CN113069209A - Deployable instrument arm - Google Patents
Deployable instrument arm Download PDFInfo
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- CN113069209A CN113069209A CN202110370008.7A CN202110370008A CN113069209A CN 113069209 A CN113069209 A CN 113069209A CN 202110370008 A CN202110370008 A CN 202110370008A CN 113069209 A CN113069209 A CN 113069209A
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- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61B—DIAGNOSIS; SURGERY; IDENTIFICATION
- A61B34/00—Computer-aided surgery; Manipulators or robots specially adapted for use in surgery
- A61B34/30—Surgical robots
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- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61B—DIAGNOSIS; SURGERY; IDENTIFICATION
- A61B34/00—Computer-aided surgery; Manipulators or robots specially adapted for use in surgery
- A61B34/70—Manipulators specially adapted for use in surgery
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25J—MANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
- B25J9/00—Programme-controlled manipulators
- B25J9/10—Programme-controlled manipulators characterised by positioning means for manipulator elements
- B25J9/106—Programme-controlled manipulators characterised by positioning means for manipulator elements with articulated links
- B25J9/1065—Programme-controlled manipulators characterised by positioning means for manipulator elements with articulated links with parallelograms
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- Health & Medical Sciences (AREA)
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- Surgery (AREA)
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- Biomedical Technology (AREA)
- Heart & Thoracic Surgery (AREA)
- Nuclear Medicine, Radiotherapy & Molecular Imaging (AREA)
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Abstract
The present disclosure provides a deployable instrument arm, comprising: the connecting part is of a telescopic structure and comprises a driving end and a driven end; the control part is connected with the active end of the connecting part; a far-end executing part, one end of which is connected with the driven end of the connecting part and the other end of which is connected with an executing mechanism; the control part can control the connecting part to stretch and swing along a spherical surface, so that the actuating mechanism always points to the spherical center corresponding to the spherical surface. No part for transmission is arranged above the spherical surface of the expandable structure formed by the components of the mechanical arm, so that no extra motion inertia is generated in the motion process of the mechanical arm driving operation to be a fixed point, and the motion stability of the mechanical arm is improved.
Description
Technical Field
The present disclosure relates to an instrument arm, and more particularly, to a deployable instrument arm.
Background
At present, a slave end instrument arm of a surgical robot with an immobile point is provided with a connecting rod assembly for transmitting motion in the axial direction of a surgical tool guide pipe, and in order to avoid interference between an assembly and an auxiliary surgical instrument or a patient in the motion process, the length of each connecting rod of the assembly needs to be increased, so that the volume of the instrument arm is increased. The surgical robot arm can be regarded as a cantilever beam structure, when the length of each connecting rod in the structure is increased, the motion inertia of the arm is increased, the elastic deformation of each component is increased in the motion process, and the repeated positioning precision of the tail end of a surgical tool is reduced.
Disclosure of Invention
Technical problem to be solved
Based on the above-mentioned problem, this disclosure provides a deployable instrument arm to alleviate technical problem such as the terminal repeated positioning precision of surgical tool reduces among the prior art.
(II) technical scheme
The present disclosure provides a deployable instrument arm, comprising:
the connecting part is of a telescopic structure and comprises a driving end and a driven end;
the control part is connected with the active end of the connecting part;
a far-end executing part, one end of which is connected with the driven end of the connecting part and the other end of which is connected with an executing mechanism;
the control part can control the connecting part to stretch and swing along a spherical surface, so that the actuating mechanism always points to the spherical center corresponding to the spherical surface.
In an embodiment of the present disclosure, the deployment control portion includes:
the base is provided with a first driving rotating shaft and a second driving rotating shaft, and the axis of the first driving rotating shaft is superposed with the axis of the second driving rotating shaft;
the first driving rod comprises a first driving connecting end, and the first driving connecting end is fixedly connected with the first driving rotating shaft;
and the second driving rod comprises a third driving connecting end, and the third driving connecting end is fixedly connected with the second driving rotating shaft.
In an embodiment of the present disclosure, the distal executing portion includes:
the instrument seat is provided with an instrument seat bracket;
a first driven link including a first driven connection end;
the second driven rod comprises a third driven connecting end;
the first driven connecting end and the third driven connecting end are pivoted to the instrument base support through a driven rotating shaft.
In the embodiment of the present disclosure, the deployable instrument arm further includes a first auxiliary connecting rod and a second auxiliary connecting rod, one end of the first auxiliary connecting rod is pivoted to the auxiliary connecting rod support, the auxiliary connecting rod support is fixedly connected to the connecting portion, one end of the second auxiliary connecting rod is pivoted to the instrument base support, and the other end of the first auxiliary connecting rod is pivoted to the other end of the second auxiliary connecting rod.
In an embodiment of the present disclosure, the driving end includes a first deployment connection end and a second deployment connection end, and the driven end includes a third deployment connection end and a fourth deployment connection end;
the first driving rod further comprises a second driving connecting end;
the second driving rod further comprises a fourth driving connecting end;
the first unfolding connecting end and the second active connecting end are pivoted through a first connecting rotating shaft;
the second unfolding connecting end and the fourth driving connecting end are pivoted through a fourth connecting rotating shaft;
the third unfolding connecting end and the second driven connecting end are pivoted through a third connecting rotating shaft;
and the fourth unfolding connecting end and the fourth driven connecting end are pivoted through a fourth connecting rotating shaft.
Furthermore, the connecting part further comprises a first spherical connecting rod, a second spherical connecting rod and a spherical connecting rotating shaft for pivotally connecting the first spherical connecting rod with the second spherical connecting rod, and the spherical connecting rotating shaft penetrates through the middle part of the first spherical connecting rod and the middle part of the second spherical connecting rod.
Furthermore, the first connecting rotating shaft, the spherical connecting rotating shaft and the fourth connecting rotating shaft intersect at a point.
Furthermore, the second connecting rotating shaft, the spherical connecting rotating shaft and the third connecting rotating shaft intersect at a point.
Further, the radius of curvature of the first spherical link is equal to or greater than the radius of curvature of the second spherical link.
In an embodiment of the present disclosure, the control portion further includes a driving motor for driving the first driving rotating shaft and the second driving rotating shaft to rotate.
(III) advantageous effects
According to the technical scheme, the deployable instrument arm disclosed by the invention has at least one or part of the following beneficial effects:
(1) the instrument arm structure can be realized to have a physical fixed point, and other components for transmission are not arranged below the structure, so that a larger space is formed below the instrument arm for placing other surgical tools for assisting in surgical implementation, the instrument arm structure is more compact, and the occupied space is smaller;
(2) the instrument arm is of a spherical expandable structure, on the premise of realizing the same stroke, the size of each part is smaller in the scheme adopted by the method, the instrument arm of the surgical robot can be generally regarded as a cantilever beam structure, when the length of each component in the structure is reduced, the motion inertia of the instrument arm is reduced, the elastic deformation of each component in the motion process is correspondingly reduced, and the repeated positioning precision of the tail end of a surgical tool is further improved; and
(3) no part for transmission is arranged above the spherical surface of the expandable structure formed by the components of the mechanical arm, so that no extra motion inertia is generated in the motion process of the mechanical arm driving operation to be a fixed point, and the motion stability of the mechanical arm is improved.
Drawings
Fig. 1 is a schematic diagram of a slave operation end of a robot applied to a deployable robot arm according to an embodiment of the present disclosure.
Fig. 2 is a schematic structural view of an instrument arm applied to a deployable instrument arm according to an embodiment of the present disclosure.
Fig. 3 is a structural diagram of an auxiliary link support of an instrument arm applied to a deployable instrument arm according to an embodiment of the present disclosure.
Fig. 4 is a schematic view of a structure of an instrument holder bracket of an instrument arm applied to a deployable instrument arm according to an embodiment of the present disclosure.
Fig. 5 is a schematic view of the structure of each spherical link of an instrument arm applied to a deployable instrument arm according to an embodiment of the present disclosure.
Fig. 6 is a schematic view of the geometry of two adjacent links of an instrument arm applied to a deployable instrument arm according to an embodiment of the disclosure.
Fig. 7 is a schematic view of an instrument arm physical motionless point position for application to a deployable instrument arm in accordance with an embodiment of the disclosure.
Fig. 8 is a schematic view of instrument arm motion applied to a deployable instrument arm in accordance with an embodiment of the disclosure.
[ description of main reference numerals in the drawings ] of the embodiments of the present disclosure
L01 Instrument arm
101 base
102 first active lever
103 second active lever
104 first spherical connecting rod
105 second spherical connecting rod
106 instrument seat
107 first driven lever
108 second driven lever
109 auxiliary connecting rod support
110 first auxiliary link
111 second auxiliary link
112 instrument seat support
201 first active shaft
202 second active shaft
203 first connecting rotating shaft
204 second connecting rotating shaft
205 spherical connection rotating shaft
206 third connecting rotating shaft
207 fourth connecting shaft
208 bracket connecting shaft
209 passive shaft
210 first support shaft
211 second support shaft
212 third support shaft
Detailed Description
The utility model provides a can expand apparatus arm, can expand apparatus arm can realize that apparatus arm structure has a physics motionless point, and does not have all the other driven spare parts that are used for below this structure for there is great space to be used for placing other surgical instruments and be used for assisting the operation to implement in apparatus arm below, and apparatus arm structure is compacter, and occupation space is littleer, improves the terminal repeated positioning accuracy of surgical instruments, more is favorable to lifting mechanism arm motion stability.
For the purpose of promoting a better understanding of the objects, aspects and advantages of the present disclosure, reference is made to the following detailed description taken in conjunction with the accompanying drawings.
In an embodiment of the present disclosure, there is provided a deployable instrument arm, as shown in fig. 1 to 8, including: the connecting part is of a telescopic structure and comprises a driving end and a driven end; the control part is connected with the active end of the connecting part; a far-end executing part, one end of which is connected with the driven end of the connecting part and the other end of which is connected with an executing mechanism; the control part can control the connecting part to stretch and swing along a spherical surface, so that the actuating mechanism always points to the spherical center corresponding to the spherical surface.
In an embodiment of the present disclosure, the deployment control portion includes: the base 101 is provided with a first driving rotating shaft 201 and a second driving rotating shaft 202, and the axis of the first driving rotating shaft 201 is overlapped with the axis of the second driving rotating shaft 202; the first driving rod 102 comprises a first driving connecting end, and the first driving connecting end is fixedly connected with the first driving rotating shaft 201; the second driving rod 103 includes a third driving connecting end, and the third driving connecting end is fixedly connected to the second driving rotating shaft 202.
In an embodiment of the present disclosure, the distal executing portion includes: an instrument holder 106 provided with an instrument holder bracket 112; a first driven link 107 including a first driven connection end; a second driven link 108 including a third driven connection end; the first driven connection end and the third driven connection end are both pivotally connected to the instrument holder bracket 112 through a driven shaft 209.
In the embodiment of the present disclosure, the deployable instrument arm further includes a first auxiliary link 110 and a second auxiliary link 111, one end of the first auxiliary link 110 is pivotally connected to the auxiliary link bracket 109, the auxiliary link bracket 109 is fixedly connected to the connecting portion, one end of the second auxiliary link 111 is pivotally connected to the instrument base bracket 112, and the other end of the first auxiliary link 110 is pivotally connected to the other end of the second auxiliary link 111.
In an embodiment of the present disclosure, the driving end includes a first deployment connection end and a second deployment connection end, and the driven end includes a third deployment connection end and a fourth deployment connection end; the first active lever 102 further comprises a second active connecting end; the second driving lever 103 further comprises a fourth driving connecting end; the first unfolding connecting end and the second active connecting end are pivoted through a first connecting rotating shaft 203; the second unfolding connecting end and the fourth driving connecting end are pivoted through a fourth connecting rotating shaft 207; the third unfolding connecting end and the second driven connecting end are pivoted through a third connecting rotating shaft 206; the fourth unfolding connecting end and the fourth driven connecting end are pivoted through a fourth connecting rotating shaft 207.
Further, the connecting portion further includes a first spherical connecting rod 104, a second spherical connecting rod 105, and a spherical connecting rotating shaft 205 for pivotally connecting the first spherical connecting rod 104 and the second spherical connecting rod 105, wherein the spherical connecting rotating shaft 205 passes through the middle portion of the first spherical connecting rod 104 and the middle portion of the second spherical connecting rod 105.
Further, the first connecting rotating shaft 203, the spherical connecting rotating shaft 205 and the fourth connecting rotating shaft 207 intersect at a point.
Further, the second connecting shaft 204, the spherical connecting shaft 205 and the third connecting shaft 206 intersect at a point.
Further, the radius of curvature of the first spherical link 104 is equal to or greater than the radius of curvature of the second spherical link 105.
Further, the control portion further includes a driving motor for driving the first driving rotating shaft 201 and the second driving rotating shaft 202 to rotate.
In an embodiment of the present disclosure, there is provided a deployable instrument arm system of a deployable instrument arm unit according to any one of the above, including: the deployable instrument arm is connected with an endoscope; the deployable instrument arm is connected with a surgical tool; the deployable instrument arm is connected with a detection device; forming a multifunctional medical device.
Specifically, in the embodiment of the present disclosure, as shown in fig. 1, it is a schematic view of a slave operation end of a surgical robot, and the slave operation end is generally provided with 3 or 4 slave operation arms, one of the slave operation arms generally serves as a scope holding arm of an endoscope, and the other slave operation arms are instrument arms. As shown in fig. 1, L01 is a robot arm. The mechanical arm is characterized in that the main structure of the mechanical arm is a spherical extensible structure formed by a plurality of spherical connecting rods, and the spherical extensible structure can move around one point in space, namely a fixed point, in 2 degrees of freedom. Before the operation is carried out, the space position of the immobile point can be adjusted by adjusting the posture of the passive arm of the slave operation arm so as to adapt to the operation requirements of different operations.
The operation arm of the present disclosure will be described with reference to the robot arm L01 as an example. As shown in fig. 2, the instrument arm L01 includes a base 101, a plurality of spherical links, an instrument holder 106, and the like. The base 101 is used for connecting the passive adjusting mechanism and the instrument arm L01, and the base 101 is provided with two rotating shafts, a first driving rotating shaft 201 and a second driving rotating shaft 202. The first driving shaft 201 is provided with a first driving rod 102, one end of the first driving rod 102 is connected with the base 101 through the first driving shaft 201, and the first driving rod 102 can rotate around the first driving shaft 201. The second driving shaft 202 is provided with a second driving rod 103, the second driving rod 103 is connected with the base 101 through the second driving shaft 202, and the second driving rod 103 can rotate around the second driving shaft 202. The axes of the first driving rotating shaft 201 and the second driving rotating shaft 202 are overlapped, and a driving motor is installed in the base 101 to respectively drive the first driving rotating shaft 201 and the second driving rotating shaft 202 to rotate, so that the rotation angles of the first driving rod 102 and the second driving rod can be accurately controlled. The other end of the first driving rod 102 is connected with one end of the first spherical connecting rod 104 through a first connecting rotating shaft 203, the other end of the second driving rod 103 is connected with the second spherical connecting rod 105 through a second connecting rotating shaft 204, a spherical connecting rotating shaft 205 is arranged in the middle of the first spherical connecting rod 104 and the second spherical connecting rod 105, and the first spherical connecting rod 104 and the second spherical connecting rod 105 are connected through the spherical connecting rotating shaft 205. The other ends of the first spherical connecting rod 104 and the second spherical connecting rod 105 are sequentially connected with the other second spherical connecting rods and the first spherical connecting rod in the same mode, and the spherical connecting rods connected with each other form a spherical expandable structure. One end of the first driven rod 107 and one end of the second driven rod 108 at the distal end of the expandable structure are respectively connected with the second spherical connecting rod 105 and the first spherical connecting rod 104 at the distal end of the expandable structure through a third connecting rotating shaft 206 and a fourth connecting rotating shaft 207. The other ends of the first driven rod 107 and the second driven rod 108 are connected with the instrument holder bracket 112 through a driven rotating shaft 209, and the instrument holder bracket 112 is fixedly connected with the instrument holder 106. A support connecting shaft 208 is arranged in the middle of the first spherical connecting rod 104 and the second spherical connecting rod 105 at the far end of the expandable structure, an auxiliary connecting rod support 109 (as shown in fig. 3) is fixedly arranged at the upper part of the support connecting shaft, one end of the first auxiliary connecting rod 110 is connected with the auxiliary connecting rod support 109 through a first support shaft 210, the first auxiliary connecting rod 110 can rotate around the first support shaft 210, the other end of the first auxiliary connecting rod 10 is connected with the second auxiliary connecting rod 111 through a second support shaft 211, and the other end of the second auxiliary connecting rod 111 is connected with the instrument seat support 112 through a third support shaft 212. As shown in fig. 3, the first bracket shaft 210 is disposed perpendicular to the bracket connection shaft 208. As shown in fig. 4, the passive rotating shaft 209 is disposed perpendicular to the third support shaft 212.
Under the constraint of the first auxiliary link 110 and the second auxiliary link 111, the movement of the instrument holder bracket 112 and the instrument holder 106 can be controlled. The rotation of the first and second active levers 102 and 103 can drive the mechanical seat 106 to move around a point in two degrees of freedom in space.
As shown in fig. 5, the first driving link 102, the second driving link 103, the first spherical connecting rod 104, the second spherical connecting rod 105, the first driven link 107 and the second driven link 108 are all spherical connecting rods, wherein the first driving link 102, the second spherical connecting rod 105 and the second driven link 108 have the same radius, and the second driving link 103, the first spherical connecting rod 104 and the first driven link 107 have the same radius. The geometric relationship between the first spherical connecting rod 104 and the second spherical connecting rod 105 is shown in fig. 6, the radius of the lower curved surface of the second spherical connecting rod 105 is greater than or equal to the radius of the upper curved surface of the first spherical connecting rod 104, and the axes of the upper rotating shafts of the two connecting rods can meet at a point O.
As shown in fig. 7 and 8, when the first and second driving levers 102 and 103 are driven, the movement of each link is always on a spherical surface with a spherical center at point O, i.e., a physical fixed point of the instrument arm L01, and the movement of the instrument holder 106 is also on a spherical surface with a spherical center at point O, and the physical fixed point O and the sticking point can be kept coincident with each other by adjusting the posture of the passive arm during the operation, and the axis of the catheter of the surgical instrument can always pass through point O.
Because the radius of the lower curved surface of the second spherical connecting rod 105 is greater than or equal to the radius of the upper curved surface of the first spherical connecting rod 104, interference does not occur in the motion process of each connecting rod, and meanwhile, the robot arm L01 has two degrees of freedom, and the robot base 106 can reach any position on the spherical surface with the point O as the sphere center in the working space range.
As shown in fig. 6, the deployable structure formed by the links can be regarded as being arranged on a spherical surface, and there are no other components below the deployable structure, i.e. there are no links or other components used for transmission inside the spherical surface, or there are no links used for transmission in the radial direction of the spherical surface, and there is a large space below the instrument arm L01 for placing other surgical tools for assisting the surgical operation. Compared with the prior art, the instrument arm L01 is more compact in structure and occupies less space.
So far, the embodiments of the present disclosure have been described in detail with reference to the accompanying drawings. It is to be noted that, in the attached drawings or in the description, the implementation modes not shown or described are all the modes known by the ordinary skilled person in the field of technology, and are not described in detail. Further, the above definitions of the various elements and methods are not limited to the various specific structures, shapes or arrangements of parts mentioned in the examples, which may be easily modified or substituted by those of ordinary skill in the art.
From the above description, those skilled in the art should clearly recognize that a deployable instrument arm of the present disclosure is disclosed.
In summary, the present disclosure provides a deployable instrument arm, which can realize that an instrument arm structure has one physical fixed point, and there are no other components for transmission below the structure, so that there is a larger space below the instrument arm for placing other surgical tools for assisting surgical implementation, the instrument arm structure is more compact, and the occupied space is smaller; the instrument arm is of a spherical expandable structure, on the premise of realizing the same stroke, the size of each part is smaller in the scheme adopted by the method, the instrument arm of the surgical robot can be generally regarded as a cantilever beam structure, when the length of each component in the structure is reduced, the motion inertia of the instrument arm is reduced, the elastic deformation of each component in the motion process is correspondingly reduced, and the repeated positioning precision of the tail end of a surgical tool is further improved; no part for transmission is arranged above the spherical surface of the expandable structure formed by the components of the mechanical arm, so that no extra motion inertia is generated in the motion process of the mechanical arm driving operation to be a fixed point, and the motion stability of the mechanical arm is improved.
It should also be noted that directional terms, such as "upper", "lower", "front", "rear", "left", "right", and the like, used in the embodiments are only directions referring to the drawings, and are not intended to limit the scope of the present disclosure. Throughout the drawings, like elements are represented by like or similar reference numerals. Conventional structures or constructions will be omitted when they may obscure the understanding of the present disclosure.
And the shapes and sizes of the respective components in the drawings do not reflect actual sizes and proportions, but merely illustrate the contents of the embodiments of the present disclosure. Furthermore, in the claims, any reference signs placed between parentheses shall not be construed as limiting the claim.
Unless otherwise indicated, the numerical parameters set forth in the specification and attached claims are approximations that can vary depending upon the desired properties sought to be obtained by the present disclosure. In particular, all numbers expressing quantities of ingredients, reaction conditions, and so forth used in the specification and claims are to be understood as being modified in all instances by the term "about". Generally, the expression is meant to encompass variations of ± 10% in some embodiments, 5% in some embodiments, 1% in some embodiments, 0.5% in some embodiments by the specified amount.
Furthermore, the word "comprising" does not exclude the presence of elements or steps not listed in a claim. The word "a" or "an" preceding an element does not exclude the presence of a plurality of such elements.
The use of ordinal numbers such as "first," "second," "third," etc., in the specification and claims to modify a corresponding element does not by itself connote any ordinal number of the element or any ordering of one element from another or the order of manufacture, and the use of the ordinal numbers is only used to distinguish one element having a certain name from another element having a same name.
In addition, unless steps are specifically described or must occur in sequence, the order of the steps is not limited to that listed above and may be changed or rearranged as desired by the desired design. The embodiments described above may be mixed and matched with each other or with other embodiments based on design and reliability considerations, i.e., technical features in different embodiments may be freely combined to form further embodiments.
Those skilled in the art will appreciate that the modules in the device in an embodiment may be adaptively changed and disposed in one or more devices different from the embodiment. The modules or units or components of the embodiments may be combined into one module or unit or component, and furthermore they may be divided into a plurality of sub-modules or sub-units or sub-components. All of the features disclosed in this specification (including any accompanying claims, abstract and drawings), and all of the processes or elements of any method or apparatus so disclosed, may be combined in any combination, except combinations where at least some of such features and/or processes or elements are mutually exclusive. Each feature disclosed in this specification (including any accompanying claims, abstract and drawings) may be replaced by alternative features serving the same, equivalent or similar purpose, unless expressly stated otherwise. Also in the unit claims enumerating several means, several of these means may be embodied by one and the same item of hardware.
Similarly, it should be appreciated that in the foregoing description of exemplary embodiments of the disclosure, various features of the disclosure are sometimes grouped together in a single embodiment, figure, or description thereof for the purpose of streamlining the disclosure and aiding in the understanding of one or more of the various disclosed aspects. However, the disclosed method should not be interpreted as reflecting an intention that: that is, the claimed disclosure requires more features than are expressly recited in each claim. Rather, as the following claims reflect, disclosed aspects lie in less than all features of a single foregoing disclosed embodiment. Thus, the claims following the detailed description are hereby expressly incorporated into this detailed description, with each claim standing on its own as a separate embodiment of this disclosure.
The above-mentioned embodiments are intended to illustrate the objects, aspects and advantages of the present disclosure in further detail, and it should be understood that the above-mentioned embodiments are only illustrative of the present disclosure and are not intended to limit the present disclosure, and any modifications, equivalents, improvements and the like made within the spirit and principle of the present disclosure should be included in the scope of the present disclosure.
Claims (10)
1. A deployable instrument arm, comprising:
the connecting part is of a telescopic structure and comprises a driving end and a driven end;
the control part is connected with the active end of the connecting part;
a far-end executing part, one end of which is connected with the driven end of the connecting part and the other end of which is connected with an executing mechanism;
the control part can control the connecting part to stretch and swing along a spherical surface, so that the actuating mechanism always points to the spherical center corresponding to the spherical surface.
2. The deployable instrument arm of claim 1, wherein the deployment control comprises:
the base is provided with a first driving rotating shaft and a second driving rotating shaft, and the axis of the first driving rotating shaft is superposed with the axis of the second driving rotating shaft;
the first driving rod comprises a first driving connecting end, and the first driving connecting end is fixedly connected with the first driving rotating shaft;
and the second driving rod comprises a third driving connecting end, and the third driving connecting end is fixedly connected with the second driving rotating shaft.
3. The deployable instrument arm of claim 1, wherein the distal implement comprises:
the instrument seat is provided with an instrument seat bracket;
a first driven link including a first driven connection end;
the second driven rod comprises a third driven connecting end;
the first driven connecting end and the third driven connecting end are pivoted to the instrument base support through a driven rotating shaft.
4. The deployable instrument arm of claim 3, further comprising a first auxiliary link pivotally connected at one end to an auxiliary link support, the auxiliary link support being fixedly connected to the connecting portion, and a second auxiliary link pivotally connected at one end to the instrument holder support, the other end of the first auxiliary link being pivotally connected to the other end of the second auxiliary link.
5. The deployable instrument arm of claim 1, wherein the active end comprises first and second deployment connection ends and the passive end comprises third and fourth deployment connection ends;
the first driving rod further comprises a second driving connecting end;
the second driving rod further comprises a fourth driving connecting end;
the first unfolding connecting end and the second active connecting end are pivoted through a first connecting rotating shaft;
the second unfolding connecting end and the fourth driving connecting end are pivoted through a fourth connecting rotating shaft;
the third unfolding connecting end and the second driven connecting end are pivoted through a third connecting rotating shaft;
and the fourth unfolding connecting end and the fourth driven connecting end are pivoted through a fourth connecting rotating shaft.
6. The deployable instrument arm of claim 5, wherein the connecting portion further comprises a first spherical link, a second spherical link, and a spherical connecting shaft pivotally connecting the first spherical link to the second spherical link, the spherical connecting shaft passing through a middle portion of the first spherical link and a middle portion of the second spherical link.
7. The deployable instrument arm of claim 6, wherein the first connecting pivot, the spherical connecting pivot, and the fourth connecting pivot intersect at a point.
8. The deployable instrument arm of claim 6, wherein the second connecting pivot, the spherical connecting pivot, and the third connecting pivot intersect at a point.
9. The deployable instrument arm of claim 6, wherein the radius of curvature of the first spherical link is equal to or greater than the radius of curvature of the second spherical link.
10. The deployable instrument arm of any one of claims 1 to 9, wherein the control unit further comprises a driving motor for driving the first active spindle and the second active spindle to rotate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110370008.7A CN113069209B (en) | 2021-04-06 | 2021-04-06 | Deployable instrument arm |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110370008.7A CN113069209B (en) | 2021-04-06 | 2021-04-06 | Deployable instrument arm |
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| CN113069209A true CN113069209A (en) | 2021-07-06 |
| CN113069209B CN113069209B (en) | 2023-02-21 |
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| CN202110370008.7A Active CN113069209B (en) | 2021-04-06 | 2021-04-06 | Deployable instrument arm |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113069210A (en) * | 2021-04-06 | 2021-07-06 | 天津大学医疗机器人与智能系统研究院 | Deployable instrument arm |
| CN113081277A (en) * | 2021-04-06 | 2021-07-09 | 天津大学医疗机器人与智能系统研究院 | Deployable instrument arm |
| CN114652451A (en) * | 2022-04-20 | 2022-06-24 | 天津大学医疗机器人与智能系统研究院 | Instrument arm driving device and instrument arm using same |
| CN114652452A (en) * | 2022-04-20 | 2022-06-24 | 天津大学医疗机器人与智能系统研究院 | From the operating end arm |
| CN114770457A (en) * | 2022-04-20 | 2022-07-22 | 天津大学医疗机器人与智能系统研究院 | Manipulator and slave operation end using same |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN113069210A (en) * | 2021-04-06 | 2021-07-06 | 天津大学医疗机器人与智能系统研究院 | Deployable instrument arm |
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| CN113069210B (en) * | 2021-04-06 | 2023-02-17 | 天津大学医疗机器人与智能系统研究院 | Deployable instrument arm |
| CN114652451A (en) * | 2022-04-20 | 2022-06-24 | 天津大学医疗机器人与智能系统研究院 | Instrument arm driving device and instrument arm using same |
| CN114652452A (en) * | 2022-04-20 | 2022-06-24 | 天津大学医疗机器人与智能系统研究院 | From the operating end arm |
| CN114770457A (en) * | 2022-04-20 | 2022-07-22 | 天津大学医疗机器人与智能系统研究院 | Manipulator and slave operation end using same |
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