CN118107825A - Mechanical arm joint loosening-stopping and folding structure - Google Patents
Mechanical arm joint loosening-stopping and folding structure Download PDFInfo
- Publication number
- CN118107825A CN118107825A CN202310821536.9A CN202310821536A CN118107825A CN 118107825 A CN118107825 A CN 118107825A CN 202310821536 A CN202310821536 A CN 202310821536A CN 118107825 A CN118107825 A CN 118107825A
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- assembly
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- horn
- rotating shaft
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- 230000006835 compression Effects 0.000 claims description 21
- 238000007906 compression Methods 0.000 claims description 21
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical group O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 16
- 230000002265 prevention Effects 0.000 claims description 14
- 235000008331 Pinus X rigitaeda Nutrition 0.000 claims 1
- 235000011613 Pinus brutia Nutrition 0.000 claims 1
- 241000018646 Pinus brutia Species 0.000 claims 1
- 239000000306 component Substances 0.000 description 11
- 239000003292 glue Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000008358 core component Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The invention discloses a mechanical arm joint loosening-stopping and folding structure which comprises a center disc cantilever assembly, a mechanical arm folding assembly and a thread sleeve assembly. According to the invention, the threaded sleeve is tightly matched with the central disc inner part, and the threaded sleeve presses the horn inner part, so that the horn folding assembly and the central disc cantilever assembly are firmly connected, and meanwhile, the designed threaded sleeve loosening stopping assembly can stop loosening of the threaded sleeve assembly, so that the flight safety and reliability of the unmanned aerial vehicle are improved. According to the folding transfer device, the first rotating shaft pin and the second rotating shaft pin which are connected with the folding transfer piece are rotated around the shaft twice, so that the folding transfer device can not interfere with other components of the unmanned aerial vehicle when the folding transfer device is folded, and can be folded to the designed minimum storage size space without increasing the structural weight and the complexity.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a mechanical arm joint loosening-stopping and folding structure.
Background
Unmanned aerial vehicles have obtained wide application in various fields such as entertainment consumption, agriculture and forestry plant protection, inspection and mapping, security protection, emergency rescue, engineering monitoring, etc. The horn joint connection spare is the core component of unmanned aerial vehicle horn connection center dish, and its design is reliable and the dismouting folding accomodate of being convenient for, is unmanned aerial vehicle structural design's difficult point and pain point historically. Traditional thread bush subassembly mode connection structure can let horn and central disk connect firmly, but hardly locking, and when folding simultaneously, can only be in a direction, is difficult for keeping away the position, when need keep away the position, need misplaced front and back horn mounting structure, increase size space, structure weight and complexity.
Disclosure of Invention
The invention aims to solve the technical problem of providing a mechanical arm joint loosening prevention and folding structure which can realize stable connection of mechanical arm and central disc installation and loosening prevention, and can realize front-back misplacement of a folding mechanical arm installation structure.
In order to solve the above problems, the present invention provides a mechanical arm joint loosening and folding structure, comprising:
The center plate cantilever assembly comprises a center plate cantilever beam, a thread sleeve loosening prevention assembly and a center plate inner piece; a limiting groove and a guide pin hole are formed in the center of the upper part of the center disc cantilever beam, close to the edge; the thread sleeve loosening prevention assembly is arranged on a cavity structure formed by the limiting groove and the guide pin hole; the center plate inner piece is adhered to the inner surface of the center plate cantilever beam;
The folding assembly of the horn comprises a horn, a horn inner part, a first rotating shaft pin, a folding adapter, a second rotating shaft pin and a guide pin; the horn is adhered to the horn inner part; the inner part of the horn is provided with an adapter mounting boss, a guide post and an arc-shaped boss; the folding adapter is provided with a first rotating shaft body and a second rotating shaft body, and the first rotating shaft body is connected with the adapter mounting boss through a first rotating shaft pin; the guide pin is provided with a guide pin cylinder and a guide pin limiting table, and the guide pin cylinder is connected with the second rotating shaft body through a second rotating shaft pin;
The thread sleeve assembly comprises a thread sleeve member and a silica gel ring; the external part of the thread sleeve is provided with an annular groove and an lug, the internal part of the thread sleeve is provided with an internal thread, the annular groove is used for installing a silica gel ring, and the lug is used for increasing the rotation torque of the thread sleeve, so that the thread sleeve can be conveniently screwed and unscrewed;
When the internal threads arranged on the thread sleeve member are matched with the external threads arranged on the central disc internal member, the thread sleeve member correspondingly compresses the horn internal member, so that the horn folding assembly and the central disc cantilever assembly are connected and fixed.
Further, the thread bushing loosening prevention assembly comprises a sliding pin, a compression spring and an extension pin; the sliding pin is provided with a handle, a limiting boss and a pin, the pin is partially installed in the guide pin hole, the compression spring is sleeved on the pin, one end of the compression spring is limited by the guide pin hole, and the extension pin is connected with the external thread of the pin through an inner threaded hole of an extension pin body, so that the other end of the compression spring is limited.
Further, the extension pin is provided with a clamping plane and an antenna column for clamping and tightening by a tool when the extension pin is connected with a pin.
Further, when the limit boss is matched with the limit groove, the compression spring is in a tensioning state, and the feeler column is in compression fit with the knurled groove formed in the silica gel ring so as to prevent the silica gel ring from rotating and further prevent the screw sleeve from loosening.
Further, when the thread sleeve member is required to be disassembled and loosened, the handle is shifted, the sliding pin is retracted and rotated for a certain angle, the limiting boss is separated from the limiting groove in a staggered mode, the compression spring is in a compression state, the feeler column is separated from the silica gel ring, the lug arranged on the thread sleeve member is held, and the thread sleeve member is rapidly disassembled.
Further, a guide post hole matched with the guide post is formed in the center plate inner piece, and when the guide post is matched with the guide post hole, the rotation of the horn inner piece can be limited.
Further, when the arm folding assembly is withdrawn, the guide pin slides outwards until the guide pin limiting table is matched with the limiting notch of the guide pin hole so as to limit the rotation of the guide pin.
Further, the first rotating shaft body and the second rotating shaft body are different from each other, and an angle theta is formed between the first rotating shaft body and the second rotating shaft body.
Further, when the horn folding assembly is folded, the horn folding assembly rotates around the second rotating shaft pin by an angle theta 1, and the axis of the horn folding assembly and the axis of the center disc cantilever assembly are positioned on the same plane; when the horn folding assembly rotates around the first rotating shaft pin by an angle theta 2, the axis of the horn folding assembly and the axis of the center disc cantilever assembly are different from each other.
Compared with the prior art, the invention has the following beneficial effects:
The thread sleeve is tightly matched with the central disc internal part, and the thread sleeve compresses the horn internal part, so that the horn folding assembly and the central disc cantilever assembly are firmly connected, and meanwhile, the thread sleeve loosening stopping assembly can stop loosening of the thread sleeve assembly, so that the flight safety and reliability of the unmanned aerial vehicle are improved; according to the folding assembly of the horn, through the two times of pivoting of the first rotating shaft pin and the second rotating shaft pin which are connected with the folding adapter, the angles are respectively theta 1 and theta 2, so that the folding assembly of the horn is not interfered with other assemblies of the unmanned aerial vehicle when being folded, and can be folded to the designed minimum storage size space without increasing the structural weight and complexity.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings required for the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present application, and other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic view of an overall assembly of an embodiment of the present invention;
FIG. 2 is a schematic diagram of the assembly of components of an embodiment of the present invention;
FIG. 3 is a schematic view of an overall assembly cut-away view of an embodiment of the present invention;
FIG. 4 is a partially expanded schematic illustration of a component of an embodiment of the invention;
FIG. 5 is an expanded schematic view of a center plate cantilever assembly and a threaded sleeve assembly according to an embodiment of the present invention;
FIG. 6 is an expanded schematic view of a threaded sleeve loosening prevention assembly according to an embodiment of the present invention;
FIG. 7 is a schematic view of the center plate cantilever beam of FIG. 6;
FIG. 8 is a schematic view of a folding assembly of a horn according to an embodiment of the present invention;
FIG. 9 is a schematic view of a folding adapter according to an embodiment of the present invention;
fig. 10 is a schematic diagram of a folding state of a folding assembly of a horn according to an embodiment of the present invention.
Reference numerals illustrate: the device comprises a10 central disc cantilever component, a 20 horn folding component, a 30 thread bush component, a 11 central disc cantilever beam, a 12 thread bush loosening stopping component, a 13 central disc inner component, a 1101 limit groove, a 1102 guide pin hole, a 121 sliding pin, a 122 compression spring, a 123 extension pin, a 1211 handle, a 1212 limit boss, a 1213 pin, a 1231 extension pin column, a 1232 contact angle column, a 1233 clamping plane, a 21 horn, a 22 horn inner component, a 23 first rotating shaft pin, a 24 folding adapter, a 25 second rotating shaft pin, a 26 guide pin, a 221 adapter mounting boss, a 222 guide column, a 223 arc-shaped boss, a 241 first rotating shaft body, a 242 second rotating shaft body, a 261 guide pin column, a 262 guide pin limit table, a 31 thread sleeve, a 32 silica gel ring, a 3101 annular groove and a 3102 lug.
Detailed Description
The following description of the embodiments of the present application will be made clearly and fully with reference to the accompanying drawings, in which it is evident that the embodiments described are some, but not all embodiments of the application. All other embodiments, which can be made by those skilled in the art based on the embodiments of the application without making any inventive effort, are intended to be within the scope of the application.
It should be understood that the terms "comprises" and "comprising," when used in this specification and the appended claims, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof.
It is also to be understood that the terminology used in the description of the application is for the purpose of describing particular embodiments only and is not intended to be limiting of the application. As used in this specification and the appended claims, the singular forms "a," "an," and "the" are intended to include the plural forms as well, unless the context clearly indicates otherwise.
It should be further understood that the term "and/or" as used in the present specification and the appended claims refers to any and all possible combinations of one or more of the associated listed items, and includes such combinations.
As shown in fig. 1-10, the present embodiment provides a joint loosening and folding structure of a horn, which includes a center plate cantilever assembly 10, a horn folding assembly 20 and a thread bush assembly 30. Wherein the center plate cantilever assembly 10 and the threaded sleeve assembly 30 are assembled together by the horn fold assembly 20 (see fig. 1, 2).
Wherein the center plate cantilever assembly 10 comprises a center plate cantilever beam 11, a threaded sleeve loosening prevention assembly 12 and a center plate inner member 13.
The center of the upper part of the center plate cantilever beam 11 is provided with a limit groove 1101 and a guide pin hole 1102 near the edge, a thread bushing loosening prevention assembly 12 is arranged on a cavity structure formed by the limit groove 1101 and the guide pin hole 1102, and a center plate inner piece 13 is adhered to the inner surface of the center plate cantilever beam 11 through glue (see fig. 6).
The threaded sleeve stop assembly 12 includes a slide pin 121, a compression spring 122, and an extension pin 123 (see fig. 5). The sliding pin 121 is provided with a handle 1211, a limit boss 1212 and a pin 1213, the pin 1213 of the sliding pin 121 is partially installed in the guide pin hole 1102, the compression spring 122 is sleeved on the pin 1213, one end of the compression spring 122 is limited by the guide pin hole 1102, the extension pin 123 is connected with the external thread of the pin 1213 through an internal thread hole of the arranged extension pin cylinder 1231, thereby limiting the other end of the compression spring 122, the extension pin 123 is additionally provided with a clamping plane 1233 for clamping and tightening by a tool when being connected with the pin 1213, and the extension pin 123 is also provided with an antenna post 1232 (see fig. 6).
The inner part 13 of the central disc is internally provided with a guide post hole 131 and a guide pin hole 132, the guide pin hole 132 is provided with a limit notch, the outer part is provided with external threads, and the inner part 13 of the central disc is adhered to the cantilever beam 11 of the central disc through glue (see fig. 8).
The horn folding assembly 20 includes a horn 21, a horn inner 22, a first pivot pin 23, a folding adaptor 24, a second pivot pin 25, and a guide pin 26, and the horn 21 is adhered to the horn inner 22 by glue (see fig. 4).
Specifically, the horn inner 22 is provided with an adapter mounting boss 221, a guide post 222 and an arc-shaped boss 223;
The folding adaptor 24 is provided with a first rotating shaft body 241 and a second rotating shaft body 242, the first rotating shaft body 241 and the second rotating shaft body 242 are different surfaces, and the first rotating shaft body 241 arranged on the folding adaptor 24 is connected with the adaptor mounting boss 221 of the arm inner part 22 through the first rotating shaft pin 23;
the guide pin 26 is provided with a guide pin cylinder 261 and a guide pin stopper 262, and the guide pin cylinder 261 is connected with a second rotation shaft body 242 provided to the folder 24 through a second rotation shaft pin 25 (see fig. 8).
The thread bush assembly 30 comprises a thread bush 31 and a silica gel ring 32. The thread sleeve 31 is externally provided with an annular groove 3101 and a lug 3102, and internally provided with an internal thread, the annular groove 3101 is used for mounting the silica gel ring 32, and the lug 3102 is used for increasing the rotation torque of the thread sleeve 31, so as to facilitate screwing and unscrewing of the thread sleeve 31 (see fig. 5).
In this embodiment, referring to fig. 1 and 2, when the internal threads provided by the thread set 31 are mated with the external threads provided by the center plate internal member 13, the thread set 31 compresses the horn internal member 22, thereby securing the horn folding assembly 20 in connection with the center plate cantilever assembly 10.
In this embodiment, referring to fig. 3, 5 and 6, when the limit boss 1212 provided at the sliding pin 121 of the thread sleeve loosening prevention assembly 12 is matched with the limit groove 1101, the compression spring 122 is in a tensioning state, and the feeler post 1232 on the extension pin 123 is in press fit with the knurled groove provided on the silica gel ring 32 of the tightened thread sleeve assembly 30, so as to prevent the silica gel ring 32 from rotating, and further prevent the loosening of the thread sleeve 31.
In this embodiment, referring to fig. 5 and 6, when the screw sleeve 31 needs to be disassembled and loosened, the handle 1211 of the sliding pin 121 is shifted, so that the sliding pin 121 is retracted and rotated by a certain angle, the limit boss 1212 is separated from and staggered with the limit groove 1101, the compression spring 122 is in a compressed state capable of maintaining greater deformation, the antenna post 1232 on the extension pin 123 is separated from the silica gel ring 32, and the lug 3102 arranged on the screw sleeve 31 is held, so that the screw sleeve 31 is quickly disassembled.
In this embodiment, referring to fig. 8, the guide post 222 of the inner part 22 of the arm is matched with the guide post hole 131 of the inner part 13 of the central disc to limit the rotation of the inner part 22 of the arm, and the arc-shaped boss 223 is matched with the inner surface of the inner part 13 of the central disc to guide and increase the force contact surface.
In this embodiment, referring to fig. 8, when the arm-folding assembly 20 is to be withdrawn, the guide pins 26 slide outwardly until the guide pin stop 262 is positioned to mate with the stop notch positioned in the guide pin aperture 132 of the hub inner member 13 to limit the rotation of the guide pins 26.
In the present embodiment, referring to fig. 9, the first rotating shaft body 241 and the second rotating shaft body 242 of the folding adapter 24 are different from each other and form an angle θ.
In this embodiment, referring to fig. 10, when the horn folding assembly 20 is to be folded, the axis of the horn folding assembly 20 and the axis of the center disk cantilever assembly 10 are still in the same plane by rotating the horn folding assembly 20 around the second rotation axis pin 25 by an angle θ 1, and when the horn folding assembly 20 is rotated around the first rotation axis pin 23 by an angle θ 2 again, the axis of the horn folding assembly 20 and the axis of the center disk cantilever assembly 10 are different from each other, so that the horn folding assembly 20 is folded without interfering with other components of the unmanned aerial vehicle and can be folded into the designed minimum storage size space.
In summary, the thread sleeve is tightly matched with the central disc inner part, and the thread sleeve presses the horn inner part, so that the horn folding assembly and the central disc cantilever assembly are firmly connected, and meanwhile, the designed thread sleeve loosening stopping assembly can stop loosening of the thread sleeve assembly, so that the flight safety and reliability of the unmanned aerial vehicle are improved.
The embodiments of the invention have been described in detail above, but they are merely examples, and the invention is not limited to the embodiments described above. It will be apparent to those skilled in the art that any equivalent modifications or substitutions to this invention are within the scope of the invention, and therefore, all equivalent changes and modifications, improvements, etc. that do not depart from the spirit and scope of the principles of the invention are intended to be covered by this invention.
Claims (9)
1. The utility model provides a horn joint ends pine and beta structure which characterized in that includes:
A center plate cantilever assembly (10), wherein the center plate cantilever assembly (10) comprises a center plate cantilever beam (11), a thread sleeve loosening prevention assembly (12) and a center plate inner piece (13); a limiting groove (1101) and a guide pin hole (1102) are formed in the center of the upper part of the center disc cantilever beam (11) close to the edge; the thread sleeve loosening prevention assembly (12) is arranged on a cavity structure formed by a limit groove (1101) and a guide pin hole (1102); the center disc inner piece (13) is adhered to the inner surface of the center disc cantilever beam (11);
The folding device comprises a horn folding assembly (20), wherein the horn folding assembly (20) comprises a horn (21), a horn inner piece (22), a first rotating shaft pin (23), a folding adapter (24), a second rotating shaft pin (25) and a guide pin (26); the horn (21) is adhered to the horn inner piece (22); the arm inner piece (22) is provided with an adapter mounting boss (221), a guide column (222) and an arc-shaped boss (223); the folding adapter (24) is provided with a first rotating shaft body (241) and a second rotating shaft body (242), and the first rotating shaft body (241) is connected with the adapter mounting boss (221) through a first rotating shaft pin (23); the guide pin (26) is provided with a guide pin cylinder (261) and a guide pin limiting table (262), and the guide pin cylinder (261) is connected with the second rotating shaft body (242) through a second rotating shaft pin (25);
A thread bush assembly (30), wherein the thread bush assembly (30) comprises a thread bush (31) and a silica gel ring (32); an annular groove (3101) and lugs (3102) are arranged on the outer portion of the thread sleeve (31), internal threads are arranged in the annular groove (3101) and used for installing a silica gel ring (32), and the lugs (3102) are used for increasing the rotation torsion of the thread sleeve (31) so as to facilitate screwing and unscrewing of the thread sleeve (31);
When the internal threads arranged on the thread sleeve member (31) are matched with the external threads arranged on the central disc inner member (13), the thread sleeve member (31) correspondingly presses the horn inner member (22), so that the horn folding assembly (20) and the central disc cantilever assembly (10) are connected and fixed.
2. The arm joint loosening and folding structure of claim 1, wherein the threaded sleeve loosening prevention assembly (12) comprises a sliding pin (121), a compression spring (122) and an extension pin (123); the sliding pin (121) is provided with a handle (1211), a limit boss (1212) and a pin (1213), the pin (1213) is partially installed in the guide pin hole (1102), the compression spring (122) is sleeved on the pin (1213), one end of the compression spring (122) is limited by the guide pin hole (1102), and the extension pin (123) is connected with the external thread of the pin (1213) through an internal thread hole of the extension pin column (1231) so as to limit the other end of the compression spring (122).
3. The arm joint loosening and folding structure of claim 2, wherein the extension pin (123) is provided with a clamping plane (1233) and an antenna post (1232) for clamping up with a tool when connected with the pin (1213).
4. The arm joint loosening prevention and folding structure according to claim 3, wherein when the limit boss (1212) is matched with the limit groove (1101), the compression spring (122) is in a tensioning state, and the antenna post (1232) is in press fit with a knurled groove provided on the silica gel ring (32) so as to prevent the silica gel ring (32) from rotating, thereby preventing loosening of the thread sleeve (31).
5. The arm joint loosening prevention and folding structure according to claim 3, wherein when the screw thread sleeve (31) needs to be disassembled and loosened, the handle (1211) is shifted, the sliding pin (121) is retracted and rotated for a certain angle, the limit boss (1212) is separated from the limit groove (1101) and staggered, the compression spring (122) is in a state capable of being kept compressed, the antenna post (1232) is separated from the silica gel ring (32), and the lug (3102) arranged on the screw thread sleeve (31) is held, so that the screw thread sleeve (31) is quickly disassembled.
6. A horn joint loosening and folding structure as claimed in claim 3, characterized in that the central disc inner member (13) is provided with a guide post hole (131) for cooperation with the guide post (222), the rotation of the horn inner member (22) being limited when the guide post (222) is in cooperation with the guide post hole (131).
7. A horn joint loosening and folding structure as claimed in claim 3, characterized in that when the horn folding assembly (20) is withdrawn, the guide pins (26) slide outwards until the guide pin stop (262) cooperates with the stop notches of the guide pin holes (132) to limit the rotation of the guide pins (26).
8. The arm joint loosening and folding structure according to claim 3, wherein the first rotating shaft body (241) and the second rotating shaft body (242) are different surfaces, and an angle θ is formed between the two.
9. The arm joint loosening and folding structure according to claim 8, wherein when the arm folding assembly (20) is folded, the arm folding assembly (20) rotates by an angle θ 1 about the second rotation shaft pin (25), and the axis of the arm folding assembly (20) and the axis of the center disc cantilever assembly (10) are in the same plane; when the arm folding assembly (20) rotates by an angle theta 2 around the first rotating shaft pin (23), the axis of the arm folding assembly (20) and the axis of the center disc cantilever assembly (10) are different from each other.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202310821536.9A CN118107825A (en) | 2023-07-06 | 2023-07-06 | Mechanical arm joint loosening-stopping and folding structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202310821536.9A CN118107825A (en) | 2023-07-06 | 2023-07-06 | Mechanical arm joint loosening-stopping and folding structure |
Publications (1)
Publication Number | Publication Date |
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CN118107825A true CN118107825A (en) | 2024-05-31 |
Family
ID=91216114
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202310821536.9A Pending CN118107825A (en) | 2023-07-06 | 2023-07-06 | Mechanical arm joint loosening-stopping and folding structure |
Country Status (1)
Country | Link |
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CN (1) | CN118107825A (en) |
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2023
- 2023-07-06 CN CN202310821536.9A patent/CN118107825A/en active Pending
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