CN207921227U - A kind of support plate applied to unmanned plane - Google Patents
A kind of support plate applied to unmanned plane Download PDFInfo
- Publication number
- CN207921227U CN207921227U CN201721824293.0U CN201721824293U CN207921227U CN 207921227 U CN207921227 U CN 207921227U CN 201721824293 U CN201721824293 U CN 201721824293U CN 207921227 U CN207921227 U CN 207921227U
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- CN
- China
- Prior art keywords
- support arm
- support
- unmanned plane
- holder
- receiver
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Abstract
The utility model discloses a kind of support plates applied to unmanned plane,Its structure includes bottom bar,Through-hole,Support arm,Inner support,Receiver,Damper,Bottom plate,Holder,Power cord,The support arm is combined by the identical arch frame body in both sides and is integrally formed,Identical circular through hole is equipped at lower end,Position between on the upside of the support arm is equipped with connecting plate,End face is smooth and is rectangular,Two side position of the support arm is equipped with the corresponding through-hole of shape,By bottom bar through connection at the support arm lower end,Bottom bar is run through by both ends component and middle part cross bar,Two middle side part of the support arm is connected with inner support,The " U "-shaped structure of inner support,Right end is equipped with receiver,The holder is located in the inner cavity that support arm arches upward,The utility model is equipped with damper,Cushioning effect is carried out using fluid damping mode,The vibrations that unmanned plane generates in flight course can be effectively eliminated.
Description
Technical field
The utility model is a kind of support plate applied to unmanned plane, belongs to unmanned plane accessory technical field.
Background technology
Support plate is used in a kind of accessory on unmanned plane, and unmanned plane is to utilize radio robot and the program provided for oneself
The not manned aircraft that control device manipulates.Without cockpit on machine, but the equipment such as automatic pilot, presetting apparatus are installed.
Prior art discloses application No. is：201520614418.1 a kind of support plate applied to unmanned plane, belong to
Air vehicle technique field, including pillar, the first plate, the second plate and elastic parts.The support plate applied to unmanned plane passes through
Holder and unmanned plane are flexibly connected, the holder on unmanned plane is overcome and is typically due to the effect of its own gravity and opposite
It is final so that the technological deficiency that the connecting portion between holder and unmanned plane is worn in unmanned plane vertical tremor.But its
It is disadvantageous in that support plate uses flexible connection mode, unmanned plane is in flight course, since the running between device generates
Vibrations be easy to be transmitted on supporting body.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of support plate applied to unmanned plane,
Flexible connection mode is used to solve support plate, unmanned plane is in flight course, due to the vibrations of the running generation between device
It is easy to be transmitted to the problem on supporting body.
To achieve the goals above, the utility model is to realize by the following technical solutions：One kind being applied to nobody
The support plate of machine, structure include bottom bar, through-hole, support arm, inner support, receiver, damper, bottom plate, holder, power cord,
The support arm is combined by the identical arch frame body in both sides and is integrally formed, and identical circular through hole, the outer branch are equipped at lower end
Position between on the upside of frame is equipped with connecting plate, and end face is smooth and is rectangular, and it is corresponding logical that two side position of the support arm is equipped with shape
Hole, by bottom bar through connection at the support arm lower end, bottom bar is run through by both ends component and middle part cross bar, the support arm both sides
Middle part is connected with inner support, the " U "-shaped structure of inner support, and right end is equipped with receiver, and the holder is located at support arm
In the inner cavity arched upward, the receiver wiring is passed through between support arm both sides, and the inner support is by receiver and states bottom plate
It is linked together, damper is equipped at left and right sides of the backplate surface；The damper by outer barrel, end, liquid storage cylinder, piston valve,
Rubber pad, piston rod composition, the outer barrel both ends are equipped with end, and the end wherein side is connected with liquid storage cylinder, the work
Plug valve is located at outer barrel side, and is connected with inside, and the outer barrel is equipped with rubber pad, and the rubber pad middle through-hole is by living
Stopper rod is flexibly connected using up-down mode, and described piston rod one end is connected with end, lower end and position and the bottom of the end
Plate is in contact and connects.
Further, the holder port uses energization connection type with power cord.
Further, bottom plate is equipped between the bottom bar both sides.
Further, the power cord upper end passes through on the upside of support arm.
Further, the holder is located on backplate surface, using fastening mounting means.
Further, the receiver uses wiring succession with holder.
Further, fluid built in the liquid storage cylinder, can continuous loopy moving.
Further, the rubber pad is round pad body structure.
Advantageous effect
A kind of support plate applied to unmanned plane of the utility model, the protection chamber being mainly made up of support arm and inner support
Body structure carries holder using bottom plate, and backplate surface both sides are equipped with damper, increase shock-absorbing protecting, using fluid damping mode
Cushioning effect is carried out, vibrations are imported into end first, piston rod is driven to be moved up and down at rubber pad center, constantly lifting acting,
Liquid storage cylinder plays damping action in the case of circulating, piston valve construction is compact, reasonable, good seal performance, passes through outer barrel pair
Inner cavity is protected, and the vibrations that unmanned plane generates in flight course can be effectively eliminated.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural schematic diagram of support plate applied to unmanned plane of the utility model；
Fig. 2 is the damper schematic diagram of the utility model；
Fig. 3 is the bottom bar structural decomposition diagram of the utility model；
Fig. 4 is the damper surface structure decomposition diagram of the utility model.
In figure：Bottom bar -1, through-hole -2, support arm -3, inner support -4, receiver -5, damper -6, outer barrel -601, end -
602, liquid storage cylinder -603, piston valve -604, rubber pad -605, piston rod -606, bottom plate -7, holder -8, power cord -9.
Specific implementation mode
To make the technical means, creative features, achievement of purpose, and effectiveness of the utility model be easy to understand, below
In conjunction with specific implementation mode, the utility model is expanded on further.
- Fig. 4 is please referred to Fig.1, the utility model provides a kind of technical solution：A kind of support plate applied to unmanned plane,
Structure includes bottom bar 1, through-hole 2, support arm 3, inner support 4, receiver 5, damper 6, bottom plate 7, holder 8, power cord 9, described
Support arm 3 is combined by the identical arch frame body in both sides and is integrally formed, and identical circular through hole, the support arm 3 are equipped at lower end
Position between upside is equipped with connecting plate, and end face is smooth and is rectangular, and 3 liang of side positions of the support arm are equipped with the corresponding through-hole of shape
2, by bottom bar 1 through connection at 3 lower end of the support arm, bottom bar 1 is run through by both ends component and middle part cross bar, the support arm 3
Two middle side parts are connected with inner support 4,4 " U "-shaped structure of the inner support, and right end is equipped with receiver 5, and the holder 8 is set
In the inner cavity that support arm 3 arches upward, 5 wiring of the receiver is passed through between 3 both sides of support arm, and the inner support 4 is by connecing
It receives device 5 to be linked together with bottom plate 7 is stated, damper 6 is equipped at left and right sides of 7 surface of bottom plate；The damper 6 by outer barrel 601,
End 602, liquid storage cylinder 603, piston valve 604, rubber pad 605, piston rod 606 form, and 601 both ends of the outer barrel are equipped with end
602, the wherein side of the end 602 is connected with liquid storage cylinder 603, and the piston valve 604 is located at 601 side of outer barrel, and with it is interior
Portion is connected, and the outer barrel 601 is internally provided with rubber pad 605, and 605 middle through-hole of the rubber pad is by piston rod 606 using liter
Drop mode is flexibly connected, and 606 one end of the piston rod is connected with end 602, lower end and position and the bottom plate of the end 602
7 are in contact and connect, and 8 port of the holder uses energization connection type with power cord 9, and bottom is equipped between 1 both sides of the bottom bar
Plate 7,9 upper end of the power cord pass through the upside of support arm 3, the holder 8 to be located on 7 surface of bottom plate, using fastening mounting means,
The receiver 5 uses wiring succession with holder 8.
Piston rod 606 described in this patent is the connecting component of supporting piston acting, using rolling and processing, to improve table
Face resistance to corrosion, the generation or expansion of piston rod and energy delay fatigue crackle.
It is carrying out in use, the protection cavity body structure being mainly made up of support arm 3 and inner support 4, is carried using bottom plate 7
Holder 8,7 surface both sides of bottom plate are equipped with damper 6, increase shock-absorbing protecting, carry out cushioning effect using fluid damping mode, first
Vibrations are imported into end 602, piston rod 606 is driven to be moved up and down at 605 center of rubber pad, constantly lifting acting, liquid storage cylinder 603
Play damping action in the case of circulating, piston valve 604 is compact-sized, reasonable, good seal performance, right by outer barrel 601
Inner cavity is protected, and the vibrations that unmanned plane generates in flight course can be effectively eliminated.
The utility model solve the problems, such as be support plate use flexible connection mode, unmanned plane in flight course, due to
The vibrations that running between device generates are easy to be transmitted on supporting body, and the utility model is combined with each other by above-mentioned component,
The vibrations that unmanned plane generates in flight course can be effectively eliminated, it is described in detail below：
601 both ends of outer barrel are equipped with end 602, and the wherein side of the end 602 is connected with liquid storage cylinder 603, the piston
Valve 604 is located at 601 side of outer barrel, and is connected with inside, and the outer barrel 601 is internally provided with rubber pad 605, the rubber pad
605 middle through-holes are flexibly connected by piston rod 606 using up-down mode, and 606 one end of the piston rod is connected with end 602,
The lower end of the end 602 is in contact and connect with position with bottom plate 7.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent requirements of the claims
All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiment being appreciated that.
Claims (6)
1. a kind of support plate applied to unmanned plane, structure include bottom bar (1), through-hole (2), support arm (3), inner support (4),
Receiver (5), damper (6), bottom plate (7), holder (8), power cord (9), the support arm (3) is by the identical arched frame in both sides
Body combination is integrally formed, and identical circular through hole is equipped at lower end, and the position between support arm (3) upside is equipped with connecting plate,
End face is smooth and is rectangular, it is characterised in that：
(3) two side position of the support arm is equipped with the corresponding through-hole of shape (2), is passed through by bottom bar (1) at support arm (3) lower end
Connection is worn, bottom bar (1) is run through by both ends component and middle part cross bar, and (3) two middle side part of the support arm is connected with inner support (4)
It connects, the " U "-shaped structure of the inner support (4), right end is equipped with receiver (5), and the holder (8) is located at support arm (3) and arches upward
Inner cavity in, receiver (5) wiring is passed through between support arm (3) both sides, and the inner support (4) passes through receiver (5)
It is linked together with bottom plate (7) is stated, damper (6) is equipped at left and right sides of bottom plate (7) surface；
The damper (6) is by outer barrel (601), end (602), liquid storage cylinder (603), piston valve (604), rubber pad (605), work
Stopper rod (606) forms, and outer barrel (601) both ends are equipped with end (602), the end (602) wherein side and liquid storage cylinder
(603) it is connected, the piston valve (604) is located at outer barrel (601) side, and is connected with inside, and the outer barrel (601) is internal
Equipped with rubber pad (605), rubber pad (605) middle through-hole is flexibly connected by piston rod (606) using up-down mode, described
Piston rod (606) one end is connected with end (602), and the lower end of the end (602) is in contact and connects with position with bottom plate (7)
It connects.
2. a kind of support plate applied to unmanned plane according to claim 1, it is characterised in that：Holder (8) port
Energization connection type is used with power cord (9).
3. a kind of support plate applied to unmanned plane according to claim 1, it is characterised in that：Bottom bar (1) both sides
Between be equipped with bottom plate (7).
4. a kind of support plate applied to unmanned plane according to claim 1, it is characterised in that：On the power cord (9)
End is on the upside of support arm (3).
5. a kind of support plate applied to unmanned plane according to claim 1, it is characterised in that：The holder (8) is located at
On bottom plate (7) surface, using fastening mounting means.
6. a kind of support plate applied to unmanned plane according to claim 1, it is characterised in that：The receiver (5) with
Holder (8) uses wiring succession.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721824293.0U CN207921227U (en) | 2017-12-24 | 2017-12-24 | A kind of support plate applied to unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721824293.0U CN207921227U (en) | 2017-12-24 | 2017-12-24 | A kind of support plate applied to unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207921227U true CN207921227U (en) | 2018-09-28 |
Family
ID=63607603
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721824293.0U Expired - Fee Related CN207921227U (en) | 2017-12-24 | 2017-12-24 | A kind of support plate applied to unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207921227U (en) |
-
2017
- 2017-12-24 CN CN201721824293.0U patent/CN207921227U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| 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: 20180928 Termination date: 20181224 |