CN207550480U - Unmanned plane damping push and pull system and unmanned plane - Google Patents
Unmanned plane damping push and pull system and unmanned plane Download PDFInfo
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- CN207550480U CN207550480U CN201721297155.1U CN201721297155U CN207550480U CN 207550480 U CN207550480 U CN 207550480U CN 201721297155 U CN201721297155 U CN 201721297155U CN 207550480 U CN207550480 U CN 207550480U
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- unmanned plane
- frame
- pull system
- quick release
- damping push
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Abstract
The utility model discloses a kind of unmanned plane damping push and pull system and unmanned plane, including link assembly and the multiple dampening assemblies being arranged on link assembly；Link assembly includes upper support frame and lower bracing frame and multiple upright bars；Upper support frame and lower bracing frame are set from top to bottom in vertical direction, and edge is connected by multiple upright bars between upper support frame and lower bracing frame；Upright bar is respectively perpendicular to upper support frame and lower bracing frame；It is the Quick Release plate of L-shape and intermediate support, multiple O-shaped shock rings that dampening assembly, which includes two pieces of cross sections,；Multiple dampening assemblies are mounted on the top surface of lower bracing frame, and multiple dampening assemblies are set with the circumferencial direction of lower bracing frame successively sequence interval, and one end of each dampening assembly is directed at the center of lower bracing frame.Unmanned plane damping push and pull system provided by the utility model and unmanned plane, damping effect is more prominent, and dampening assembly is rapidly assembled and disassembled.
Description
Technical field
The utility model is related to unmanned plane equipment technical field more particularly to a kind of unmanned plane damping push and pull system and nobody
Machine.
Background technology
In recent years, with the rise of unmanned plane and the fast development of related model plane and unmanned plane field technology, nobody
Machine is also applied in more and more occasions；In the process, more and more masses also start to contact unmanned plane, from this nothing
It is man-machine to have entered into common people's entertainment field from profession, scientific research field.
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates.
In some project unmanned vehicle R＆D process, research staff according to the design needs, be on unmanned aerial vehicle body
Design one damping push and pull system of installation；Simultaneously according to specific design requirement, need in damping push and pull system using quick
Dismounting and the adjustable dampening assembly design of damping level；But the study found that in the prior art and there is no such damping group
Part.
Therefore, how to design a dampening assembly for meeting above-mentioned design requirement is that those skilled in the art are badly in need of solving
Problem.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane damping push and pull system and unmanned plane, to solve above-mentioned ask
Topic.
In order to achieve the above object, the technical solution of the utility model is realized in：
The utility model additionally provides a kind of unmanned plane damping push and pull system, including link assembly and is arranged on the connecting rod
Multiple dampening assemblies on component；
Wherein, the link assembly includes upper support frame and lower bracing frame and multiple upright bars；
The upper support frame and the lower bracing frame are set from top to bottom in vertical direction, and the upper support frame with it is described
Edge is connected by multiple upright bars between lower bracing frame；The upright bar be respectively perpendicular to the upper support frame and it is described under
Supporting rack；
It is the Quick Release plate of L-shape and intermediate support, multiple O-shaped dampings that the dampening assembly, which includes two pieces of cross sections,
Ring；Wherein, multiple O-shaped shock ring sequences are socketed in the intermediate support；Two blocks of Quick Release plates are oppositely arranged, and are enclosed
The Quick Release frame of one, city rectangular shape；The Quick Release frame is formed by bolt assembly between two blocks of Quick Release plates；
Multiple dampening assemblies are mounted on the top surface of the lower bracing frame, and multiple dampening assemblies are with described
Sequence interval is set the circumferencial direction of lower bracing frame successively, and one end of each dampening assembly is directed to the lower bracing frame
Center at.
It preferably, can embodiment as one kind；The upright bar is specially four；The upper support frame and the lower support
Edge is detachably connected by four upright bar realizations between frame.
It preferably, can embodiment as one kind；The upper support frame is cross centre frame；The cross centre frame
Surface be provided with mounting hole；And the surface of the cross centre frame is additionally provided with engraved structure.
It preferably, can embodiment as one kind；The lower bracing frame is disc-shaped central frame；The disc-shaped central frame
Surface be provided with mounting hole；And the surface of the disc-shaped central frame is additionally provided with engraved structure.
It preferably, can embodiment as one kind；The intermediate support is two, and two intermediate supports are simultaneously
Row arrangement；The intermediate support is plate support.
It preferably, can embodiment as one kind；The inner surface of the intermediate support is provided with multiple arc-shaped
Concave part.
It preferably, can embodiment as one kind；The Quick Release plate includes first substrate portion and second substrate portion；Described
One baseplate part connect the Quick Release plate to form that cross section is L-shape with the second substrate portion；And the first substrate portion is interior
Side surface is provided with multiple arc-shaped concave parts.
It preferably, can embodiment as one kind；The Quick Release plate is oppositely arranged one by one with the intermediate support, and institute
Quick Release plate is stated to be used to clamp the O-shaped shock ring with the corresponding intermediate support.
It preferably, can embodiment as one kind；The concave part in the first substrate portion of the Quick Release plate and the intermediate branch
The concave part position of support member is opposite, and the concave part in the first substrate portion of the Quick Release plate and the concave part of the intermediate support
Merge the partial arc structure for clamping the O-shaped shock ring.
Correspondingly, the utility model provides a kind of unmanned plane, including unmanned aerial vehicle body and the unmanned plane damping
Push and pull system；
Wherein, multiple upright bars of the unmanned plane damping push and pull system run through across in the unmanned aerial vehicle body
Portion；For being fixedly connected with battery warehouse component, the unmanned plane damping connects upper support frame in the unmanned plane damping push and pull system
Lower bracing frame on lever system is used to be fixedly connected with holder and fuselage Fast detachable unit；And in the unmanned plane damping push and pull system
Between multiple dampening assemblies are located at the top of the bottom and the lower bracing frame of the unmanned aerial vehicle body.
Compared with prior art, it is the advantages of the utility model embodiment：
A kind of unmanned plane damping push and pull system provided by the utility model and unmanned plane；
First aspect：The utility model provides a kind of unmanned plane damping push and pull system；The unmanned plane damping push and pull system
Mainly it is made of dampening assembly and link assembly.The primary structure for analyzing above-mentioned dampening assembly is understood：It will be apparent that two pieces described fast
It tears plate open to be oppositely arranged, the Quick Release frame for a rectangular shape of encircling a city；The Quick Release frame primarily serves to form dampening assembly
Agent structure；The plurality of O-shaped shock ring sequence is socketed in the intermediate support, the core which primarily serves
Cushioning effect；Since multiple O-shaped shock ring sequences are socketed in intermediate support, while multiple O-shaped shock rings do not limit tool
Body quantity can be two, three or any amount, due to using quick-disassembly structure, it is possible to easily to O-shaped
The quantity of shock ring is replaced, and then realizes adjusting (in a certain range, the O-shaped shock ring of the damping level of dampening assembly
Quantity it is more, formed dampening assembly cushioning effect it is more apparent)；Meanwhile above-mentioned dampening assembly employs L-shape
Quick Release plate, be mutually butted, then screw on bolt assembly and rapid disassembling can be realized.Meanwhile the dampening assembly, it both can be real
Existing dampening assembly is rapidly assembled and disassembled, while can also realize the adjustable of damping level, and the practicality is stronger, meets
The design requirement of the unmanned plane shock-damping structure of specific condition.Above-mentioned dampening assembly coordinates can installing for above-mentioned link assembly
Form a unmanned plane damping push and pull system；In the structure of above-mentioned unmanned plane damping push and pull system, above-mentioned multiple dampening assemblies
Mounted on the top surface of the lower bracing frame, and multiple dampening assemblies are suitable successively with the circumferencial direction of the lower bracing frame
Sequence is arranged at intervals, and one end of each dampening assembly is directed at the center of the lower bracing frame.Utilize above-mentioned damping group
Part is compounded in formation unmanned plane damping push and pull system on link assembly, which utilizes multiple dampening assemblies
Composite shock-absorbing effect, further enhance damping effect.
Second aspect：The utility model additionally provides a kind of unmanned plane, which is to include above-mentioned unmanned plane damping
The unmanned plane type of push and pull system specific structure；The damping effect of the unmanned machine equipment is more prominent, damping effect clearly,
And its structural reliability of above-mentioned unmanned plane damping push and pull system is stronger, and structure construction is more stable.
Description of the drawings
It, below will be right in order to illustrate more clearly of specific embodiment of the present invention or technical solution of the prior art
Specific embodiment or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, it is described below
In attached drawing be the utility model some embodiments, for those of ordinary skill in the art, do not paying creativeness
Under the premise of labour, other attached drawings are can also be obtained according to these attached drawings.
Fig. 1 is the stereochemical structure signal that the unmanned plane damping linkage that the utility model embodiment provides is unified under visual angle
Figure；
Fig. 2 is the stereochemical structure signal under another visual angle of unmanned plane damping push and pull system that the utility model embodiment provides
Figure；
Fig. 3 is the main structure diagram of unmanned plane damping push and pull system that the utility model embodiment provides；
Fig. 4 is the overlooking the structure diagram of unmanned plane damping push and pull system that the utility model embodiment of Fig. 3 provides；
Fig. 5 is the present invention looks up structural representation of unmanned plane damping push and pull system that the utility model embodiment of Fig. 3 provides；
Fig. 6 is under a visual angle of the dampening assembly in the unmanned plane damping push and pull system that the utility model embodiment provides
Dimensional structure diagram；
Fig. 7 is under another visual angle of the dampening assembly in the unmanned plane damping push and pull system that the utility model embodiment provides
Dimensional structure diagram；
Fig. 8 is under another visual angle of the dampening assembly in the unmanned plane damping push and pull system that the utility model embodiment provides
Dimensional structure diagram；
Fig. 9 is that the front view structure of the dampening assembly in the unmanned plane damping push and pull system that the utility model embodiment provides is shown
It is intended to；
Figure 10 is the explosive decomposition of the dampening assembly in the unmanned plane damping push and pull system that the utility model embodiment provides
Structure diagram；
Figure 11 is the unmanned plane integral installation distribution structure schematic diagram that the utility model embodiment provides.
Label：
1- link assemblies；11- upper support frames；12- lower bracing frames；13- upright bars；
2- dampening assemblies；21- Quick Release plates；211- first substrates portion；212- second substrates portion；22- intermediate supports；23-O
Type shock ring；
3- mounting holes；
4- engraved structures；
5- concave parts.
Specific embodiment
The technical solution of the utility model is clearly and completely described below in conjunction with attached drawing, it is clear that described
Embodiment is the utility model part of the embodiment, instead of all the embodiments.Based on the embodiment in the utility model, sheet
Field those of ordinary skill all other embodiments obtained without making creative work, belong to this practicality
Novel protected range.
In the description of the present invention, it should be noted that term " " center ", " on ", " under ", it is "left", "right", " perpendicular
Directly ", the orientation of the instructions such as " level ", " interior ", " outer " or position relationship are based on orientation shown in the drawings or position relationship, are only
The utility model must have specific with the device or element for simplifying description rather than instruction or hint meaning for ease of description
Orientation, with specific azimuth configuration and operation, therefore it is not intended that limitation to the utility model.In addition, term " the
One ", " second ", " third " are only used for description purpose, and it is not intended that instruction or hint relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected or integrally
Connection；Can be mechanical connection or electrical connection；It can be directly connected, can also be indirectly connected by intermediary,
It can be the connection inside two elements.For the ordinary skill in the art, can above-mentioned art be understood with concrete condition
Concrete meaning of the language in the utility model.
The utility model is further described in detail below through specific implementation examples and in conjunction with the accompanying drawings.
Referring to Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, Fig. 7, Fig. 8, Fig. 9, Figure 10, the utility model additionally provides a kind of nothing
Man-machine damping push and pull system, including link assembly 1 and the multiple dampening assemblies 2 being arranged on the link assembly 1；
Wherein, the link assembly 1 includes upper support frame 11 and lower bracing frame 12 and multiple upright bars 13；The upper support
Frame 11 and the lower bracing frame 12 are set from top to bottom in vertical direction, and the upper support frame 11 and the lower bracing frame 12 it
Between edge connected by multiple upright bars 13；The upright bar 13 is respectively perpendicular to the upper support frame 11 and the lower support
Frame 12；
It is the Quick Release plate 21 of L-shape and intermediate support 22, multiple O that the dampening assembly 2, which includes two pieces of cross sections,
Type shock ring 23；Wherein, multiple O-shaped 23 sequences of shock ring are socketed in the intermediate support 22；Two pieces of Quick Release
Plate 21 is oppositely arranged, the Quick Release frame for a rectangular shape of encircling a city；It is formed between two blocks of Quick Release plates 21 by bolt assembly
The Quick Release frame；
Multiple dampening assemblies 2 be mounted on the lower bracing frame 12 top surface, and multiple dampening assemblies 2 with
Sequence interval is set the circumferencial direction of the lower bracing frame 12 successively, and one end of each dampening assembly 2 be directed to it is described
At the center of lower bracing frame 12.
The primary structure for analyzing above-mentioned unmanned plane damping push and pull system is understood：
The utility model provides a kind of unmanned plane damping push and pull system；The unmanned plane damping push and pull system is mainly by damping
Component and link assembly are formed；The primary structure for first analyzing above-mentioned dampening assembly is understood：It will be apparent that two blocks of Quick Release plates are opposite
Setting, the Quick Release frame for a rectangular shape of encircling a city；The Quick Release frame primarily serves the agent structure to form a dampening assembly；
The plurality of O-shaped shock ring sequence is socketed in the intermediate support, and the damping for the core which primarily serves is made
With；Since multiple O-shaped shock ring sequences are socketed in intermediate support, while multiple O-shaped shock rings do not limit particular number,
Can be two, three or any amount, due to using quick-disassembly structure, it is possible to easily to O-shaped shock ring
Quantity is replaced, and then (in a certain range, the quantity of O-shaped shock ring is got over for the adjusting of the damping level of realization dampening assembly
More, the cushioning effect of the dampening assembly formed is more apparent)；Meanwhile above-mentioned dampening assembly employs the Quick Release of L-shape
Plate is mutually butted, and then screws on bolt assembly and rapid disassembling can be realized.Meanwhile the dampening assembly, it can both realize damping
Component is rapidly assembled and disassembled, while can also realize the adjustable of damping level, and the practicality is stronger, meets specific
The design requirement of the unmanned plane shock-damping structure of situation.The above-mentioned link assembly of above-mentioned dampening assembly cooperation can install composition one
A unmanned plane damping push and pull system；In the structure of above-mentioned unmanned plane damping push and pull system, above-mentioned multiple dampening assemblies are mounted on
The top surface of the lower bracing frame, and multiple dampening assemblies are with the circumferencial direction of the lower bracing frame successively sequence interval
Setting, and one end of each dampening assembly is directed at the center of the lower bracing frame.It is compound using above-mentioned dampening assembly
Unmanned plane damping push and pull system is formed on link assembly, the unmanned plane damping push and pull system is compound using multiple dampening assemblies
Cushioning effect further enhances damping effect.
It should be noted that the mentality of designing of above-mentioned double leval jib damping and its (relative to fuselage, holder, battery compartment) dress
With mode, the above-mentioned design such as mating fuselage hollow structure, the O-shaped rubber ring damping module in bottom matched is all more novel, and
With certain novelty.
The concrete structure and particular technique of the unmanned plane damping push and pull system provided below the utility model embodiment
Effect, which is done, to be described in detail：
It preferably, can embodiment as one kind；Referring to Fig. 1-Fig. 3, the upright bar 13 is specially four；The upper support
Edge is detachably connected by four upright bar realizations between frame 11 and the lower bracing frame 12.
It should be noted that referring to Fig. 1, above-mentioned upright bar 13 is preferably four, upper support frame 11 and the lower bracing frame 12
Between edge be detachably connected by four upright bars realizations, in this way by four upright bars 13, one can be formed
A frame structure；The frame structure employs the connection mode design of connection easy to disassemble.
It preferably, can embodiment as one kind；Referring to Fig. 1-Fig. 3, the upper support frame 11 is cross centre frame；Institute
The surface for stating cross centre frame is provided with mounting hole 3；And the surface of the cross centre frame is additionally provided with engraved structure 4.
It should be noted that upper support frame 11 is cross centre frame, above-mentioned shape can ensure the knot of frame structure
Structure stability, while the surface of the cross centre frame is additionally provided with engraved structure 4, can reduce to the full extent so above-mentioned
Upper support frame 11 (i.e. and then reduction link assembly) unnecessary dead weight weight.
It preferably, can embodiment as one kind；Referring to Fig. 1-Fig. 3, the lower bracing frame 12 is disc-shaped central frame；Institute
The surface for stating disc-shaped central frame is provided with mounting hole 3；And the surface of the disc-shaped central frame is additionally provided with engraved structure 4.
It should be noted that lower bracing frame 12 is disc-shaped central frame, above-mentioned shape can ensure the knot of frame structure
Structure stability, while the surface of the disc-shaped central frame is additionally provided with engraved structure 4, can reduce to the full extent so above-mentioned
Lower bracing frame 12 (i.e. and then reduction link assembly) unnecessary dead weight weight.
It preferably, can embodiment as one kind；Referring to Fig. 6-Figure 10, the intermediate support 22 is two, and two
22 arranged in parallel of intermediate support；The intermediate support 22 is plate support.The inside of the intermediate support 22
Surface is provided with multiple arc-shaped concave parts 5.
It should be noted that intermediate support 22 is plate support, at the same time, also in the inside of intermediate support 22
Surface is provided with multiple arc-shaped concave parts 5, which is the portion for accommodating O-shaped shock ring 23
Separation structure can be embedded in into, and then it is whole to ensure that two 22 sets of intermediate supports connect formation one after multiple O-shaped shock rings 23
Body structure.
It preferably, can embodiment as one kind；Referring to Figure 10, the Quick Release plate 21 includes first substrate portion 211 and the
Two baseplate parts 212；The first substrate portion 211 connect the Quick Release to form that cross section is L-shape with the second substrate portion 212
Plate；And the inner surface in the first substrate portion 211 is provided with multiple arc-shaped concave parts 5.
It preferably, can embodiment as one kind；Referring to Fig. 6-Figure 10, the Quick Release plate 21 and the intermediate support 22
It is oppositely arranged one by one, and the Quick Release plate is used to clamp the O-shaped shock ring with the corresponding intermediate support.
It should be noted that the Quick Release plate 21 is oppositely arranged one by one with the intermediate support 22, and the Quick Release plate
21 are used to clamp the O-shaped shock ring 23 with the corresponding intermediate support 22.
It preferably, can embodiment as one kind；Referring to Fig. 6-Figure 10, the first substrate portion 211 of the Quick Release plate 21
Concave part 5 is opposite with 5 position of concave part of the intermediate support 22, and the concave part in the first substrate portion of the Quick Release plate 21
5 merge the partial arc structure for clamping the O-shaped shock ring 23 with the concave part 5 of the intermediate support 22.
It should be noted that the inner surface in each first substrate portion 211 on Quick Release plate 21 be both provided with it is arc-shaped
Concave part 5, the arc-shaped concave part 5 on the Quick Release plate 21 and the arc-shaped groove on the inner surface of intermediate support 22
Portion 5 cooperates, so as to which O-shaped shock ring 23 is locked in some installed position.
Referring to Figure 11, correspondingly, the utility model additionally provides a kind of unmanned plane, including unmanned aerial vehicle body A and nothing
Man-machine damping push and pull system；
Wherein, multiple upright bars 13 of the unmanned plane damping push and pull system run through across the unmanned aerial vehicle body A's
Middle part；For being fixedly connected with battery warehouse component, the unmanned plane subtracts upper support frame 11 in the unmanned plane damping push and pull system
Lower bracing frame 12 in shake push and pull system is used to be fixedly connected with holder and fuselage Fast detachable unit；And the unmanned plane damping linkage
Multiple dampening assemblies on system are located between 12 top of bottom and the lower bracing frame of the unmanned aerial vehicle body A.
The utility model additionally provides a kind of unmanned plane, which is to include above-mentioned unmanned plane damping push and pull system spy
Determine the unmanned plane type of structure；The damping effect of the unmanned machine equipment is more prominent, damping effect clearly, and above-mentioned nothing
Man-machine its structural reliability of damping push and pull system is stronger, and structure construction is more stable.
The unmanned plane damping push and pull system that the utility model embodiment provides has the technical advantage of following aspect：
First, the unmanned plane damping push and pull system and unmanned plane that the utility model embodiment provides, the unmanned plane damping connecting rod
System is mainly made of dampening assembly and link assembly；It is L-shaped shape that the primary structure of above-mentioned dampening assembly, which includes two pieces of cross sections,
The Quick Release plate and intermediate support of shape, multiple O-shaped shock rings；The primary structure of above-mentioned link assembly includes upper support frame under
Supporting rack and multiple upright bars；Multiple dampening assemblies are mounted on the top surface of the lower bracing frame, and multiple described subtract
It shakes component to set with the circumferencial direction of the lower bracing frame successively sequence interval, and one end of each dampening assembly is directed to
At the center of the lower bracing frame.It will be apparent that the concrete structure and connection relation of above-mentioned link assembly and dampening assembly, position
The relationship of putting has specific design, therefore the unmanned plane damping push and pull system that the utility model embodiment provides, technical construction
More rationally, and the relatively traditional unmanned plane difference of damping effect is larger.
2nd, the unmanned plane damping push and pull system and unmanned plane that the utility model embodiment provides, dampening assembly is using fast
Tear structure open, it is possible to easily the quantity of O-shaped shock ring is replaced, and then realize the damping level of dampening assembly
It adjusts (in a certain range, the quantity of O-shaped shock ring is more, and the cushioning effect of the dampening assembly formed is more apparent)；
3rd, the unmanned plane damping push and pull system and unmanned plane that the utility model embodiment provides, above-mentioned double leval jib damping
Mentality of designing can ensure that unmanned plane damping push and pull system structure is more stablized, while (the apolegamy such as its assembly method, damping modes
The O-shaped rubber ring shock ring in bottom) etc. above-mentioned design it is all more novel, and with certain novelty.
4th, the unmanned plane damping push and pull system and unmanned plane, connection structure that the utility model embodiment provides are more steady
It is fixed, it is highly reliable, device security is high；It can be perfectly safe reliably in this way, ensure that the structure of unmanned plane is steady
It is qualitative, ensure the flight reappearance and flight efficiency of unmanned plane.
Based on above many significant technical advantages, unmanned plane damping push and pull system provided by the utility model and unmanned plane
Good market prospects and economic benefit will be brought.
Finally it should be noted that：The above various embodiments is only to illustrate the technical solution of the utility model rather than it is limited
System；Although the utility model is described in detail with reference to foregoing embodiments, those of ordinary skill in the art should
Understand：It can still modify to the technical solution recorded in foregoing embodiments either to which part or whole
Technical characteristic carries out equivalent replacement；And these modifications or replacement, this practicality that it does not separate the essence of the corresponding technical solution are new
The range of each embodiment technical solution of type.
Claims (10)
1. a kind of unmanned plane damping push and pull system, which is characterized in that including link assembly and be arranged on the link assembly
Multiple dampening assemblies；
Wherein, the link assembly includes upper support frame and lower bracing frame and multiple upright bars；
The upper support frame and the lower bracing frame are set from top to bottom in vertical direction, and the upper support frame and the lower branch
Edge is connected by multiple upright bars between support；The upright bar is respectively perpendicular to the upper support frame and the lower support
Frame；
It is the Quick Release plate of L-shape and intermediate support, multiple O-shaped shock rings that the dampening assembly, which includes two pieces of cross sections,；
Wherein, multiple O-shaped shock ring sequences are socketed in the intermediate support；Two blocks of Quick Release plates are oppositely arranged, besieged city
The Quick Release frame of one rectangular shape；The Quick Release frame is formed by bolt assembly between two blocks of Quick Release plates；
Multiple dampening assemblies are mounted on the top surface of the lower bracing frame, and multiple dampening assemblies are with the lower branch
Sequence interval is set the circumferencial direction of support successively, and one end of each dampening assembly is directed in the lower bracing frame
At the heart.
2. unmanned plane damping push and pull system as described in claim 1, it is characterised in that：
The upright bar is specially four；Edge is described vertical by four between the upper support frame and the lower bracing frame
Bar realization is detachably connected.
3. unmanned plane damping push and pull system as described in claim 1, it is characterised in that：
The upper support frame is cross centre frame；The surface of the cross centre frame is provided with mounting hole；And the cross
The surface of type centre frame is additionally provided with engraved structure.
4. unmanned plane damping push and pull system as described in claim 1, it is characterised in that：
The lower bracing frame is disc-shaped central frame；The surface of the disc-shaped central frame is provided with mounting hole；And the disk
The surface of shape centre frame is additionally provided with engraved structure.
5. unmanned plane damping push and pull system as described in claim 1, it is characterised in that：
The intermediate support is two, and two intermediate support arranged in parallel；The intermediate support is plate branch
Support member.
6. unmanned plane damping push and pull system as described in claim 1, it is characterised in that：
The inner surface of the intermediate support is provided with multiple arc-shaped concave parts.
7. unmanned plane damping push and pull system as claimed in claim 6, it is characterised in that：
The Quick Release plate includes first substrate portion and second substrate portion；The first substrate portion connect shape with the second substrate portion
Into the Quick Release plate that cross section is L-shape；And the inner surface in the first substrate portion is provided with multiple arc-shaped concave parts.
8. unmanned plane damping push and pull system as claimed in claim 7, it is characterised in that：
The Quick Release plate is oppositely arranged one by one with the intermediate support, and the Quick Release plate and the corresponding intermediate support
For clamping the O-shaped shock ring.
9. unmanned plane damping push and pull system as claimed in claim 8, it is characterised in that：
The concave part in the first substrate portion of the Quick Release plate is opposite with the concave part position of the intermediate support, and the Quick Release
The concave part in the first substrate portion of plate merges the part for clamping the O-shaped shock ring with the concave part of the intermediate support
Arc structure.
10. a kind of unmanned plane, it is characterised in that：It include unmanned aerial vehicle body and as claim 1-9 any one of them without
Man-machine damping push and pull system；
Wherein, multiple upright bars of the unmanned plane damping push and pull system run through across the middle part of the unmanned aerial vehicle body；Institute
The upper support frame in unmanned plane damping push and pull system is stated for being fixedly connected with battery warehouse component, the unmanned plane damping push and pull system
On lower bracing frame for being fixedly connected with holder and fuselage Fast detachable unit；And multiple institutes in the unmanned plane damping push and pull system
Dampening assembly is stated to be located between the bottom of the unmanned aerial vehicle body and lower bracing frame top.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721297155.1U CN207550480U (en) | 2017-10-09 | 2017-10-09 | Unmanned plane damping push and pull system and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721297155.1U CN207550480U (en) | 2017-10-09 | 2017-10-09 | Unmanned plane damping push and pull system and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207550480U true CN207550480U (en) | 2018-06-29 |
Family
ID=62675337
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721297155.1U Expired - Fee Related CN207550480U (en) | 2017-10-09 | 2017-10-09 | Unmanned plane damping push and pull system and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207550480U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107640310A (en) * | 2017-10-09 | 2018-01-30 | 北京沃氏航空科技有限公司 | Unmanned plane damping push and pull system and unmanned plane |
-
2017
- 2017-10-09 CN CN201721297155.1U patent/CN207550480U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107640310A (en) * | 2017-10-09 | 2018-01-30 | 北京沃氏航空科技有限公司 | Unmanned plane damping push and pull system and unmanned plane |
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