CN207191424U - A kind of unmanned plane rises and falls support - Google Patents
A kind of unmanned plane rises and falls support Download PDFInfo
- Publication number
- CN207191424U CN207191424U CN201721119865.5U CN201721119865U CN207191424U CN 207191424 U CN207191424 U CN 207191424U CN 201721119865 U CN201721119865 U CN 201721119865U CN 207191424 U CN207191424 U CN 207191424U
- Authority
- CN
- China
- Prior art keywords
- support
- unmanned plane
- fuselage
- fixed support
- falls
- 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.)
- Expired - Fee Related
Links
Landscapes
- Mobile Radio Communication Systems (AREA)
Abstract
It the utility model is related to unmanned air vehicle technique field,In particular a kind of unmanned plane rises and falls support,Including fuselage,Machine top pressure closing lid and the chassis for being arranged on fuselage lower surface,Fuselage is provided with motor drive mechanism and actuating mechanism,Fuselage and state and be provided with shock absorbing ring between machine top pressure closing lid,Connection box is provided between shock absorbing ring and fuselage,Connection box outer surfac is provided with multiple swivel joints,Swivel joint is provided with raising frame,Raising frame is provided with Wing Joint,Chassis lower surface is provided with two fixed supports,And fixed support is in the symmetrical distribution in chassis lower surface,Load-bearing transverse axis is provided between two fixed supports,Fixed support both sides are provided with bracket groove,Bracket groove is equipped with extruding sliding block up and down,Support of stopping over is provided with fixed support,Support of stopping over is stopped over being equipped with buffering below fixed support,This unmanned plane rises and falls support,It is easy to use,Meet varying environment rise and fall require while,Unmanned plane is significantly increased to rise and fall the flexibility of support,Suitable for promoting and using on a large scale.
Description
Technical field
Unmanned air vehicle technique field is the utility model is related to, specially a kind of unmanned plane rises and falls support.
Background technology
At present, unmanned plane represents equipment as the forward position of sci-tech product, and its application is also increasingly wider, more such as surveys
The high-altitude dangerous operation such as examine, rescue, taking photo by plane, replacing manual work with Intelligent unattended machine, the effect of unmanned plane just seems especially
It is prominent.
However, the time come into operation with unmanned plane is increasingly longer, different using areas will to rising and falling for unmanned plane
Ask and just seem very harsh, at present, nobody support that rises and falls of tradition is mostly fixed bracket, or hand foldable support, due to
The stationarity of its structure causes it can not meet some special environmental requirements so that based on the work high above the ground of unmanned plane without
Method is resolved, larger puzzlement of having been taken to user, and because traditional unmanned plane rises and falls the hard property of support so that nothing
The man-machine flexibility when rising and falling greatly is limited, and is additionally, since fixed bracket, or hand foldable support can not be from homophony
Section property so that unmanned plane can be damaged in landing by larger impulse force.A kind of in consideration of it, branch it is proposed that unmanned plane rises and falls
Frame.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane and risen and fallen support, to solve what is proposed in above-mentioned background technology
The problems such as limitation is big, flexibility is low.
To achieve the above object, the utility model provides following technical scheme：
A kind of unmanned plane rises and falls support, including fuselage, machine top pressure closing lid and the chassis for being arranged on fuselage lower surface, described
Fuselage is provided with motor drive mechanism and actuating mechanism, and shock absorbing ring, the damping are provided between the fuselage and the machine top pressure closing lid
Connection box is provided between circle and fuselage, the connection box outer surfac is provided with multiple swivel joints, is provided with inside the swivel joint
Gear shaft, the swivel joint are provided with raising frame, and the raising frame is provided with Wing Joint；
The chassis lower surface is provided with two fixed supports, and fixed support is in the symmetrical distribution in chassis lower surface, institute
State and load-bearing transverse axis is provided between two fixed supports, the fixed support both sides are provided with bracket groove, and the bracket groove is equipped with up and down
Sliding block is extruded, support of stopping over is provided with the fixed support, described stop over is provided with damping spring circle between support and fixed support,
The support of stopping over is provided with spacing ball, and the support of stopping over is stopped over being equipped with buffering below fixed support, and the buffering falls
Support foot plate is provided with inside pin, this has extension spring block between the support foot plate and buffering are stopped over, and the support foot plate lower surface is provided with
Several movement legs.
Preferably, the gear hole that the raising machine frame inside is provided with and gear shaft matches.
Preferably, the number of the swivel joint is no less than four, and is in uniform equidistantly distributed in connection box outer surfac.
Preferably, the load-bearing transverse axis is screwed with the fixed support by screw thread is fastenedly connected.
Preferably, the support half of stopping over is through in fixed support, and is fastenedly connected with fixed support by nut.
Preferably, the number of the mobile leg is no less than eight, and is in uniform equidistantly distributed in support foot plate lower surface.
Compared with prior art, the beneficial effects of the utility model：
1st, in the utility model, by the gear that raising machine frame inside is provided with and swivel joint inner teeth wheel shaft matches
Hole, realize that signal is connected with the external world by electrical control mechanism, so as to control the clutch degree of raising frame, and then greatly increase nothing
Man-machine flexibility so that unmanned plane can meet the requirement of taking off of varying environment, simple in construction, reasonable in design；
2nd, in the utility model, by stopping over support and fixed support matches, it is subject to the booster action of load-bearing transverse axis, and
Not using tradition, nobody rises and falls support as fixed bracket, or the mode of hand foldable support, support of stopping over borrow fixed support pair
Landing is adjusted, and solves the problems, such as that the limitation brought during the landing of traditional unmanned plane is excessive；
3rd, in the utility model, by by the rational design of structure, by being provided between fixed support and chassis
Damping spring circle, extension spring block is provided between support foot plate and support of stopping over, can greatly avoid unmanned plane in landing
Wait the impulse force damage brought；
4th, in the utility model, extruding sliding block can cause the bracket groove support that will stop over to be securely seated between fixed support
Interior, shock absorbing ring allows the pressing that machine top pressure closing lid fastens, and greatly increases the service life of device；
This unmanned plane rises and falls support, easy to use, meet varying environment rise and fall require while, significantly increase
Unmanned plane rises and falls the flexibility of support, suitable for promoting and using on a large scale.
Brief description of the drawings
Fig. 1 is the utility model overall structure diagram；
Fig. 2 is that this practicality is stopped over supporting structure schematic diagram；
Fig. 3 is this real swivel joint internal structure schematic diagram；
In figure：Fuselage 1, machine top pressure closing lid 2, connection box 3, raising frame 4, shock absorbing ring 5, Wing Joint 6, swivel joint
7th, motor drive mechanism 8, actuating mechanism 9, chassis 10, extruding sliding block 11, damping spring circle 12, bracket groove 13, stop over support 14, load-bearing
Transverse axis 15, fixed support 16, buffer 17, spacing ball 18 of stopping over, extension spring block 19, support foot plate 20, mobile leg 21, gear shaft
22。
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Fig. 1-3 are referred to, the utility model provides a kind of technical scheme：
A kind of unmanned plane rises and falls support, including fuselage 1, machine top pressure closing lid 2 and the chassis for being arranged on the lower surface of fuselage 1
10, fuselage 1 is provided with motor drive mechanism 8 and actuating mechanism 9, and shock absorbing ring 5, shock absorbing ring 5 are provided between fuselage 1 and machine top pressure closing lid 2
The pressing that machine top pressure closing lid 2 is fastened, greatly increase the service life of device, be provided between shock absorbing ring 5 and fuselage 1
Box 3 is connected, connection box 3 outer surface is provided with multiple swivel joints 7, and the number of swivel joint 7 is no less than four, and in connection box 3
Outer surface is in uniform equidistantly distributed, and the inside of swivel joint 7 is provided with gear shaft 22, and swivel joint 7 is provided with raising frame 4, rises
Rise the gear hole that the inside of frame 4 is provided with and gear shaft 22 matches, by be provided with inside raising frame 4 and swivel joint 7 in
The gear hole that portion's gear shaft 22 matches, realize that signal is connected with the external world by electrical control mechanism 8, so as to control raising frame 4
Clutch degree, and then greatly increase the flexibility of unmanned plane so that unmanned plane can meet the requirement of taking off of varying environment, rise
Rise frame 4 and be provided with Wing Joint 6.
The lower surface of chassis 10 is provided with two fixed supports 16, and fixed support 16 is symmetrical point of the lower surface of chassis 10
Cloth, load-bearing transverse axis 15 is provided between two fixed supports 16, load-bearing transverse axis 15 is screwed by screw thread with fixed support 16 and is fastenedly connected,
The both sides of fixed support 16 are provided with bracket groove 13, and bracket groove is equipped with extruding sliding block 11 about 13, extruding sliding block 11 can to prop up
The support 14 that will stop over of rack slot 13 is securely seated between in fixed support 16, improves stability during unmanned plane landing, fixed branch
Support 14 of stopping over is provided with frame 16, support 14 half of stopping over is and tight by nut with fixed support 16 through in fixed support 16
It is solidly connected, by stopping over support 14 and fixed support 16 matches, is subject to the booster action of load-bearing transverse axis 15, without using tradition
Nobody support that rises and falls is fixed bracket, or the mode of hand foldable support, support 14 of stopping over borrow fixed support 16 to land into
Row regulation, solve the problems, such as that the limitation brought during the landing of traditional unmanned plane is excessive, stop over support 14 and fixed support 16 it
Between be provided with damping spring circle 12, support 14 of stopping over is provided with spacing ball 18, and the lower section of support 14 and fixed support 16 of stopping over is equipped with
Buffering stops over 17, and buffering 17 inside of stopping over are provided with support foot plate 20, and support foot plate 20 and buffering are stopped between 17, and this has extension spring block
19, by by the rational design of structure, by being provided with damping spring circle 12 between fixed support 16 and chassis 10, propping up
Extension spring block 19 is provided between sole 20 and support 14 of stopping over, can greatly avoid what unmanned plane was brought in landing
Impulse force damages, and the lower surface of support foot plate 20 is provided with several movement legs 21, and the number of mobile leg 21 is no less than eight, and is propping up
The lower surface of sole 20 is in uniform equidistantly distributed.
The advantages of general principle of the present utility model, principal character and the utility model has been shown and described above.One's own profession
The technical staff of industry is it should be appreciated that the utility model is not restricted to the described embodiments, described in above-described embodiment and specification
Be only preference of the present utility model, be not intended to limit the utility model, do not departing from the spirit and scope of the utility model
On the premise of, the utility model also has various changes and modifications, and these changes and improvements both fall within this claimed practicality
In new scope.The utility model requires protection scope is by appended claims and its equivalent thereof.
Claims (6)
- The support 1. a kind of unmanned plane rises and falls, including fuselage (1), machine top pressure closing lid (2) and the bottom for being arranged on fuselage (1) lower surface Disk (10), it is characterised in that：The fuselage (1) is provided with motor drive mechanism (8) and actuating mechanism (9), the fuselage (1) and the machine top pressure closing lid (2) Between be provided with shock absorbing ring (5), between the shock absorbing ring (5) and fuselage (1) be provided with connection box (3), it is described connection box (3) outer surface Provided with multiple swivel joints (7), gear shaft (22) is provided with inside the swivel joint (7), the swivel joint (7) is provided with Frame (4) is risen, the raising frame (4) is provided with Wing Joint (6)；Chassis (10) lower surface is provided with two fixed supports (16), and fixed support (16) is in chassis (10) lower surface or so It is symmetrical, load-bearing transverse axis (15) is provided between two fixed support (16), fixed support (16) both sides are provided with support Groove (13), the bracket groove (13) are equipped with extruding sliding block (11), support of stopping over are provided with the fixed support (16) up and down (14) damping spring circle (12), is provided between the support of stopping over (14) and fixed support (16), on the support of stopping over (14) Provided with spacing ball (18), the support of stopping over (14) is stopped over (17) with being equipped with buffering below fixed support (16), the buffering Stopping over, (17) are internal to be provided with support foot plate (20), and this has extension spring block (19), institute between the support foot plate (20) and buffering are stopped over Support foot plate (20) lower surface is stated provided with several movement legs (21).
- The support 2. a kind of unmanned plane according to claim 1 rises and falls, it is characterised in that：Set inside the raising frame (4) There is the gear hole to match with gear shaft (22).
- The support 3. a kind of unmanned plane according to claim 1 rises and falls, it is characterised in that：The number of the swivel joint (7) It is in uniform equidistantly distributed no less than four, and in connection box (3) outer surface.
- The support 4. a kind of unmanned plane according to claim 1 rises and falls, it is characterised in that：The load-bearing transverse axis (15) with it is described Fixed support (16) is screwed by screw thread to be fastenedly connected.
- The support 5. a kind of unmanned plane according to claim 1 rises and falls, it is characterised in that：The support of stopping over (14) is partly run through In fixed support (16), and it is fastenedly connected with fixed support (16) by nut.
- The support 6. a kind of unmanned plane according to claim 1 rises and falls, it is characterised in that：The number of the mobile leg (21) It is in uniform equidistantly distributed no less than eight, and in support foot plate (20) lower surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721119865.5U CN207191424U (en) | 2017-09-04 | 2017-09-04 | A kind of unmanned plane rises and falls support |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721119865.5U CN207191424U (en) | 2017-09-04 | 2017-09-04 | A kind of unmanned plane rises and falls support |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207191424U true CN207191424U (en) | 2018-04-06 |
Family
ID=61790627
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721119865.5U Expired - Fee Related CN207191424U (en) | 2017-09-04 | 2017-09-04 | A kind of unmanned plane rises and falls support |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207191424U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639543A (en) * | 2018-06-22 | 2018-10-12 | 江苏永康机械有限公司 | A kind of device of High Speed Transfer article |
-
2017
- 2017-09-04 CN CN201721119865.5U patent/CN207191424U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639543A (en) * | 2018-06-22 | 2018-10-12 | 江苏永康机械有限公司 | A kind of device of High Speed Transfer article |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102717897B (en) | Aerodynamic loading system and loading method for undercarriage self-control spring-damping system | |
| CN207191424U (en) | A kind of unmanned plane rises and falls support | |
| CN206785917U (en) | A kind of damping feet for motor work | |
| CN204312525U (en) | Loading universal joint | |
| CN206767413U (en) | A kind of lifting sucker of building glass | |
| CN205919320U (en) | Preparation of fat end is planted with steady low noise vibratory liquefaction bed to no trans -fatty acid | |
| CN204868622U (en) | Take self -locking function's automobile engine support anchor clamps | |
| CN207886875U (en) | A kind of fog gun machine being easily installed | |
| CN206592251U (en) | A kind of ECOLOGICAL ENVIRONMENTAL MONITORING equipment | |
| CN207101806U (en) | A kind of P.E. teacher's basketball frame for training | |
| CN210284600U (en) | A undercarriage for unmanned aerial vehicle | |
| CN204015549U (en) | Foldable table tennis table | |
| CN206724713U (en) | Anti-collapse support meanss when a kind of tunnel kiln is built | |
| CN108528687B (en) | Adjustable intelligent landing gear of amphibious aircraft | |
| CN203448952U (en) | Gear hot jacket workbench of locomotive gear box | |
| CN206970101U (en) | A kind of power plant steam turbine cylinder jacking system | |
| CN206760862U (en) | A kind of dress designing trunk Model rack | |
| CN207101867U (en) | A kind of swing limiter | |
| CN207157560U (en) | A kind of integral truss-type aircraft wing structure of hanging rack | |
| CN204549979U (en) | A kind of high-altitude operation platform | |
| CN211289426U (en) | High equipment base of stability | |
| CN204507484U (en) | Plastic bag sack launches bracing frame | |
| CN208616210U (en) | Huge suspension is floatd the panel construction of row device | |
| CN207748792U (en) | A kind of fixed fork hydraulic lifting Cargo Lift | |
| CN106314767B (en) | A kind of lightweight undercarriage for solar energy unmanned plane |
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: 20180406 Termination date: 20200904 |