CN118009209A - Stepless hovering support balanced by gravity - Google Patents
Stepless hovering support balanced by gravity Download PDFInfo
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- CN118009209A CN118009209A CN202410310929.8A CN202410310929A CN118009209A CN 118009209 A CN118009209 A CN 118009209A CN 202410310929 A CN202410310929 A CN 202410310929A CN 118009209 A CN118009209 A CN 118009209A
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- support
- joint
- bearing
- stepless
- gravity
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- 230000005484 gravity Effects 0.000 title claims abstract description 31
- 238000013016 damping Methods 0.000 claims abstract description 10
- 230000000694 effects Effects 0.000 abstract description 8
- 238000009434 installation Methods 0.000 abstract description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 210000001503 joint Anatomy 0.000 description 1
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Abstract
The invention relates to a stepless hovering support balanced by gravity, which is characterized in that: the device comprises a device support, a fixed hinge, a support bottom plate, an adjustable hinge, a support joint, a bearing, a rotating shaft, a guide rod, a driving shaft and a disc spring, wherein the fixed hinge is used for connecting the device support with the upper end of the support joint, the adjustable hinge is arranged in an inner hole of the support bottom plate, the head of the adjustable hinge is fixed on one side of the lower end of the support joint, the bearing is arranged in an inner hole of the other side of the support bottom plate, the bearing is pressed through the rotating shaft and is fixed on the other side of the lower end of the support joint, the guide rod is connected with the lower end of the support joint through the driving shaft, and the disc spring is stacked and sleeved on the guide rod. The disc springs are arranged in the support, the moment provided by the disc springs is balanced with the moment generated by the gravity of the product, and meanwhile, the damping effect of the small-torque hinge can not reset or shift the support, so that the hovering effect is achieved. The support can be easily adjusted at any angle, so that a user can freely adjust the support to a comfortable angle. Because the disc spring has the characteristics of simple structure, compact size and large bearing capacity, the bracket is convenient to use, and the required installation space is smaller, so that the universality is strong.
Description
Technical Field
The invention relates to a stepless hovering support balanced by gravity, belonging to the technical field of gravity balance mechanisms.
Background
At present, an existing electronic equipment bracket is required to hover at a certain position, and hinges with different torque magnitudes are used for counteracting moment generated by gravity. However, as the bracket hover angle decreases, the moment arm of gravity increases, which results in a desire to hover at a low angle position, with the corresponding high torque hinge being selected to balance. When the equipment support rotates from a small angle to a large angle, the force required to be applied is larger than the force of gravity plus the force of the large torque hinge, so that the equipment support can rotate, the equipment support is not friendly to a user, the angle of the equipment support cannot be freely adjusted, and the equipment support is inconvenient to use.
In order to solve the problems, a stepless hovering support which is balanced by gravity is designed, so that the stepless hovering support can be easily adjusted at any angle, and a user can freely adjust the support to a comfortable angle. The disc springs are arranged in the support, the moment provided by the disc springs is balanced with the moment generated by the gravity of the product, and meanwhile, the damping effect of the low-torque hinge can not reset or shift the support, so that the stepless hovering effect is achieved. Because the disc spring has the characteristics of simple structure, compact size and large bearing capacity, the bracket is convenient to use, and the required installation space is smaller, so that the universality is strong.
Disclosure of Invention
Aiming at the problems of inconvenient use and difficult angle adjustment in the background technology, the invention provides a stepless hovering support which relies on gravity balance.
In order to achieve the above purpose, the present invention adopts the following technical scheme:
The utility model provides a rely on gravity balance's stepless support of hovering, includes equipment support, fixed hinge, support bottom plate, adjustable hinge, support joint, bearing, axis of rotation, guide bar, drive axle, dish spring, fixed hinge links to each other equipment support and support joint upper end, adjustable hinge is placed in the hole of support bottom plate, and adjustable hinge head is fixed in support joint lower extreme one side, the bearing is placed in support bottom plate opposite side hole, compresses tightly and the axis of rotation is fixed with support joint lower extreme opposite side through the axis of rotation, the guide bar passes through the drive axle and links to each other with support joint lower extreme, dish spring stacks the cover on the guide bar.
Preferably, through holes are formed in the upper ends of the equipment support and the support joint, and the fixing hinge penetrates through the through holes of the support joint and the equipment support to connect the equipment support and the support joint and is fixed through a set screw.
Preferably, an arc-shaped inner hole is formed in one side of the support base plate, and the adjustable hinge is placed in the arc-shaped hole.
Preferably, the adjustable hinge head is provided with an opening, one side of the lower end of the bracket joint is provided with a threaded hole, the adjustable hinge is connected with the bracket joint through a screw, the adjustable hinge can adjust the damping, and the bracket joint has a damping effect during rotation.
Preferably, the bearing is placed in the inner hole at the other side of the bottom plate of the bracket, and the bearing is pressed tightly through the inner hole of the bearing by the rotating shaft.
Preferably, the rotating shaft penetrates through the bearing and is inserted into the inner hole of the joint of the bracket, a threaded hole is formed in the other side of the lower end of the joint of the bracket, the fastening screw is used for fixing the rotating shaft through the threaded hole, and the rotating shaft can drive the bearing inner ring to rotate along with the joint bracket.
Preferably, the driving shaft penetrates through the guide rod and the inner hole of the bracket joint to connect the guide rod and the bracket joint, the bracket joint is provided with a threaded hole, and the set screw is used for fixing the driving shaft through the threaded hole.
Preferably, the guide rod passes through the opening at the bottom of the bottom plate of the bracket, and the disc springs are stacked according to a certain rule and sleeved on the guide rod.
Preferably, the rotation of the joint support can drive the guide rod to move in the vertical direction, and the disc springs can be compressed to different degrees according to the rotation angle of the joint support.
Preferably, the bearing is a rotating fulcrum, the bracket joint is a lever, one end of the lever is a product, the other end of the lever is a disc spring, the moment of the disc spring can be changed along with moment change generated by gravity of the product, and the damping value of the adjustable hinge can compensate moment difference between the disc spring and the dead weight of the product, so that the gravity balance effect is realized.
Compared with the prior art, the invention has the following beneficial effects:
(1) The use is convenient: the moment balance is realized by utilizing the disc spring, so that the joint support can apply a small force to realize rotation at any angle.
(2) The space is compact: the support can utilize smaller space according to the characteristics of the disc spring to provide enough force to balance with the dead weight of the equipment.
(3) The universality is strong: the damping of the bracket hinge can be adjusted, and the bracket hinge can be matched with a disc spring to be suitable for most display screens, tablet computers, industrial monitors and the like on the market.
Drawings
Fig. 1 is a schematic diagram of an overall structure of an electronic device according to an embodiment of the present invention
Fig. 2 is a schematic back view of an electronic device according to an embodiment of the present invention
FIG. 3 is a schematic structural view of a gravity-balanced stepless hovering support according to an embodiment of the invention
FIG. 4 is a cross-sectional view of a gravity-balanced stepless hover support provided by an embodiment of the invention
FIG. 5 is a schematic diagram of moment balance according to an embodiment of the present invention
FIG. 6 is a graph illustrating an analysis of a gravity balance curve according to an embodiment of the present invention
Marked in the figure as: 10-equipment support, 11-fixed hinge, 20-support joint, 21-groove, 22-joint decorative cover, 30-support bottom plate, 40-adjustable hinge, 50-driving shaft, 51-guide rod, 52-guide barrel, 53-disc spring, 60-bearing and 61-rotating shaft.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
In one embodiment of the present invention, as shown in fig. 1 to 4, there is provided a gravity-balanced stepless hovering support, comprising a device support 10, a fixed hinge 11, a support base 30, an adjustable hinge 40, a support joint 20, a bearing 60, a rotation shaft 61, a guide rod 51, a driving shaft 50, a disc spring 53, etc.
In this embodiment, as shown in fig. 2, the display screen comprises a device bracket 10, the device bracket 10 is fixed with the display screen through screws, the device bracket 10 is connected with a bracket joint 20 through two symmetrical fixed hinges 11, the hinges have damping effect, and at the moment, the display screen can realize rotation and hovering by taking the fixed hinges 11 as the center. The bracket joint 20 is provided with the groove 21, the groove 21 can facilitate the wiring of the display screen cable, and the joint decorative cover 22 can be arranged on the bracket joint 20 to achieve the beautiful effect.
In this embodiment, as shown in fig. 3, the lower end of the joint support 20 is connected to the support bottom plate 30, both sides of the support bottom plate 30 are provided with inner holes, wherein the outer dimensions of the inner hole on one side are identical to those of the adjustable hinge 40, the adjustable hinge 40 is placed in the inner hole of the support bottom plate 30, and the other end of the adjustable hinge 40 is provided with an opening, and is fixed with the joint support 20 by a screw. The adjustable hinge 40 can adjust the damping according to the dead weight of the product, and the joint support 20 can drive the adjustable hinge 40 to rotate.
In this embodiment, as shown in fig. 4, the bearing 60 is placed in the inner hole on the other side of the bracket base plate 30, and the rotation shaft 61 passes through the inner hole of the bearing 60 and the inner hole of the bracket joint 20 and is fixed to the bracket joint 20 by a set screw. The bearing 60 serves as a support, and the inner race is rotatable with the knuckle mount 20. The disc springs 53 are arranged on the side of the bearing 60 at the same time, the concave surface of the uppermost disc spring 53 is upward, the concave surfaces of the middle five pairs of disc springs 53 are opposite to the concave surfaces, the concave surfaces of the lowermost disc spring 53 are downward, and the disc springs 53 are stacked on the guide rod 51 in a butt joint mode, and the outer side of the disc springs 53 is sleeved with a guide barrel to play a guide role. The disc springs can be selected to have proper number of pieces and combination mode according to the compression deformation and the required spring load value. The guide rod 51 sleeved with the disc spring 53 passes through the bottom opening of the bracket bottom plate 30, the upper end hole position of the guide rod is aligned with the opening of the joint bracket 20, the rotating shaft 61 sequentially passes through the inner hole of the joint bracket 20, the inner hole of the guide rod 51 and the inner hole of the joint bracket 20, and finally the rotating shaft 61 is fixed with the joint bracket 20 through the set screw.
In this embodiment, as shown in fig. 5, a lever mechanism is formed in which the bearing 60 is used as a pivot, and the bracket joint 20 is used as a lever. Wherein one end of the lever is the product gravity G, and the other end is the reaction force of the guide rod 51 moving vertically to compress the disc spring 53 plus the resultant force F provided by the adjustable hinge 40. When the balance is realized at the two ends of the lever, the resultant moment of the fulcrum is 0, namely the moment formed by the resultant force F is equal to the moment formed by the product gravity G in magnitude and opposite in direction, a formula of FxL=GxL 2 can be obtained, and meanwhile, according to a trigonometric function L 2=L1 xcos theta, a formula of F= (GxL 1 xcos theta)/L is finally obtained, wherein L, L 1 and G are constants, and theta is a variable. From the above formula and the characteristic curve of the disc spring, a bracket gravity balance fitting curve is drawn as shown in fig. 6, wherein the abscissa θ is the rotation angle of the joint bracket 20, which corresponds to the deformation of the disc spring, and the ordinate is the load. It can be seen that there is a difference Δf between the function curve of the resultant force F and the characteristic curve of the disc spring, Δf being compensated by the damping value of the adjustable hinge 40, when the disc spring load plus Δf is equal to the resultant force F, the resultant moment at the pivot point is 0, i.e. the bracket achieves gravity balance.
In this embodiment, the large torque hinge is not required to balance gravity, and the disc spring 53 can provide a large force in a small space. When the knuckle mount 20 is at a small angle, the disc spring 53 is less compressed and provides relatively little force, and the moment provided by the adjustable hinge 40 is added to achieve gravitational equilibrium. When the joint support 20 rotates to a large angle, the deformation amount of the disc spring 53 subjected to compression is correspondingly increased, the reaction force is larger, gravity balance can be realized by adding the moment provided by the adjustable hinge 40, and the joint support 20 can be pushed to rotate by only needing a small force, so that hovering at different angles is realized, and the use is convenient.
The foregoing description is only a preferred embodiment of the present invention, and the present invention is not limited thereto, but it is to be understood that modifications and equivalents of some of the technical features described in the foregoing embodiments may be made by those skilled in the art, although the present invention has been described in detail with reference to the foregoing embodiments. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (8)
1. A gravity balanced stepless hover support characterized by: the device comprises a device support, a fixed hinge, a support bottom plate, an adjustable hinge, a support joint, a bearing, a rotating shaft, a guide rod, a driving shaft and a disc spring, wherein the fixed hinge is used for connecting the device support with the upper end of the support joint, the adjustable hinge is arranged in an inner hole of the support bottom plate, the head of the adjustable hinge is fixed on one side of the lower end of the support joint, the bearing is arranged in an inner hole of the other side of the support bottom plate, the bearing is pressed through the rotating shaft and is fixed on the other side of the lower end of the support joint, the guide rod is connected with the lower end of the support joint through the driving shaft, and the disc spring is stacked and sleeved on the guide rod.
2. The gravity balanced stepless hover support according to claim 1, characterized in that: the device support and the upper end of the support joint are provided with through holes, and the fixed hinge penetrates through the through holes of the support joint and the device support to connect the support joint and the device support and is fixed by a set screw.
3. The gravity balanced stepless hover support according to claim 1, characterized in that: the adjustable hinge is characterized in that an arc inner hole is formed in one side of the support bottom plate, the adjustable hinge is arranged in the arc inner hole, an opening is formed in the head of the adjustable hinge, a threaded hole is formed in one side of the lower end of the support joint, and the adjustable hinge is connected with the support joint through a screw.
4. The gravity balanced stepless hover support according to claim 1, characterized in that: the bearing is placed in the inner hole at the other side of the bottom plate of the bracket, and the rotating shaft penetrates through the inner hole of the bearing to compress the bearing.
5. The gravity balanced stepless hover support according to claim 1, characterized in that: the rotating shaft penetrates through the bearing and is inserted into the inner hole of the bracket joint, a threaded hole is formed in the other side of the lower end of the bracket joint, and the fastening screw is used for fixing the rotating shaft through the threaded hole.
6. The gravity balanced stepless hover support according to claim 1, characterized in that: the driving shaft penetrates through the guide rod and the inner hole of the bracket joint to connect the guide rod and the bracket joint, the bracket joint is provided with a threaded hole, and the set screw fixes the driving shaft through the threaded hole.
7. The gravity balanced stepless hover support according to claim 1, characterized in that: the guide rod penetrates through the opening at the bottom of the support bottom plate, the disc springs are stacked according to a certain rule, and the disc springs are sleeved on the guide rod.
8. The gravity balanced stepless hover support according to claim 1, characterized in that: the bearing is a rotating fulcrum, the bracket joint is a lever, one end of the lever is a product, the other end of the lever is a disc spring, and the moment generated by the disc spring and the moment generated by the gravity of the product can be balanced by the damping value compensation disc spring of the adjustable hinge.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202410310929.8A CN118009209A (en) | 2024-03-19 | 2024-03-19 | Stepless hovering support balanced by gravity |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202410310929.8A CN118009209A (en) | 2024-03-19 | 2024-03-19 | Stepless hovering support balanced by gravity |
Publications (1)
Publication Number | Publication Date |
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CN118009209A true CN118009209A (en) | 2024-05-10 |
Family
ID=90944586
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202410310929.8A Pending CN118009209A (en) | 2024-03-19 | 2024-03-19 | Stepless hovering support balanced by gravity |
Country Status (1)
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CN (1) | CN118009209A (en) |
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2024
- 2024-03-19 CN CN202410310929.8A patent/CN118009209A/en active Pending
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