CN209600794U - A kind of unmanned plane detects decoding apparatus - Google Patents
A kind of unmanned plane detects decoding apparatus Download PDFInfo
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- CN209600794U CN209600794U CN201920177506.8U CN201920177506U CN209600794U CN 209600794 U CN209600794 U CN 209600794U CN 201920177506 U CN201920177506 U CN 201920177506U CN 209600794 U CN209600794 U CN 209600794U
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- fuselage
- unmanned plane
- supporting leg
- decoding apparatus
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Abstract
The utility model discloses a kind of unmanned planes to detect decoding apparatus, including fuselage, the fuselage is equipped with several horns, the fuselage is additionally provided with the filming apparatus detachably installed, be characterized in that: the fuselage is equipped with several adjustment disks, several adjustment disks offer several adjustment holes, the fuselage is equipped with undercarriage, the undercarriage includes two supporting legs that are hinged with the fuselage and being oppositely arranged, the supporting leg sets to the concave fluted, the locating part for fixing the supporting leg and the adjustment disk and with the clamping of adjustment hole described in one is equipped in the groove, the supporting leg is equipped with the hollow connecting rod penetrated through with the groove, the shifting part for the locating part to be detached from adjustment hole described in one and connect with the locating part is equipped in the hollow connecting rod.The unmanned plane has to reduce to wear between filming apparatus and ground, plays a good protective effect to filming apparatus, guarantees the advantages of capture apparatus acquires clearly picture.
Description
Technical field
The utility model relates to airmanship fields, more specifically, it relates to which a kind of unmanned plane detects decoding apparatus.
Background technique
Unmanned plane is that have body using the not manned aircraft of radio robot and the presetting apparatus provided for oneself manipulation
Product small, low cost and it is easy to use the advantages that, compared with manned aircraft, unmanned plane be often more suitable for those too " it is slow-witted or
It is dangerous " task, unmanned plane can be divided by application field it is dual-use, wherein in civilian aspect unmanned plane combination industrial application
That unmanned plane has really just needed, at present take photo by plane, agricultural, plant protection, miniature self-timer, fast transportation, disaster relief, wild plant see
It examines, infectious disease monitoring, mapping, news report, electric inspection process, the disaster relief, the application in the fields such as movies-making.
With the continuous development of unmanned air vehicle technique, existing unmanned plane include fuselage, fuselage surrounding design have several horns,
Fuselage is equipped with dismountable capture apparatus, but existing unmanned plane, in decline, unmanned plane can drop to any on ground
Place, so can cause to wear to filming apparatus, the capture apparatus after abrasion, which has the acquisition of image, shoots unclear phenomenon,
Therefore there are also improve space.
Utility model content
In view of the deficienciess of the prior art, the purpose of this utility model is to provide a kind of unmanned planes to detect decoding apparatus, tool
It is reduced between filming apparatus and ground and wears, play a good protective effect to filming apparatus, guarantee that capture apparatus acquisition is clear
The advantages of clear picture.
To achieve the above object, the utility model provides following technical solution:
A kind of unmanned plane detects decoding apparatus, including fuselage, and the fuselage is equipped with several horns, and the fuselage is additionally provided with detachably
The filming apparatus of installation；The fuselage is equipped with several adjustment disks, and several adjustment disks offer several adjustment holes, the machine
Body is equipped with undercarriage, and the undercarriage includes two supporting legs that are hinged with the fuselage and being oppositely arranged, and the supporting leg is inside
It is recessed fluted, be equipped in the groove for by the supporting leg and the adjustment disk fix and with adjustment hole card described in one
The locating part connect, the supporting leg are equipped with the hollow connecting rod penetrated through with the groove, are equipped in the hollow connecting rod for inciting somebody to action
The shifting part that the locating part is detached from adjustment hole described in one and connect with the locating part.
By using above-mentioned technical proposal, by the setting of supporting leg, supporting leg plays the role of a support to fuselage,
So that unmanned plane in decline supporting leg first with ground face contact so that exist between filming apparatus and ground it is certain away from
From, and then play a protective role to filming apparatus, reduce the possibility of filming apparatus and ground friction damage, extends unmanned plane
Service life；The adjusting of tilt angle between supporting leg and ground is realized by the setting of adjustment disk, and then can basis
The case where actual ground, adjusts the tilt angle between supporting leg and ground, so that unmanned plane is whole more stable to be placed on ground
On face；Realized by the clamping between locating part and adjustment hole it is relatively fixed between supporting leg and adjustment disk, and by dialling
Moving part realizes the disengaging between locating part and adjustment hole, realizes the change of relative angle between supporting leg and adjustment disk, operation letter
It is single convenient and efficient；Certain booster action is played to supporting leg by the setting of hollow connecting rod simultaneously.
The utility model is further arranged to: the planform of the supporting leg is arranged in " U-shaped ", and the supporting leg includes
Cross bar and two vertical bars disposed in parallel, two described vertical bar one end and the fuselage are hinged, and two vertical bars are far from itself and the machine
One end of body is connect with the cross bar.
By using above-mentioned technical proposal, vertical bar plays the role of a support to fuselage, and cross bar plays one to vertical bar
The effect of connection, and the contact area between vertical bar and ground is increased by the setting of cross bar, and then enhance unmanned plane
The stability being placed on the ground；Simultaneously because it is hinged between vertical bar and fuselage, and by between locating part and adjustment hole
Angle is relatively fixed between clamping realization vertical bar and fuselage；Since vertical bar is hinged with fuselage, so cross bar also corresponds to one
The effect of handle, and then carry out taking and placing unmanned plane convenient for doing one's assignment personnel by cross bar, it is simple to operate quick.
The utility model is further arranged to: the locating part includes limited block and elastic component, described elastic component one end with
The limited block connection, the elastic component other end are connect with the groove slot bottom.
By using above-mentioned technical proposal, limited block squeezes elastic component and moves towards the direction close to groove slot bottom, works as adjusting
Limited block is under the action of the elastic member towards the direction movement far from groove slot bottom and then solid limit when hole is aligned with groove notch
Connecting and fixing between vertical bar and adjustment disk relatively is realized in clamping between block and adjustment hole, simple to operate quick.
The utility model is further arranged to: the hollow connecting rod offers slot, the shifting part include poke rod and
The planform of slide block, the poke rod is arranged in " L shape ", and described poke rod one end penetrates the slot and the limited block
Connection, the poke rod other end are pierced by the slot and connect with the slide block.
By using above-mentioned technical proposal, make driving lever that limited block adjacent thereto be driven to squeeze elasticity by stirring shifting block
Part is moved towards the direction close to groove slot bottom, and then realizes the disengaging between limited block and adjustment hole, so as to change support
Tilt angle between leg and fuselage is simple to operate quick.
The utility model is further arranged to: the cross bar is rotatably connected to shackle member, and shackle member includes and the cross bar
The interconnecting piece of rotation connection, the interconnecting piece are equipped with the elastic card socket part with another cross bar clamping.
By using above-mentioned technical proposal, in operating personnel's taking and placing unmanned plane, due to close to each other between two cross bars,
It is in disengaged position between limited block and adjustment hole, i.e. angle between vertical bar and adjustment disk can change, so
By the setting of shackle member, two cross bars can be linked together by elastic card socket part, and then reduce the pine between two cross bars
It is dynamic, convenient for operating personnel by the entire unmanned plane of cross bar taking and placing.
The utility model is further arranged to: the elastic component is spring, and spring one end is connect with the limited block, spring
The other end is connect with the groove slot bottom.
By using above-mentioned technical proposal, spring plays a connection function to limited block and groove slot bottom, and limited block exists
Spring is squeezed under the squeezing action of adjustment disk to move towards the direction close to groove, when adjustment hole is aligned with groove notch, limit
Block is moved towards the direction far from groove slot bottom under the elastic force effect of spring and is connected and fixed with adjustment hole, and then realizes supporting leg
Fixation between adjustment disk is simple to operate quick.
The utility model is further arranged to: the cross bar is concaved with non-slip texture along its length.
By using above-mentioned technical proposal, by the setting of non-slip texture, on the one hand when unmanned plane and ground touch,
It enhances the stability between cross bar and ground and then enhances the stability between unmanned plane entirety and ground；On the other hand horizontal
Bar is equivalent to the effect of a handle, and non-slip texture increases the frictional force between operating personnel and handle, and then is convenient for operation
The more stable taking and placing unmanned plane of personnel.
The utility model is further arranged to: one side of the horn close to ground is sticked and has phosphor strip.
By using above-mentioned technical proposal, by the phosphor strip that is sticked on fuselage, phosphor strip can under conditions of pitch-dark
Fluorescence is issued, so that unmanned plane flies with having certain suggesting effect to operating personnel, relatively under pitch-dark environment
For the equipment such as headlamp are installed on fuselage, electric energy is on the one hand saved, the theory of environment protecting and power-saving is embodied, it is another
Aspect phosphor strip alleviates the overall weight of unmanned plane for headlamp.
In conclusion the utility model has the following beneficial effects:
1. the utility model structure is simple, there is exploitativeness, a support is played to fuselage by the setting of supporting leg
Effect, and then reduce unmanned plane filming apparatus in lifting and and then filming apparatus played directly with ground contact wear
Certain protective effect extends the service life of filming apparatus；
2. since supporting leg is made of vertical bar and cross bar, the support that vertical bar plays the role of unmanned plane, the setting of cross bar
On the one hand a connection function is played to vertical bar and on the other hand increases the contact area between vertical bar and ground, enhance unmanned plane
The stability being placed on the ground；
3. by the setting of adjustable plate and several adjustment holes, so that relative angle between vertical bar and adjustable plate can be with
It adjusts, can be integrally placed to ground according to the angle adjusted between supporting leg and ground the case where actual ground, enhancing unmanned plane
Stability on face；
4. realized by the clamping between limited block and adjustment hole it is relatively fixed between vertical bar and adjustment disk, relative to
It is simple to operate quick for screw is locked；
5. making poke rod drive the limited block compressed spring being attached thereto towards close to groove slot bottom by stirring slide block
Direction movement, and then realize the disengaging between limited block and adjustment hole, it is simple to operate quick；
6. the setting by shackle member reduces the loosening between two cross bars, the taking and placing convenient for operating personnel to unmanned plane；
7. certain suggesting effect is played to operating personnel under pitch-dark environment, is embodied by the setting of phosphor strip
The theory of environment protecting and power-saving.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the structural schematic diagram of supporting leg；
Fig. 3 is the structural schematic diagram of locating part.
Appended drawing reference: 11, fuselage；12, horn；13, filming apparatus；14, phosphor strip；2, undercarriage；21, supporting leg；
211, vertical bar；212, cross bar；213, hollow connecting rod；214, non-slip texture；3, groove；31, locating part；311, limited block；312,
Elastic component；4, adjustment disk；41, adjustment hole；5, shifting part；50, slot；51, poke rod；52, slide block；6, shackle member；61, even
Socket part；62, elastic card socket part.
Specific embodiment
The utility model is described in further detail below in conjunction with attached drawing.
A kind of unmanned plane detects decoding apparatus, and as shown in Figs. 1-2, including fuselage 11, fuselage 11 circumferentially fixed is connected with four along its
A evenly arranged horn 12, fuselage 11 are also equipped with dismountable filming apparatus close to the center of the one side on ground
13。
One side of each horn 12 close to ground is sticked and has phosphor strip 14.
One side of the fuselage 11 close to ground is fixedly connected there are four adjustment disk 4, and the planform of adjustment disk 4 is in " semicircle
Shape " setting, four adjustment disks 4 are symmetrical set about the central axis of fuselage 11；If each adjustment disk 4 is offered along its circumferential direction
Do equally distributed adjustment hole 41.
Fuselage 11 is additionally provided with undercarriage 2, and undercarriage 2 includes two supporting legs 21 that are hinged with fuselage 11 and being oppositely arranged.
Each supporting leg 21 includes the vertical bar 211 of two mutual parallel vertical settings, and the planform of two vertical bars 211 is arc-shaped
Setting, two vertical bars, 211 one end and fuselage 11 are hinged, and two vertical bars 211 are fixedly connected with far from one end of itself and 11 hinge joint of fuselage
Connect the cross bar 212 of two vertical bars 211.
Two cross bars 212 are concaved with several evenly arranged non-slip textures 214 along its length.
Two cross bars 212 are respectively rotatably connected to a shackle member 6, and shackle member 6 includes interconnecting piece 61 and elastic card socket part 62, connect
It is fixedly connected between socket part 61 and elastic card socket part 62, the planform of interconnecting piece 61 is arranged in " circular ring shape ", elastic card socket part
62 planform is arranged in " hoop ", and elastic card socket part 62 is adapted to the mutually clamping of cross bar 212.
As Figure 2-3, two vertical bars 211 set to the concave fluted 3 close to the side of itself and 11 hinge joint of fuselage, groove 3
It is inside provided inwardly with for locating part 31 that is vertical bar 211 and adjustment disk 4 is fixed and being clamped with one adjustment hole 41.
Locating part 31 includes limited block 311 and elastic component 312, and elastic component 312 is spring, the radial section of limited block 311
Shape is arranged in " circle ", and spring one end is fixedly connected with limited block 311, and the spring other end is fixedly connected with 3 slot bottom of groove；It adjusts
The shape size of knothole 41 is adapted with limited block 311.
The hollow connecting rod 213 penetrated through with groove 3 is fixedly connected between two vertical bars 211, hollow connecting rod 213 offers slot
50, the shifting part 5 for limited block 311 to be detached from one adjustment hole 41 and connect with limited block 311 is equipped in slot 50,
Shifting part 5 includes poke rod 51 and slide block 52；The planform of poke rod 51 is arranged in " L shape ", and the radial direction of slide block 52 is cut
Face shape is arranged in " circle "；The radial cross-sectional area of poke rod 51 is less than the radial cross-sectional area of slide block 52；Poke rod 51
One end penetrates slot 50 and is fixedly connected with limited block 311, and 51 other end of poke rod is pierced by slot 50 and fixes with slide block 52
Connection.
It the concrete operating principle of the present embodiment and has the beneficial effect that
Working principle:
Operating personnel stirs slide block 52 and makes poke rod 51 that the limited block 311 that is attached thereto be driven to squeeze spring towards close
One end motion of 3 slot bottom of groove rotates the angle between the adjusting vertical bar 211 of vertical bar 211 and adjustment disk 4 according to actual ground situation
Degree decontrols slide block 52 after determining to angle, limited block 311 is under the effect of spring force towards the side close to adjustment hole 41
To moving and connecting and fixing with adjustment hole 41, connecting and fixing between vertical bar 211 and adjustment disk 4 can be realized.
The utility model has the advantages that
Play the role of a support to fuselage 11 by the setting of supporting leg 21, and then reduces unmanned plane in lifting
Filming apparatus 13 directly with ground contact wear, and then plays a certain protective role filming apparatus 13, extends shooting dress
Set 13 service life.
Since supporting leg 21 is made of vertical bar 211 and cross bar 212, the support that vertical bar 211 plays the role of unmanned plane is horizontal
On the one hand the setting of bar 212 plays a connection function to vertical bar 211 and on the other hand increases contact between vertical bar 211 and ground
Area enhances the stability that unmanned plane is placed on the ground.
By the setting of adjustable plate and several adjustment holes 41, so that the relative angle between vertical bar 211 and adjustable plate
It is adjustable, it can integrally be put according to the angle adjusted the case where actual ground between supporting leg 21 and ground, enhancing unmanned plane
Set stability on the ground.
Realized by the clamping between limited block 311 and adjustment hole 41 it is relatively fixed between vertical bar 211 and adjustment disk 4,
It is simple to operate quick for being locked with screw.
Poke rod 51 is made to drive 311 compressed spring of limited block being attached thereto towards close to groove by stirring slide block 52
The direction of 3 slot bottoms moves, and then realizes the disengaging between limited block 311 and adjustment hole 41, simple to operate quick.
Reduce the loosening between two cross bars 212 by the setting of shackle member 6, unmanned plane is taken convenient for operating personnel
It puts.
By the setting of phosphor strip 14, certain suggesting effect is played to operating personnel under pitch-dark environment, is embodied
The theory of environment protecting and power-saving.
This specific embodiment is only the explanation to the utility model, is not limitations of the present invention, ability
Field technique personnel can according to need the modification that not creative contribution is made to the present embodiment after reading this specification, but
As long as all by the protection of Patent Law in the scope of the claims of the utility model.
Claims (8)
1. a kind of unmanned plane detects decoding apparatus, including fuselage (11), the fuselage (11) is equipped with several horns (12), the fuselage
(11) it is additionally provided with the filming apparatus (13) detachably installed, it is characterised in that: the fuselage (11) is equipped with several adjustment disks (4),
Several adjustment disks (4) offer several adjustment holes (41), and the fuselage (11) is equipped with undercarriage (2), the undercarriage
It (2) include two supporting legs (21) that are hinged with the fuselage (11) and being oppositely arranged, the supporting leg (21) is concaved with recessed
Slot (3), the groove (3) is interior to be equipped with for fixing the supporting leg (21) and the adjustment disk (4) and adjusting with described in one
The locating part (31) of knothole (41) clamping, the supporting leg (21) are equipped with the hollow connecting rod (213) penetrated through with the groove (3),
Be equipped in the hollow connecting rod (213) for by the locating part (31) and adjustment hole described in one (41) disengaging and with it is described
The shifting part (5) of locating part (31) connection.
2. a kind of unmanned plane according to claim 1 detects decoding apparatus, it is characterised in that: the structure shape of the supporting leg (21)
Shape is arranged in " U-shaped ", and the supporting leg (21) includes cross bar (212) and two vertical bars (211) disposed in parallel, two vertical bars
(211) hingedly, two vertical bars (211) are far from its one end with the fuselage (11) and the cross for one end and the fuselage (11)
Bar (212) connection.
3. a kind of unmanned plane according to claim 1 detects decoding apparatus, it is characterised in that: the locating part (31) includes limit
Block (311) and elastic component (312), described elastic component (312) one end are connect with the limited block (311), the elastic component (312)
The other end is connect with the groove (3) slot bottom.
4. a kind of unmanned plane according to claim 3 detects decoding apparatus, it is characterised in that: the hollow connecting rod (213) opens up
Have slot (50), the shifting part (5) includes poke rod (51) and slide block (52), and the planform of the poke rod (51) is in
" L shape " setting, described poke rod (51) one end penetrate the slot (50) and connect with the limited block (311), the poke rod
(51) other end is pierced by the slot (50) and connect with the slide block (52).
5. a kind of unmanned plane according to claim 2 detects decoding apparatus, it is characterised in that: cross bar (212) rotation connection
Have shackle member (6), shackle member (6) includes the interconnecting piece (61) with the cross bar (212) rotation connection, and the interconnecting piece (61) sets
There is the elastic card socket part (62) with another cross bar (212) clamping.
6. a kind of unmanned plane according to claim 3 detects decoding apparatus, it is characterised in that: the elastic component (312) is spring,
Spring one end is connect with the limited block (311), and the spring other end is connect with the groove (3) slot bottom.
7. a kind of unmanned plane according to claim 2 detects decoding apparatus, it is characterised in that: the cross bar (212) is along its length
Direction is concaved with non-slip texture (214).
8. a kind of unmanned plane according to claim 1 detects decoding apparatus, it is characterised in that: the horn (12) is close to ground
One side, which is sticked, phosphor strip (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920177506.8U CN209600794U (en) | 2019-01-31 | 2019-01-31 | A kind of unmanned plane detects decoding apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920177506.8U CN209600794U (en) | 2019-01-31 | 2019-01-31 | A kind of unmanned plane detects decoding apparatus |
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| Publication Number | Publication Date |
|---|---|
| CN209600794U true CN209600794U (en) | 2019-11-08 |
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ID=68403158
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| Application Number | Title | Priority Date | Filing Date |
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| CN201920177506.8U Active CN209600794U (en) | 2019-01-31 | 2019-01-31 | A kind of unmanned plane detects decoding apparatus |
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| CN (1) | CN209600794U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112544395A (en) * | 2020-12-07 | 2021-03-26 | 山东省水利科学研究院 | Irrigation device based on unmanned aerial vehicle monitoring |
-
2019
- 2019-01-31 CN CN201920177506.8U patent/CN209600794U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112544395A (en) * | 2020-12-07 | 2021-03-26 | 山东省水利科学研究院 | Irrigation device based on unmanned aerial vehicle monitoring |
| CN112544395B (en) * | 2020-12-07 | 2022-05-27 | 山东省水利科学研究院 | Irrigation device based on unmanned aerial vehicle monitoring |
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