive lumbar fusion device model and implantation: in existing Invasive lumbar fusion device model bank, according to the upper limb anatomic form of centrum three-dimensional model, select the geometric configuration of fusion device model, according to the height of disc height determination Invasive lumbar fusion device model, according to length and the width of centrum transverse diameter, centrum radius vector determination Invasive lumbar fusion device model, according to the quantity of the Invasive lumbar fusion device model implanted, be implanted to the different parts of centrum three-dimensional model;
5) FEM meshing and level and smooth: respectively FEM meshing and level and smooth is carried out to centrum three-dimensional model and Invasive lumbar fusion device model;
6) assignment of material and boundary condition are arranged: the material properties and the boundary condition that arrange centrum three-dimensional model each several part, by above-mentioned steps, complete the foundation of the centrum finite element model being implanted with Invasive lumbar fusion device model;
7) the solving and analyzing of finite element model: adopt voxel finite element model derivation algorithm to solve centrum finite element model, solving result is used for evaluating stress distribution situation and the misalignment of centrum three-dimensional model and Invasive lumbar fusion device model, thus determines whether design is reasonable; For irrational design, turn back to step 4) design to be modified, final realization had not only been considered geometric match but also had been considered the design of personalized Invasive lumbar fusion device model of function match.
2. the method for designing of personalized Invasive lumbar fusion device model according to claim 1, is characterized in that, the 1st) Image semantic classification described in step comprises medium filtering, gaussian filtering and binary conversion treatment.
3. the method for designing of personalized Invasive lumbar fusion device model according to claim 1, it is characterized in that, 4th) described in step, the concrete mode of Invasive lumbar fusion device model implant site is: for two pieces of Invasive lumbar fusion device models, by latter half of for its symmetrical implantation centrum three-dimensional model, for single fusion cage model, it is tiltedly implanted centrum three-dimensional model center.
4. the method for designing of personalized Invasive lumbar fusion device model according to claim 1, it is characterized in that, 5th) FEM meshing described in step and level and smooth concrete mode are: adopt the Meshing Method based on voxel to carry out stress and strain model and level and smooth to centrum three-dimensional model, adopt the method mapped to carry out stress and strain model to designed Invasive lumbar fusion device model.
5. the method for designing of personalized Invasive lumbar fusion device model according to claim 1, is characterized in that, the 7th) solving result described in step specifically comprises major principal stress, equivalent stress, sinks and displacement.
CN201410558933.2A 2014-10-20 2014-10-20 A kind of personalized Invasive lumbar fusion device design method Expired - Fee Related CN104318009B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410558933.2A CN104318009B (en) 2014-10-20 2014-10-20 A kind of personalized Invasive lumbar fusion device design method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410558933.2A CN104318009B (en) 2014-10-20 2014-10-20 A kind of personalized Invasive lumbar fusion device design method

Publications (2)

Publication Number Publication Date
CN104318009A true CN104318009A (en) 2015-01-28
CN104318009B CN104318009B (en) 2017-10-10

Family

ID=52373240

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410558933.2A Expired - Fee Related CN104318009B (en) 2014-10-20 2014-10-20 A kind of personalized Invasive lumbar fusion device design method

Country Status (1)

Country Link
CN (1) CN104318009B (en)

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104952068A (en) * 2015-05-25 2015-09-30 西安电子科技大学 Automatic vertebral feature point recognition method
CN105581832A (en) * 2016-02-26 2016-05-18 张朝跃 Elasticity modulus determination method and preparation method of individual posterior spinal pedicle screw rod system
CN107252373A (en) * 2017-06-14 2017-10-17 北京航空航天大学 A kind of personalized concrete dynamic modulus Invasive lumbar fusion device and design method
CN108171804A (en) * 2017-12-14 2018-06-15 深圳市毕美科技有限公司 The determining method and device of threedimensional model section plane
CN108289660A (en) * 2015-10-13 2018-07-17 马佐尔机器人有限公司 Global backbone alignment schemes
CN108711187A (en) * 2018-08-03 2018-10-26 华侨大学 The method that registration fusion CT and MRI signal establish human body lumbar vertebrae three-dimensional simulation model
CN109727311A (en) * 2018-12-28 2019-05-07 广州市久邦数码科技有限公司 A kind of 3 D model construction method and mobile terminal
CN109766599A (en) * 2018-12-26 2019-05-17 国家康复辅具研究中心 A kind of personalized anterior intervertebral fusion device design method based on bone remoulding principle
CN109953841A (en) * 2019-04-10 2019-07-02 上海交通大学医学院附属第九人民医院 A kind of construction method of the porous Invasive lumbar fusion device of personalization
CN110384572A (en) * 2019-07-16 2019-10-29 天津市天津医院 CAD personalization lumbar intervertebral fusion device and its designing and manufacturing method
CN110464514A (en) * 2019-07-16 2019-11-19 太原理工大学 The preparation method of application and implantation material of the honeycomb sandwich structure in vertebral implant
CN111281613A (en) * 2020-02-16 2020-06-16 华中科技大学同济医学院附属协和医院 3D printing-based bionic porous artificial vertebral body preparation method
US10902944B1 (en) 2020-01-06 2021-01-26 Carlsmed, Inc. Patient-specific medical procedures and devices, and associated systems and methods
US11083586B2 (en) 2017-12-04 2021-08-10 Carlsmed, Inc. Systems and methods for multi-planar orthopedic alignment
US11112770B2 (en) 2017-11-09 2021-09-07 Carlsmed, Inc. Systems and methods for assisting a surgeon and producing patient-specific medical devices
CN113408172A (en) * 2021-06-28 2021-09-17 大连理工大学 Intervertebral fusion device manufacturing method and manufacturing system
US11166764B2 (en) 2017-07-27 2021-11-09 Carlsmed, Inc. Systems and methods for assisting and augmenting surgical procedures
US11376076B2 (en) 2020-01-06 2022-07-05 Carlsmed, Inc. Patient-specific medical systems, devices, and methods
USD958151S1 (en) 2018-07-30 2022-07-19 Carlsmed, Inc. Display screen with a graphical user interface for surgical planning
US11432943B2 (en) 2018-03-14 2022-09-06 Carlsmed, Inc. Systems and methods for orthopedic implant fixation
US11439514B2 (en) 2018-04-16 2022-09-13 Carlsmed, Inc. Systems and methods for orthopedic implant fixation
US11443838B1 (en) 2022-02-23 2022-09-13 Carlsmed, Inc. Non-fungible token systems and methods for storing and accessing healthcare data
US11696833B2 (en) 2018-09-12 2023-07-11 Carlsmed, Inc. Systems and methods for orthopedic implants
WO2023165071A1 (en) * 2022-03-01 2023-09-07 博志生物科技(深圳)有限公司 Interbody fusion cage, manufacturing method and system therefor, intelligent manufacturing device, and medium
US11793577B1 (en) 2023-01-27 2023-10-24 Carlsmed, Inc. Techniques to map three-dimensional human anatomy data to two-dimensional human anatomy data
US11806241B1 (en) 2022-09-22 2023-11-07 Carlsmed, Inc. System for manufacturing and pre-operative inspecting of patient-specific implants

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102920537A (en) * 2012-11-01 2013-02-13 上海理工大学 Double safety and effectiveness inspection method of human lumbar bone and implant
US20130079679A1 (en) * 2011-09-23 2013-03-28 Orthosensor System And Method For Vertebral Load And Location Sensing

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130079679A1 (en) * 2011-09-23 2013-03-28 Orthosensor System And Method For Vertebral Load And Location Sensing
CN102920537A (en) * 2012-11-01 2013-02-13 上海理工大学 Double safety and effectiveness inspection method of human lumbar bone and implant

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
王甲甲: "人体颈椎有限元建模及仿生颈椎椎间融合器研究", 《中国博士学位论文全文数据库工程科技II辑》 *
蒲放 等: "基于体素的牙种植体及颌骨的有限元建模", 《航天医学与医学工程》 *

Cited By (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104952068A (en) * 2015-05-25 2015-09-30 西安电子科技大学 Automatic vertebral feature point recognition method
CN104952068B (en) * 2015-05-25 2017-11-21 西安电子科技大学 A kind of vertebra characteristic point automatic identifying method
CN108289660A (en) * 2015-10-13 2018-07-17 马佐尔机器人有限公司 Global backbone alignment schemes
US11410767B2 (en) 2015-10-13 2022-08-09 Mazor Robitcs Ltd. Global spinal alignment method
CN108289660B (en) * 2015-10-13 2021-07-27 马佐尔机器人有限公司 Global spinal alignment method
CN105581832B (en) * 2016-02-26 2018-04-10 张朝跃 Personalized Via Posterior Spinal Approach pedicle screw-rod system resilience modulus determines and preparation method
CN105581832A (en) * 2016-02-26 2016-05-18 张朝跃 Elasticity modulus determination method and preparation method of individual posterior spinal pedicle screw rod system
CN107252373B (en) * 2017-06-14 2019-02-26 北京航空航天大学 A kind of porous Invasive lumbar fusion device of personalization and design method
CN107252373A (en) * 2017-06-14 2017-10-17 北京航空航天大学 A kind of personalized concrete dynamic modulus Invasive lumbar fusion device and design method
US11857264B2 (en) 2017-07-27 2024-01-02 Carlsmed, Inc. Systems and methods for physician designed surgical procedures
US11497559B1 (en) 2017-07-27 2022-11-15 Carlsmed, Inc. Systems and methods for physician designed surgical procedures
US11166764B2 (en) 2017-07-27 2021-11-09 Carlsmed, Inc. Systems and methods for assisting and augmenting surgical procedures
US11112770B2 (en) 2017-11-09 2021-09-07 Carlsmed, Inc. Systems and methods for assisting a surgeon and producing patient-specific medical devices
US11083586B2 (en) 2017-12-04 2021-08-10 Carlsmed, Inc. Systems and methods for multi-planar orthopedic alignment
CN108171804A (en) * 2017-12-14 2018-06-15 深圳市毕美科技有限公司 The determining method and device of threedimensional model section plane
CN108171804B (en) * 2017-12-14 2021-10-19 深圳市毕美科技有限公司 Method and device for determining three-dimensional model sectioning plane
US11432943B2 (en) 2018-03-14 2022-09-06 Carlsmed, Inc. Systems and methods for orthopedic implant fixation
US11439514B2 (en) 2018-04-16 2022-09-13 Carlsmed, Inc. Systems and methods for orthopedic implant fixation
USD958151S1 (en) 2018-07-30 2022-07-19 Carlsmed, Inc. Display screen with a graphical user interface for surgical planning
CN108711187A (en) * 2018-08-03 2018-10-26 华侨大学 The method that registration fusion CT and MRI signal establish human body lumbar vertebrae three-dimensional simulation model
US11717412B2 (en) 2018-09-12 2023-08-08 Carlsmed, Inc. Systems and methods for orthopedic implants
US11696833B2 (en) 2018-09-12 2023-07-11 Carlsmed, Inc. Systems and methods for orthopedic implants
CN109766599A (en) * 2018-12-26 2019-05-17 国家康复辅具研究中心 A kind of personalized anterior intervertebral fusion device design method based on bone remoulding principle
CN109727311A (en) * 2018-12-28 2019-05-07 广州市久邦数码科技有限公司 A kind of 3 D model construction method and mobile terminal
CN109953841A (en) * 2019-04-10 2019-07-02 上海交通大学医学院附属第九人民医院 A kind of construction method of the porous Invasive lumbar fusion device of personalization
CN110464514A (en) * 2019-07-16 2019-11-19 太原理工大学 The preparation method of application and implantation material of the honeycomb sandwich structure in vertebral implant
CN110384572A (en) * 2019-07-16 2019-10-29 天津市天津医院 CAD personalization lumbar intervertebral fusion device and its designing and manufacturing method
CN110464514B (en) * 2019-07-16 2020-09-04 太原理工大学 Application of honeycomb sandwich structure in vertebral body implant and preparation method of implant
US11376076B2 (en) 2020-01-06 2022-07-05 Carlsmed, Inc. Patient-specific medical systems, devices, and methods
US10902944B1 (en) 2020-01-06 2021-01-26 Carlsmed, Inc. Patient-specific medical procedures and devices, and associated systems and methods
US11854683B2 (en) 2020-01-06 2023-12-26 Carlsmed, Inc. Patient-specific medical procedures and devices, and associated systems and methods
US11678938B2 (en) 2020-01-06 2023-06-20 Carlsmed, Inc. Patient-specific medical systems, devices, and methods
CN111281613A (en) * 2020-02-16 2020-06-16 华中科技大学同济医学院附属协和医院 3D printing-based bionic porous artificial vertebral body preparation method
CN113408172A (en) * 2021-06-28 2021-09-17 大连理工大学 Intervertebral fusion device manufacturing method and manufacturing system
US11443838B1 (en) 2022-02-23 2022-09-13 Carlsmed, Inc. Non-fungible token systems and methods for storing and accessing healthcare data
WO2023165071A1 (en) * 2022-03-01 2023-09-07 博志生物科技(深圳)有限公司 Interbody fusion cage, manufacturing method and system therefor, intelligent manufacturing device, and medium
US11806241B1 (en) 2022-09-22 2023-11-07 Carlsmed, Inc. System for manufacturing and pre-operative inspecting of patient-specific implants
US11793577B1 (en) 2023-01-27 2023-10-24 Carlsmed, Inc. Techniques to map three-dimensional human anatomy data to two-dimensional human anatomy data

Also Published As

Publication number Publication date
CN104318009B (en) 2017-10-10

Similar Documents

Publication Publication Date Title
CN104318009B (en) A kind of personalized Invasive lumbar fusion device design method
CN104462723A (en) Personalized interbody fusion cage design method based on topological optimization and bony reconstitution simulation
CN102920537B (en) Double safety and effectiveness inspection method of human lumbar bone and implant
Doubrovski et al. Voxel-based fabrication through material property mapping: A design method for bitmap printing
US9250620B2 (en) 3D design and fabrication system for implants
Lavecchia et al. Lumbar model generator: a tool for the automated generation of a parametric scalable model of the lumbar spine
Wang et al. Computational biomechanical modelling of the lumbar spine using marching-cubes surface smoothened finite element voxel meshing
ES2382205T3 (en) Procedure, system, device and software for the creation of a prosthesis stem
CN104523354B (en) Method for manufacturing orthopedic implant based on 3D printing technology
CN113408172A (en) Intervertebral fusion device manufacturing method and manufacturing system
Stojkovic et al. Reverse modelling of human long bones using T-splines-case of tibia
KR101179081B1 (en) Apparatus for designing custom-made prosthesis based on bone density measurement
CN101991422A (en) Method for positioning human body knee joint flexible motion axis in lateral femoral condyle long-axis section
Maloul et al. A technique for the quantification of the 3D connectivity of thin articulations in bony sutures
KR20160126185A (en) Method, System and Computer Program for Fracture Evaluation via X-Ray Image Processing using Computer
Łodygowski et al. Three-dimensional nonlinear finite element model of the human lumbar spine segment
CN113408174A (en) Skeleton model construction method and device, computer equipment and storage medium
Phate et al. Three-Dimensional Finite Element Analysis of Human Tibia Bone
Rayward et al. A subject-specific FEM to predict deep tissue mechanical stresses when supine: Development of efficient contact interfaces using Shared Topology
Li An approach to lumbar vertebra biomechanical analysis using the finite element modeling based on CT Images
Trajanović et al. Morphometric analysis of the hip bone as the basis for reverse engineering
Chen Verification and validation of microCT-based finite element models of bone tissue biomechanics
Zhao et al. The Application of Contact Theory in Finite Element Model of Human L1-L5 Lumbar Segments
TWI463345B (en) Multimedia artificial joint development platform
Branni Constitutive models of bone: The human femur

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20171010

Termination date: 20191020