CN203638105U - Damping ball - Google Patents
Damping ball Download PDFInfo
- Publication number
- CN203638105U CN203638105U CN201420015975.7U CN201420015975U CN203638105U CN 203638105 U CN203638105 U CN 203638105U CN 201420015975 U CN201420015975 U CN 201420015975U CN 203638105 U CN203638105 U CN 203638105U
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- CN
- China
- Prior art keywords
- shock
- absorbing ball
- buffer part
- adapter plate
- offset plate
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Abstract
The utility model discloses a damping ball. The damping ball comprises a cylindrical body, an upper buffer portion and a lower buffer portion, wherein the upper buffer portion and the lower buffer portion are symmetrically connected to the upper and lower sides of the body and are in step shape. The damping ball can help acquiring more stable aerial photography effect, and high-frequency vibration of rotation parts such as a motor and a propeller is reduced, and the problem that instable shaking caused by aerodynamic force to an aircraft is transmitted to a cloud deck and a camera to cause poor aerial photography effect is reduced as well.
Description
Technical field
The application belongs to unmanned vehicle field, particularly relates to a kind of shock-absorbing ball that is applied to unmanned vehicle.
Background technology
Unmanned plane has that volume is little, lightweight, expense is low, flexible operation and safe feature, can be widely used in taking photo by plane, monitors, the field such as search and rescue, resource exploration.
In prior art, holder for aerial photographing conventionally direct and unmanned plane combines, and because unmanned plane easily produces unsettled rocking under aerodynamic effect, these vibrations are easily conducted to camera rigidly, and directly connection also can directly be passed to pick up camera by the high-frequency vibration of aircraft motor, this turning unit of oar, cause picture to occur image blurring apprehensive, even picture distortion twisting, needs a large amount of post-production to make up the deficiency of the operation quality of taking photo by plane.
Utility model content
The purpose of this utility model is to provide a kind of shock-absorbing ball, solves the problem of Aerial Images shakiness in prior art.
For achieving the above object, the utility model provides following technical scheme:
The embodiment of the present application discloses a kind of shock-absorbing ball, and described shock-absorbing ball comprises cylindrical main part, and symmetrical upper buffer part and the lower buffer part that is connected in the upper and lower both sides of described main part, and described upper buffer part and lower buffer part are all set to stepped.
Preferably, in above-mentioned shock-absorbing ball, described shock-absorbing ball middle part is hollow cavity.
Preferably, in above-mentioned shock-absorbing ball, the cavity of described shock-absorbing ball runs through up and down.
Preferably, in above-mentioned shock-absorbing ball, the material of described shock-absorbing ball is rubber.
Preferably, in above-mentioned shock-absorbing ball, the top of described upper buffer part is formed with the first button offset plate, and the bottom of described lower buffer part is formed with the second button offset plate.
Preferably, in above-mentioned shock-absorbing ball, between described the first button offset plate and upper buffer part, be formed with the first draw-in groove of annular, between described the second button offset plate and lower buffer part, be formed with the second draw-in groove of annular.
Preferably, in above-mentioned shock-absorbing ball, described the first button offset plate and the second button offset plate are all set to circle.
Compared with prior art, the utility model has the advantage of: the utility model is by arranging shock-absorbing ball, can obtain the more stable effect of taking photo by plane, reduce the high-frequency vibration of the rotatable parts such as motor, oar, and unstable the rocking that aerodynamic force causes aircraft conduct to The Cloud Terrace and pick up camera, thereby cause the poor impact of the photographic effect of taking photo by plane.
Accompanying drawing explanation
In order to be illustrated more clearly in the embodiment of the present application or technical scheme of the prior art, to the accompanying drawing of required use in embodiment or description of the Prior Art be briefly described below, apparently, the accompanying drawing the following describes is only some embodiment that record in the application, for those of ordinary skills, do not paying under the prerequisite of creative work, can also obtain according to these accompanying drawings other accompanying drawing.
Figure 1 shows that the structural representation of holder for aerial photographing in the utility model the first embodiment;
Figure 2 shows that the schematic perspective view of holder for aerial photographing in the utility model the first embodiment;
Figure 3 shows that the structural representation of shock-absorbing ball in the utility model specific embodiment;
The structural representation of holder for aerial photographing in the embodiment of the utility model second shown in Fig. 4.
The specific embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is described in detail, obviously, described embodiment is only the utility model part embodiment, rather than whole embodiment.Based on the embodiment in the utility model, the every other embodiment that those of ordinary skills obtain under the prerequisite of not making creative work, belongs to the scope that the utility model is protected.
Shown in ginseng Fig. 1 and Fig. 2, in the utility model the first embodiment, the platform of taking photo by plane can be installed on unmanned vehicle for taking, comprise the first adapter plate 1 and the second adapter plate 2 that be arranged in parallel up and down, between the first adapter plate 1 and the second adapter plate 2, be formed with clearance space, in this clearance space, be connected with shock-absorbing ball 3, shock-absorbing ball 3 is provided with multiple, is symmetrically distributed in the edge of the first adapter plate 1 and the second adapter plate 2.
The first adapter plate 1 and the second adapter plate 2 can be offset plate, carbon fiber board, aluminium sheet, ternary plate etc., as long as the enough rigid structure intensity of quality enough.
The first adapter plate 1 and the second adapter plate 2 comprise respectively the main part of a rectangle, and the installation portion extending from four angles of rectangle main part, and 4 shock-absorbing balls are preferably installed between the installation portion at each angle.
Be easy to expect, under the prerequisite that meets damping effect, the quantity of the shock-absorbing ball between the installation portion at each angle is more few better, to reduce the weight of aircraft entirety.The quantity of shock-absorbing ball can be adjusted according to actual needs.
On the first adapter plate 1 and the second adapter plate 2, also offer lightening hole or lightening grooves 5, to reduce the weight of the first adapter plate 1 and the second adapter plate 2.Under the prerequisite that meets support strength, lightening hole or lightening grooves are many as much as possible or large.
The material of shock-absorbing ball 3 is preferably rubber, and its middle part is a hollow cavity, not only can increase elastic effect, has reduced self weight of shock-absorbing ball 3 simultaneously.The hollow cavity of shock-absorbing ball 3 runs through up and down, so that shock-absorbing ball 3 is in by upper and lower crumpling process, in cavity, gas can be discharged in time.
For realize shock-absorbing ball 3 respectively with the first adapter plate 1 and the second adapter plate 2 between be connected, on the first adapter plate 1, offer the first fixed orifice, the second adapter plate 2 offers the second fixed orifice on position corresponding to the first fixed orifice below, the upper and lower side of shock-absorbing ball 3 offers respectively the first draw-in groove and the second draw-in groove, wherein, the first fixed orifice can be sheathed in the first draw-in groove, and the second fixed orifice can be sheathed in the second draw-in groove.Thus, can self realize respectively and being fixedly connected with of the first adapter plate 1 and the second adapter plate 2 by shock-absorbing ball 3, without other attaching partss, and shock-absorbing ball 3 has certain elasticity, can conveniently fixed orifice be set in draw-in groove, in addition, because each installation portion is provided with 4 shock-absorbing balls, make between shock-absorbing ball and the first adapter plate 1 or the second adapter plate 2 be connected more fastening, difficult drop-off between shock-absorbing ball and fixed orifice.
Shown in ginseng Fig. 3, loss of weight ball 3 comprises cylindrical main part 31, and symmetrical upper buffer part 32 and the lower buffer part 33 that is connected in main part both sides Shang Xia 31, upper buffer part 32 and lower buffer part 33 are all set to stepped, can further realize the steady effect of increasing of loss of weight ball 3.The diameter that the top of upper buffer part 32 is formed with the first button offset plate 34, the first button offset plates 34 is greater than the diameter of the first fixed orifice, and the first draw-in groove 35 is between the first button offset plate 34 and upper buffer part 32.The diameter that the bottom of lower buffer part 33 is formed with the second button offset plate 36, the second button offset plates 36 is greater than the diameter of the second fixed orifice, and the second draw-in groove 37 is between the second button offset plate 36 and lower buffer part 33.
Pick up camera 4 can adopt top board pendant type, as depicted in figs. 1 and 2, pick up camera 4 is positioned at the below of the second adapter plate 2, and be fixed on the first adapter plate 1, the second adapter plate 2 is used to connect aircraft, its advantage is to dwindle the requirement of monopod video camera to space as far as possible, makes full use of the space between the first adapter plate 1 and the second adapter plate 2.
Shown in ginseng Fig. 4, in the utility model the second embodiment, pick up camera can also adopt base plate pendant type, and position for video camera is in the below of the second adapter plate, and is fixed on the second adapter plate, and the first adapter plate is used to connect aircraft, and its advantage is simple in structure.
Be easy to expect, in other embodiments, pick up camera can also be arranged at the top of the first adapter plate, and now pick up camera can be fixed on the first adapter plate or the second adapter plate.
In sum, the utility model adopts rubber shock-absorbing playing skill art, makes every effort to, do not improve under the prerequisite of aircraft weight as far as possible, the increasing of holder for aerial photographing surely be carried out to the technical finesse of detail, increases steady technology, the picture smoothness that makes to take photo by plane, clear, stable in conjunction with other.What get twice the result with half the effort completes the task of taking photo by plane.
It should be noted that, in this article, relational terms such as the first and second grades is only used for an entity or operation to separate with another entity or operational zone, and not necessarily requires or imply and between these entities or operation, have the relation of any this reality or sequentially.And, term " comprises ", " comprising " or its any other variant are intended to contain comprising of nonexcludability, thereby the process, method, article or the equipment that make to comprise a series of key elements not only comprise those key elements, but also comprise other key elements of clearly not listing, or be also included as the intrinsic key element of this process, method, article or equipment.The in the situation that of more restrictions not, the key element being limited by statement " comprising ... ", and be not precluded within process, method, article or the equipment that comprises described key element and also have other identical element.
The above is only the application's the specific embodiment; it should be pointed out that for those skilled in the art, do not departing under the prerequisite of the application's principle; can also make some improvements and modifications, these improvements and modifications also should be considered as the application's protection domain.
Claims (7)
1. a shock-absorbing ball, is characterized in that: described shock-absorbing ball comprises cylindrical main part, and symmetrical upper buffer part and the lower buffer part that is connected in the upper and lower both sides of described main part, and described upper buffer part and lower buffer part are all set to stepped.
2. shock-absorbing ball according to claim 1, is characterized in that: described shock-absorbing ball middle part is hollow cavity.
3. shock-absorbing ball according to claim 2, is characterized in that: the cavity of described shock-absorbing ball runs through up and down.
4. shock-absorbing ball according to claim 1, is characterized in that: the material of described shock-absorbing ball is rubber.
5. shock-absorbing ball according to claim 1, is characterized in that: the top of described upper buffer part is formed with the first button offset plate, and the bottom of described lower buffer part is formed with the second button offset plate.
6. shock-absorbing ball according to claim 5, is characterized in that: between described the first button offset plate and upper buffer part, be formed with the first draw-in groove of annular, be formed with the second draw-in groove of annular between described the second button offset plate and lower buffer part.
7. shock-absorbing ball according to claim 5, is characterized in that: described the first button offset plate and the second button offset plate are all set to circle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420015975.7U CN203638105U (en) | 2014-01-10 | 2014-01-10 | Damping ball |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420015975.7U CN203638105U (en) | 2014-01-10 | 2014-01-10 | Damping ball |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203638105U true CN203638105U (en) | 2014-06-11 |
Family
ID=50869372
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420015975.7U Expired - Fee Related CN203638105U (en) | 2014-01-10 | 2014-01-10 | Damping ball |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203638105U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103754376A (en) * | 2014-01-10 | 2014-04-30 | 江苏艾锐泰克无人飞行器科技有限公司 | Damping ball |
-
2014
- 2014-01-10 CN CN201420015975.7U patent/CN203638105U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103754376A (en) * | 2014-01-10 | 2014-04-30 | 江苏艾锐泰克无人飞行器科技有限公司 | Damping ball |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170519 Address after: Xie Gang Zhen Cao village 523592 Guangdong city of Dongguan province Xie Chang highway Patentee after: Dongguan JAS Unmanned Aerial Vehicle Technology Co., Ltd. Address before: Suzhou City, Jiangsu Province, Zhangjiagang free trade zone 215635 emerging industry incubation center building A room 210A Jiangsu AI retech UAV Technology Co. Ltd. Patentee before: Ai Rui Tyke, Jiangsu unmanned vehicle Science and Technology Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140611 Termination date: 20180110 |