CN114343756A - Flying wing grabbing type fascia closer - Google Patents
Flying wing grabbing type fascia closer Download PDFInfo
- Publication number
- CN114343756A CN114343756A CN202210029365.1A CN202210029365A CN114343756A CN 114343756 A CN114343756 A CN 114343756A CN 202210029365 A CN202210029365 A CN 202210029365A CN 114343756 A CN114343756 A CN 114343756A
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- CN
- China
- Prior art keywords
- rod
- closer
- recovery
- ring
- needle body
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- 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.)
- Pending
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- 210000003195 fascia Anatomy 0.000 title claims abstract description 26
- 238000011084 recovery Methods 0.000 claims abstract description 66
- 230000007246 mechanism Effects 0.000 claims description 5
- 230000006378 damage Effects 0.000 abstract description 5
- 208000027418 Wounds and injury Diseases 0.000 description 7
- 230000008859 change Effects 0.000 description 4
- 208000014674 injury Diseases 0.000 description 3
- 238000001356 surgical procedure Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000002357 laparoscopic surgery Methods 0.000 description 1
- 238000002324 minimally invasive surgery Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 210000001835 viscera Anatomy 0.000 description 1
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Abstract
The invention relates to the field of medical instruments, in particular to a flying wing grabbing type fascia closer which comprises a closer, a wire clamping rod, a limiting component and a suture traction component, wherein the closer is connected with the wire clamping rod through a connecting rod, one end of the wire clamping rod is arranged in the closer, the upper half end of the closer is fixedly provided with a handle, the limiting component is arranged on the handle, the suture traction component is arranged on the closer and is used for moving a recovery rod out of a containing groove, so that a plurality of groups of recovery rods are unfolded, meanwhile, the size design of a first through hole does not influence the unfolding of the recovery rods, the cross section area of one end of each recovery rod is increased after the recovery rods are unfolded, the operation needle body is conveniently clamped during recovery, after the operation suture falls into the recovery rods, an inner rod is reset, the recovery rods return to the containing groove, and when the needle body is extracted, the recovery rod can not cause secondary damage to the patient.
Description
Technical Field
The invention relates to the field of medical instruments, in particular to a flying wing grabbing type fascia closer.
Background
The laparoscopic surgery is a newly developed minimally invasive surgery method, has the advantages of small incision, quick recovery and less pain compared with the traditional surgery, is an inevitable trend for the development of future surgery methods, and needs to be applied to a fascia closer in the surgery.
The fascia closer is used for completing the suture of fascia through the matching of the closer and a suture retractor, the closer is inserted firstly, the middle position of a surgical suture is brought into a body, two ends of the surgical suture are brought out of the body through the suture retractor, the closer is taken out, and then the surgical suture at the two taken out ends is knotted and sutured.
The fascia occluders of the prior art have the following disadvantages: when the suture retractor is used for taking out two ends of the surgical suture from the body of a patient, the suture retractor is inconvenient to butt with the surgical suture accurately and takes out the surgical suture, and when the suture retractor is withdrawn from the body of the patient, secondary injury is easily caused to the wound of the patient.
Disclosure of Invention
The invention provides a flying wing grabbing type fascia closer aiming at the technical problems in the prior art.
The technical scheme for solving the technical problems is as follows: the utility model provides a flying wing snatchs formula manadesma obturator, includes obturator, trapping mechanism, spacing subassembly and suture traction assembly, the obturator with be connected through the connecting rod between the trapping mechanism, the one end of trapping mechanism is installed the inside of obturator, the upper half end of obturator is fixed with the handle, install on the handle spacing subassembly, suture traction assembly installs on the obturator.
Preferably, the flying wing grabbing type fascia closer is provided with a first channel and a second channel which are obliquely arranged, two groups of connecting rods are provided with a first through hole and a second through hole respectively, central axes of the first channel and the first through hole are overlapped, central axes of the second channel and the second through hole are overlapped, and the aperture of the first channel is smaller than that of the first through hole.
Preferably, the two sides of the handle are sequentially provided with an upper limiting hole, a sliding chute and a lower limiting hole from top to bottom, and the upper limiting hole and the lower limiting hole have the same shape.
Preferably, the wing grabbing type fascia closer comprises a clamping block and a movable seat, the two ends of the clamping block are fixed with the limiting blocks, two groups of connecting blocks are symmetrically arranged on the inner sides of the limiting blocks, the movable seat is arranged inside the handle, one end of the wire clamping rod is connected to the middle position of one side of the movable seat, a limiting groove is formed in the movable seat, the connecting blocks are arranged inside the limiting groove, the two groups of clamping blocks are connected through a first spring, and the first spring is located in the middle position of the movable seat.
Preferably, in the flying wing grabbing type fascia closer, the fixture block, the limiting block and the connecting block are of an integrated structure, the cross section of the limiting block is the same as that of the upper limiting hole, and the limiting block and the handle form a clamping structure.
Preferably, the flying wing grabbing type fascia closer comprises a needle body and a ring, wherein the needle body is arranged inside a first channel or a second channel, a plurality of groups of accommodating grooves are formed in the outer side of the pointed end of the needle body at equal angles, a first connecting ring is fixed inside the pointed end of the needle body, a limiting seat is fixed at the tail end of the needle body, the inside of the needle body is hollowed out, the ring is fixed at the upper end of an inner rod, a limiting ring is fixed at the upper half end of the inner rod, and a second spring is arranged between the limiting ring and the upper end of the needle body.
Preferably, in the winged grasping type fascia closer, the inner rod, the finger ring and the limiting ring are of an integrated structure, the inner rod and the needle body form a sliding structure, and the outer diameter of the needle body is the same as the aperture of the first channel.
Preferably, foretell all-wing aircraft snatchs formula manadesma closer, wherein suture traction assembly still includes recovery pole and interior pole, the recovery pole is located the inside of accomodating the groove, the wiring groove has been seted up to the upper end inboard of recovery pole, the lower half of recovery pole is fixed with the second go-between, first connecting groove has been seted up to the lower extreme of recovery pole, the internally mounted of first connecting groove has first connecting ring, interior pole is located the inside of needle body, the lower extreme of interior pole is seted up flutedly, the lower extreme of interior pole is fixed with the third go-between, the third go-between is located inside the recess, the recovery pole with be connected through the connecting rod between the interior pole, the second connecting groove has all been seted up at the upper and lower both ends of connecting rod, and upper and lower two sets of second connecting groove's inside is installed second go-between and the third go-between the pole respectively.
Preferably, the above flying wing grabbing type fascia closer, wherein the recovery rod and the first connecting ring constitute a rotating structure, the second connecting ring and the connecting rod constitute a rotating structure, and the connecting rod and the third connecting ring constitute a rotating structure.
Preferably, in the winged grasping type fascia closer, the outer side of the recovery rod is tangent to the outer side of the needle body, the upper end and the lower end of the thread bundling groove are concave, and the shortest distance between the upper ends of the two symmetrically arranged groups of recovery rods after being unfolded is smaller than the aperture of the first through hole.
The invention has the beneficial effects that: will retrieve the pole and shift out from accomodating inslot portion to make multiunit recovery pole expand, the dimensional design of first through-hole can not influence the recovery pole and expand simultaneously, increase the cross sectional area of needle body one end after the recovery pole expands, be convenient for carry out the centre gripping to the operation suture when retrieving the needle body, the operation suture falls into the inside back of recovery pole, interior pole resets, and the recovery pole is got back to and is accomodate inslot portion, when taking the needle body out, the recovery pole can not be to patient's secondary injury.
Drawings
FIG. 1 is a schematic view of a closure of the present invention;
FIG. 2 is a schematic view of the use of the closure of the present invention in conjunction with a suture traction assembly;
FIG. 3 is a schematic view of a spacing assembly according to the present invention;
fig. 4 is a schematic cross-sectional view of the needle body according to the present invention;
FIG. 5 is an enlarged view of a portion of FIG. 4;
FIG. 6 is a schematic view of the expanding structure of the recovery rod at one end of the needle body according to the present invention;
FIG. 7 is a schematic sectional view of the recovery rod at one end of the needle body according to the present invention;
FIG. 8 is a schematic cross-sectional view of the recovery rod at one end of the needle body according to the present invention in an expanded state;
fig. 9 is an exploded view of the needle body, the recovery rod, the connecting rod and the inner rod according to the present invention.
In the drawings, the components represented by the respective reference numerals are listed below:
1. a closer; 2. a connecting rod; 3. a wire clamping rod; 4. a first channel; 5. a second channel; 6. a first through hole; 7. a second through hole; 8. a handle; 9. a chute; 10. an upper limiting hole; 11. a lower limiting hole; 12. a limiting component; 121. a clamping block; 122. a limiting block; 123. connecting blocks; 124. a movable seat; 125. a limiting groove; 126. a first spring; 13. a suture traction assembly; 131. a needle body; 132. a receiving groove; 133. a first connecting ring; 134. a limiting seat; 135. a recovery rod; 136. a wiring trough; 137. a second connection ring; 138. a first connecting groove; 139. a connecting rod; 1310. a second connecting groove; 1311. an inner rod; 1312. a groove; 1313. a third connecting ring; 1314. a ring; 1315. a limiting ring; 1316. a second spring.
Detailed Description
The principles and features of this invention are described below in conjunction with the following drawings, which are set forth by way of illustration only and are not intended to limit the scope of the invention.
As shown in fig. 1-9, a winged grasping type fascia closer comprises a closer 1, a thread clamping rod 3, a limiting component 12 and a suture traction component 13, wherein the closer 1 is connected with the thread clamping rod 3 through a connecting rod 2, one end of the thread clamping rod 3 is installed inside the closer 1, the upper half end of the closer 1 is fixed with a handle 8, the limiting component 12 is installed on the handle 8, and the suture traction component 13 is installed on the closer 1.
First passageway 4 and second passageway 5 that the slope set up have been seted up on the closer 1, have seted up first through-hole 6 and second through-hole 7 on two sets of connecting rods 2 respectively, and the axis coincidence of first passageway 4 and first through-hole 6, the axis coincidence of second passageway 5 and second through-hole 7, the aperture of first passageway 4 is less than the aperture of first through-hole 6. After the connecting rod 2 is folded, the first through hole 6 and the second through hole 7 which are arranged on the connecting rod 2 correspond to the first channel 4 and the second channel 5 respectively, so that the needle body 131 can be conveniently passed through the first channel 4 and the first through hole 6, one end of the needle body 131 is enabled to fall between the connecting rods 2, the damage of the needle body 131 to the internal organs of a patient is avoided, and the size of the first through hole 6 is designed, so that the recovery rod 135 can be conveniently unfolded.
An upper limiting hole 10, a sliding chute 9 and a lower limiting hole 11 are sequentially arranged on two sides of the handle 8 from top to bottom, and the upper limiting hole 10 and the lower limiting hole 11 are identical in shape. Make spacing subassembly 12 remove on handle 8 through spout 9, through offering spacing hole 10 and lower spacing hole 11 on handle 8 upper and lower both ends, be convenient for cooperate spacing subassembly 12 to install different positions on handle 8.
Spacing subassembly 12 includes fixture block 121 and sliding seat 124, fixture block 121's both ends are fixed with spacing piece 122, spacing piece 122's inboard symmetry is provided with two sets of connecting blocks 123, sliding seat 124 installs the inside at handle 8, one side intermediate position of sliding seat 124 is connected with the one end of clamping bar 3, spacing groove 125 has been seted up to sliding seat 124's inside, the internally mounted of spacing groove 125 has connecting block 123, be connected through first spring 126 between two sets of fixture blocks 121, first spring 126 is located the intermediate position of sliding seat 124, formula structure as an organic whole between fixture block 121 and spacing piece 122 and the connecting block 123, the cross sectional shape of spacing piece 122 is the same with the cross sectional shape of last spacing hole 10, spacing piece 122 and handle 8 constitute block structure. Through pressing two sets of fixture blocks 121, make first spring 126 shrink, and then make the stopper 122 that fixture block 121 both ends set up move out from last spacing hole 10 or lower spacing hole 11 is inside, through promoting fixture block 121, make fixture block 121 drive sliding seat 124 with the help of connecting block 123 and move in handle 8 is inside, after moving to handle 8 one end, loosen fixture block 121, make first spring 126 promote two sets of fixture blocks 121, and then make stopper 122 block out the one end of last spacing hole 10 or lower spacing hole 11, thereby make the one end of clamping bar 3 go up and down fixedly, control connecting rod 2 is folded or tensile, change the form of connecting rod 2, and then change the distance of clamping bar 3 one end to closer 1.
The suture traction assembly 13 further comprises a recovery rod 135 and an inner rod 1311, the recovery rod 135 is located inside the storage groove 132, a thread binding groove 136 is formed in the inner side of the upper end of the recovery rod 135, a second connection ring 137 is fixed to the lower half end of the recovery rod 135, a first connection groove 138 is formed in the lower end of the recovery rod 135, a first connection ring 133 is installed inside the first connection groove 138, the inner rod 1311 is located inside the needle body 131, a groove 1312 is formed in the lower end of the inner rod 1311, a third connection ring 1313 is fixed to the lower end of the inner rod 1311, the third connection ring 1313 is located inside the groove 1312, the recovery rod 135 and the inner rod 1311 are connected through a connection rod 139, second connection grooves 1310 are formed in the upper and lower ends of the connection rod 139, a second connection ring 137 and a third connection ring 1313 are installed inside the upper and lower second connection grooves, the recovery rod 135 and the first connection ring 133 form a rotation structure, the second connection ring 137 and the connection rod 139 form a rotation structure, the connecting rod 139 and the third connecting ring 1313 form a rotating structure, the outer sides of the recovery rods 135 are tangent to the outer side of the needle body 131, the upper and lower ends of the bundling groove 136 are concave, and the shortest distance between the upper ends of the two groups of symmetrically arranged recovery rods 135 after being unfolded is smaller than the aperture of the first through hole 6. Through controlling the rising of the inner rod 1311, the inner rod 1311 drives the third connecting ring 1313 arranged at the tail end to rise, and then one end of the connecting rod 139 installed on the third connecting ring 1313 rises, so that the angle of the connecting rod 139 is changed, the connecting rod 139 pushes the recovery rod 135, one end of the recovery rod 135 rotates on the first connecting ring 133, and then the recovery rod 135 moves out of the storage groove 132, so that multiple groups of recovery rods 135 are unfolded, meanwhile, the size design of the first through hole 6 does not influence the unfolding of the recovery rod 135, the cross-sectional area of one end of the needle body 131 is increased after the recovery rod 135 is unfolded, the needle body 131 is conveniently clamped with the surgical suture, after the surgical suture falls into the recovery rod 135, the inner rod 1311 resets, the recovery rod 135 returns to the storage groove 132, and when the recovery rod 135 is pulled out, the recovery rod 135 does not secondarily injure the patient.
The working principle is as follows: when a wound of a patient is sutured, an operation suture is installed on the suture clamping rod 3, one end of the closer 1 provided with the suture clamping rod 3 is inserted into the body of the patient, then the two sets of fixture blocks 121 are pressed to contract the first spring 126, the limiting blocks 122 arranged at the two ends of the fixture blocks 121 are moved out of the lower limiting hole 11, the fixture blocks 121 are pushed to drive the movable seat 124 to move in the handle 8 through the connecting blocks 123, after the fixture blocks 121 are moved to one end of the handle 8, the fixture blocks 121 are released, the first spring 126 pushes the two sets of fixture blocks 121, the limiting blocks 122 are clamped out of one end of the upper limiting hole 10, one end of the suture clamping rod 3 is lifted and fixed, the connecting rod 2 is controlled to be folded or stretched to change the shape of the connecting rod 2, the connecting rod 2 is unfolded to be in a flying wing shape, one end of the needle body 131 penetrates through the first channel 4 and the first through hole 6 formed in the connecting rod 2, then the finger ring 1314 is pulled to make the finger ring 1314 drive the inner rod 1311 to move in the needle body 131, so that the limiting ring 1315 fixed on the inner rod 1311 moves, the second spring 1316 is compressed through the matching of the limiting ring 1315 and one end of the needle body 131, so that the position of the inner rod 1311 rises, the inner rod 1311 drives the third connecting ring 1313 arranged at the tail end to rise, and then one end of the connecting rod 139 arranged on the third connecting ring 1313 rises, so that the angle of the connecting rod 139 is changed, the connecting rod 139 pushes the recovery rod 135, one end of the recovery rod 135 rotates on the first connecting ring 133, so that the recovery rod 135 moves out of the accommodating groove 132, so that a plurality of groups of recovery rods 135 are unfolded, then the needle body 131 is pulled for a certain distance, the surgical suture falls to the inner side of one group of the recovery rods 135, and when the finger ring 1314 is released, the second spring 1316 resets and pushes the limiting ring 1315 to move, and then make interior pole 1311 descend and accomplish the reduction, when taking out needle body 131, the operation suture falls to restraint the inside fixed of line groove 136 to inside recovery pole 135 got back to and accomodate groove 132, recovery pole 135 can not be to patient's wound secondary injury, and in the same way, will pass the second through-hole 7 that offers on second passageway 5 and the connecting rod 2 inside at the one end of needle body 131, will pass patient's skin flesh with the other end of operation suture and take out, through knoing the both ends of operation suture, make the operation suture accomplish to sew up to the wound.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "left", "right", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are only for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the referred device or element must have a specific orientation and a specific orientation configuration and operation, and thus, should not be construed as limiting the present invention. Furthermore, "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and the like are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate member, or they may be connected through two or more elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
While one embodiment of the present invention has been described in detail, the description is only a preferred embodiment of the present invention and should not be taken as limiting the scope of the invention. All equivalent changes and modifications made within the scope of the present invention shall fall within the scope of the present invention.
Claims (10)
1. The utility model provides a wing-flying snatchs formula manadesma obturator, includes obturator (1), trapping mechanism (3), spacing subassembly (12) and suture traction assembly (13), its characterized in that: the novel wire clamping device is characterized in that the closer (1) is connected with the wire clamping rod (3) through a connecting rod (2), one end of the wire clamping rod (3) is installed inside the closer (1), a handle (8) is fixed to the upper half end of the closer (1), the limiting component (12) is installed on the handle (8), and the suture traction component (13) is installed on the closer (1).
2. The flying wing grasping fascia closer of claim 1, wherein: offer first passageway (4) and second passageway (5) that the slope set up on closer (1), it is two sets of first through-hole (6) and second through-hole (7) have been seted up on connecting rod (2) respectively, first passageway (4) with the axis coincidence of first through-hole (6), second passageway (5) with the axis coincidence of second through-hole (7), the aperture of first passageway (4) is less than the aperture of first through-hole (6).
3. The flying wing grasping fascia closer of claim 1, wherein: the handle is characterized in that an upper limiting hole (10), a sliding groove (9) and a lower limiting hole (11) are sequentially formed in the two sides of the handle (8) from top to bottom, and the upper limiting hole (10) and the lower limiting hole (11) are identical in shape.
4. The flying wing grasping fascia closer of claim 1, wherein: spacing subassembly (12) include fixture block (121) and sliding seat (124), the both ends of fixture block (121) are fixed with spacing piece (122), the inboard symmetry of spacing piece (122) is provided with two sets of connecting blocks (123), sliding seat (124) are installed the inside of handle (8), one side intermediate position of sliding seat (124) is connected with the one end of trapping mechanism pole (3), spacing groove (125) have been seted up to the inside of sliding seat (124), the internally mounted of spacing groove (125) has connecting block (123), and is two sets of be connected through first spring (126) between fixture block (121), first spring (126) are located the intermediate position of sliding seat (124).
5. The flying wing grasping fascia closer of claim 4, wherein: the clamping block (121), the limiting block (122) and the connecting block (123) are of an integrated structure, the cross section of the limiting block (122) is the same as that of the upper limiting hole (10), and the limiting block (122) and the handle (8) form a clamping structure.
6. The flying wing grasping fascia closer of claim 1, wherein: suture traction assembly (13) include needle body (131) and ring (1314), needle body (131) are installed in the inside of first passageway (4) or second passageway (5), the multiunit is accomodate groove (132) to the most advanced outside isogonism of needle body (131) has been seted up, the most advanced inside of needle body (131) is fixed with first connecting ring (133), the end of needle body (131) is fixed with spacing seat (134), the inside fretwork of needle body (131), the upper end at interior pole (1311) is fixed in ring (1314), spacing ring (1315) are fixed to the upper end of interior pole (1311), spacing ring (1315) with set up second spring (1316) between the upper end of needle body (131).
7. The flying wing grasping fascia closer of claim 6, wherein: the inner rod (1311), the finger ring (1314) and the limiting ring (1315) are of an integrated structure, the inner rod (1311) and the needle body (131) form a sliding structure, and the outer diameter of the needle body (131) is the same as the aperture of the first channel (4).
8. The flying wing grasping fascia closer of claim 1, wherein: the suture traction component (13) further comprises a recovery rod (135) and an inner rod (1311), the recovery rod (135) is located inside the containing groove (132), a thread binding groove (136) is formed in the inner side of the upper end of the recovery rod (135), a second connecting ring (137) is fixed to the lower half end of the recovery rod (135), a first connecting groove (138) is formed in the lower end of the recovery rod (135), a first connecting ring (133) is installed inside the first connecting groove (138), the inner rod (1311) is located inside the needle body (131), a groove (1312) is formed in the lower end of the inner rod (1311), a third connecting ring (1313) is fixed to the lower end of the inner rod (1311), the third connecting ring (1313) is located inside the groove (1312), the recovery rod (135) and the inner rod (1311) are connected through a connecting rod (139), and second connecting grooves (1310) are formed in the upper end and the lower end of the connecting rod (139), and a second connecting ring (137) and a third connecting ring (1313) are respectively arranged in the upper and lower groups of second connecting grooves (1310).
9. The flying wing grasping fascia closer of claim 8, wherein: the recovery rod (135) and the first connection ring (133) constitute a rotation structure, the second connection ring (137) and the connection rod (139) constitute a rotation structure, and the connection rod (139) and the third connection ring (1313) constitute a rotation structure.
10. The flying wing grasping fascia closer of claim 8, wherein: the outer side of the recovery rod (135) is tangent to the outer side of the needle body (131), the upper end and the lower end of the wire bundling groove (136) are concave, and the shortest distance between the upper ends of the two symmetrically arranged recovery rods (135) after being unfolded is smaller than the aperture of the first through hole (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210029365.1A CN114343756A (en) | 2022-01-11 | 2022-01-11 | Flying wing grabbing type fascia closer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210029365.1A CN114343756A (en) | 2022-01-11 | 2022-01-11 | Flying wing grabbing type fascia closer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114343756A true CN114343756A (en) | 2022-04-15 |
Family
ID=81110005
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210029365.1A Pending CN114343756A (en) | 2022-01-11 | 2022-01-11 | Flying wing grabbing type fascia closer |
Country Status (1)
| Country | Link |
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| CN (1) | CN114343756A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117145906A (en) * | 2023-10-26 | 2023-12-01 | 麦格纳卫蓝新能源汽车技术(镇江)有限公司 | Detachable shock absorber and dismounting device thereof |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1654016A (en) * | 1998-03-09 | 2005-08-17 | 苏图诺有限公司 | Suturing device for sealing an opening in a blood vessel |
| US20130253543A1 (en) * | 2012-03-13 | 2013-09-26 | Suture Ease, LLC | Needle and snare guide apparatus for passing suture |
| US20140128887A1 (en) * | 2012-11-02 | 2014-05-08 | Medtronic Vascular, Inc. | Suturing Device Having a Retractable Distal Tip and Method for Sealing an Opening in a Blood Vessel or Other Biological Structure |
| US20150157316A1 (en) * | 2013-12-09 | 2015-06-11 | Teleflex Medical Incorporated | Laparoscopic fascial closure system |
| CN106214196A (en) * | 2016-07-20 | 2016-12-14 | 江苏三联星海医疗器械股份有限公司 | A kind of deep fascia stiching instrument |
| CN206138151U (en) * | 2016-07-20 | 2017-05-03 | 江苏三联星海医疗器械股份有限公司 | Line hooking device of ware is sewed up to deep manadesma |
| CN206482618U (en) * | 2016-09-14 | 2017-09-12 | 上海执中医疗技术有限公司 | Tissue closing device and tissue closure system |
| CN108158635A (en) * | 2016-12-07 | 2018-06-15 | 英特姆（武汉）医疗科技有限公司 | Puncture needle and wound closure device |
| CN111631769A (en) * | 2020-07-01 | 2020-09-08 | 霍会芳 | Fascia suture device |
-
2022
- 2022-01-11 CN CN202210029365.1A patent/CN114343756A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1654016A (en) * | 1998-03-09 | 2005-08-17 | 苏图诺有限公司 | Suturing device for sealing an opening in a blood vessel |
| US20130253543A1 (en) * | 2012-03-13 | 2013-09-26 | Suture Ease, LLC | Needle and snare guide apparatus for passing suture |
| US20140128887A1 (en) * | 2012-11-02 | 2014-05-08 | Medtronic Vascular, Inc. | Suturing Device Having a Retractable Distal Tip and Method for Sealing an Opening in a Blood Vessel or Other Biological Structure |
| US20150157316A1 (en) * | 2013-12-09 | 2015-06-11 | Teleflex Medical Incorporated | Laparoscopic fascial closure system |
| CN106214196A (en) * | 2016-07-20 | 2016-12-14 | 江苏三联星海医疗器械股份有限公司 | A kind of deep fascia stiching instrument |
| CN206138151U (en) * | 2016-07-20 | 2017-05-03 | 江苏三联星海医疗器械股份有限公司 | Line hooking device of ware is sewed up to deep manadesma |
| CN206482618U (en) * | 2016-09-14 | 2017-09-12 | 上海执中医疗技术有限公司 | Tissue closing device and tissue closure system |
| CN108158635A (en) * | 2016-12-07 | 2018-06-15 | 英特姆（武汉）医疗科技有限公司 | Puncture needle and wound closure device |
| CN111631769A (en) * | 2020-07-01 | 2020-09-08 | 霍会芳 | Fascia suture device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117145906A (en) * | 2023-10-26 | 2023-12-01 | 麦格纳卫蓝新能源汽车技术(镇江)有限公司 | Detachable shock absorber and dismounting device thereof |
| CN117145906B (en) * | 2023-10-26 | 2024-03-12 | 麦格纳卫蓝新能源汽车技术(镇江)有限公司 | Detachable shock absorber and dismounting device thereof |
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Address after: No. 2, 3rd Floor, Building 13, Zone B, No. 818, Gaoxin Avenue, East Lake New Technology Development Zone, Wuhan City, Hubei Province, 430000 (Wuhan Area of Free Trade Zone) Applicant after: Interm (Wuhan) Medical Technology Co.,Ltd. Address before: No.2, 3rd floor, building 13, area B, 818 Gaoxin Avenue, Donghu New Technology Development Zone, Wuhan City, Hubei Province, 430000 Applicant before: YINGTEMU (WUHAN) MEDICAL TECHNOLOGY CO.,LTD. |