CN207129144U - A kind of carrier gas unmanned plane - Google Patents
A kind of carrier gas unmanned plane Download PDFInfo
- Publication number
- CN207129144U CN207129144U CN201720992975.6U CN201720992975U CN207129144U CN 207129144 U CN207129144 U CN 207129144U CN 201720992975 U CN201720992975 U CN 201720992975U CN 207129144 U CN207129144 U CN 207129144U
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- CN
- China
- Prior art keywords
- unmanned plane
- lens barrel
- carrier gas
- filming apparatus
- support frame
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Abstract
The utility model discloses a kind of carrier gas unmanned plane, its structure includes filming apparatus, adjusting rod, power supply indicator, bolt, unmanned plane lower half, rotor blade, rotating shaft, power connector block, the unmanned plane first half, gas tank, support frame, is welded at the top of unmanned plane lower half with unmanned plane first half bottom；Filming apparatus is made up of high-definition camera, safety glass, lens barrel, fixed block, video camera body, video camera body front end and lens barrel connecting as one structure, high-definition camera is housed inside lens barrel, safety glass is embedded in lens barrel front end, and video camera body side is welded with fixed block side, and fixed block bottom side at the top of support frame with being fixedly connected, the utility model adds filming apparatus, the equipment can realize shoot function, increase use range, improve use value.
Description
Technical field
The utility model is a kind of carrier gas unmanned plane, belongs to carrier gas unmanned plane field.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without driving cabin on machine, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or
Machine tool remote control station personnel are tracked to it, positioned, being remotely controlled, remote measurement and Digital Transmission by equipment such as radars.Can be in radio
Take off as conventional airplane or launched with booster rocket under remote control, can also take aerial launch to by machine tool and fly.Recovery
When, the mode automatic Landing as conventional airplane landing mission can be used, can also be reclaimed by remote control parachute or block.Can
It is reused several times.It is widely used in aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc..
Prior art discloses Application No.：201620081410.8 carrier gas unmanned plane disclosed in utility model, including nothing
Man-machine body and system for flight control computer；Also include four gas tanks being arranged in the frame of the unmanned plane body；Wherein：Institute
The lower section that gas tank is fixed on the frame is stated, the tail end of the gas tank is fixedly connected with the frame, and the top of the gas tank is set
Valve, the valve set corresponding valve plug, and the valve plug seals the valve and the valve plug connecting valve is opened
Close, the valve switch controls the open and close of the valve plug, and the valve switch electrically connects steering wheel, the steering wheel signal connection
The system for flight control computer, fill in the gas tank and put gas；The quality of four gas tanks is equal.It is provided by the utility model
Carrier gas unmanned plane solve thes problems, such as safety issue and the continuation of the journey of unmanned plane.But prior art imperfection, the equipment without
Method realizes shoot function, single using function, reduces use value.
Utility model content
In view of the deficienciess of the prior art, the utility model purpose is to provide a kind of carrier gas unmanned plane, it is existing to solve
Technology imperfection, the equipment can not realize shoot function, single using function, reduce use value.
To achieve these goals, the utility model is to realize a kind of carrier gas unmanned plane by the following technical solutions,
Its structure includes filming apparatus, adjusting rod, power supply indicator, bolt, unmanned plane lower half, rotor blade, rotating shaft, power connector
Block, the unmanned plane first half, gas tank, support frame, the unmanned plane lower half top is welded with unmanned plane first half bottom, described dynamic
Power contiguous block is sequentially arranged on the unmanned plane first half according to square structure, and the rotating shaft bottom is connected in power connector block
Portion, the rotating shaft side are equipped with rotor blade, and the stud base is connected to unmanned plane lower half, institute through the unmanned plane first half
State unmanned plane lower half bottom to be connected with adjusting rod plan vertical, the adjusting rod bottom is welded with filming apparatus back, described
Filming apparatus bottom is described with unmanned plane lower half bottom vertical connection at the top of the gas tank with being fixedly connected at the top of support frame
Support frame side is welded with gas tank side, and the unmanned plane first half front end is provided with power supply indicator；The filming apparatus is by height
Clear camera, safety glass, lens barrel, fixed block, video camera body composition, the video camera body front end and connecting as one of lens barrel
Structure, be equipped with high-definition camera inside the lens barrel, and the safety glass is embedded in lens barrel front end, the video camera body side and
Fixed block side is welded, and the fixed block bottom side at the top of support frame with being fixedly connected.
Further, the unmanned plane first half is provided with through hole, and the through hole and bolt are concentric circles.
Further, the bolt side mechanically connects with being used inside the unmanned plane first half.
Further, the gas tank is cylindrical structure.
Further, the gas tank is symmetric.
Further, the adjusting rod is used for the angle for adjusting shooting.
Further, the power supply indicator is used to indicate whether carrier gas unmanned plane is in running order.
The utility model adds filming apparatus, and the equipment can realize shoot function, increases use range, improves and uses
Value.
Brief description of the drawings
It is of the present utility model other by reading the detailed description made with reference to the following drawings to non-limiting example
Feature, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural representation of carrier gas unmanned plane of the utility model.
Fig. 2 is the structural representation of this practical filming apparatus.
In figure：Filming apparatus -1, adjusting rod -2, power supply indicator -3, bolt -4, unmanned plane lower half -5, rotor blade -
6th, rotating shaft -7, power connector block -8, the unmanned plane first half -9, gas tank -10, support frame -11, high-definition camera -101, tempering glass
Glass -102, lens barrel -103, fixed block -104, video camera body -105.
Embodiment
Technological means, creation characteristic, reached purpose and effect to realize the utility model are easy to understand, below
With reference to embodiment, the utility model is expanded on further.
Fig. 1, Fig. 2 are referred to, the utility model provides a kind of carrier gas unmanned air vehicle technique scheme：Its structure includes filming apparatus
1st, adjusting rod 2, power supply indicator 3, bolt 4, unmanned plane lower half 5, rotor blade 6, rotating shaft 7, power connector block 8, unmanned plane
The first half 9, gas tank 10, support frame 11, the top of unmanned plane lower half 5 are welded with the bottom of the unmanned plane first half 9, the power
Contiguous block 8 is sequentially arranged on the unmanned plane first half 9 according to square structure, and the bottom of rotating shaft 7 is connected to power connector block 8
Inside, the side of rotating shaft 7 are equipped with rotor blade 6, and the bottom of bolt 4 is connected under unmanned plane through the unmanned plane first half 9
Half portion 5, the bottom of unmanned plane lower half 5 are connected with the plan vertical of adjusting rod 2, and the bottom of adjusting rod 2 is carried on the back with filming apparatus 1
Portion is welded, and the bottom of filming apparatus 1 is fixedly connected with the top of support frame 11, the top of gas tank 10 and unmanned plane lower half 5
Bottom vertical connection, the side of support frame as described above 11 are welded with the side of gas tank 10, and the front end of the unmanned plane first half 9 refers to provided with power supply
Show lamp 3；The filming apparatus 1 is by high-definition camera 101, safety glass 102, lens barrel 103, fixed block 104, video camera body 105
Composition, the front end of video camera body 105 and the connecting as one structure of lens barrel 103, the inside of lens barrel 103 are equipped with high-definition camera
First 101, the safety glass 102 is embedded in the front end of lens barrel 103, and the side of video camera body 105 is welded with the side of fixed block 104
Connect, the bottom side of fixed block 104 is fixedly connected with the top of support frame 11, and the unmanned plane first half 9 is provided with through hole, described logical
Hole is concentric circles with bolt 4, and the side of bolt 4 is using mechanical connection, the gas tank 10 with the inside of the unmanned plane first half 9
Cylindrical structure, the gas tank 10 are symmetric, and the adjusting rod 2 is used for the angle for adjusting shooting, the power supply indicator 3
For indicating whether carrier gas unmanned plane is in running order.
High-definition camera 101 described in this patent refers to HD 1080P or HD 960P or HD 720P camera, camera lens
Element must use five layers of glass lens, because all-glass certainly well more many than plastic cement+glass definition.
It is high in progress in use, we need to realize that carrier gas unmanned plane shoots surface state by filming apparatus 1
Clear camera 101 refers to HD 1080P or HD 960P or HD 720P camera, and safety glass 102 can protect high definition to take the photograph
It is not destroyed as first 101, reduces use cost, rotor blade 6 can carries out high speed rotation, drive carrier gas unmanned plane to be flown
OK, for example, adding filming apparatus, the equipment can realize shoot function, increase use range, improve use value.
Filming apparatus 1 of the present utility model, adjusting rod 2, power supply indicator 3, bolt 4, unmanned plane lower half 5, whirler
The wing 6, rotating shaft 7, power connector block 8, the unmanned plane first half 9, gas tank 10, support frame 11, high-definition camera 101, safety glass
102nd, lens barrel 103, fixed block 104, video camera body 105.The portion that part is universal standard part or those skilled in the art know
Part, its structure and principle all can be learnt by technical manual or be known by normal experiment method, this reality for this technology personnel
Solve the problems, such as it is prior art imperfection with new, the equipment can not realize shoot function, single using function, reduce and use
Value, the utility model are combined with each other by above-mentioned part, add filming apparatus, and the equipment can realize shoot function,
Increase use range, improve use value, it is described in detail below：
The filming apparatus 1 is by high-definition camera 101, safety glass 102, lens barrel 103, fixed block 104, video camera body
105 compositions, the front end of video camera body 105 and the connecting as one structure of lens barrel 103, the inside of lens barrel 103 are equipped with high definition
Camera 101, the safety glass 102 are embedded in the front end of lens barrel 103, the side of video camera body 105 and the side of fixed block 104
Welding, the bottom side of fixed block 104 are fixedly connected with the top of support frame 11.
The top of first company unmanned plane lower half 5 is welded with the bottom of the unmanned plane first half 9, and company B's unmanned plane lower half 5 is pushed up
Portion is fitted and connected with the bottom of the unmanned plane first half 9.
First company built-up time is 40min, and using effect is good；
Company B's built-up time is 60min, it is very difficult to is used；
This practical top of unmanned plane lower half 5 is welded with the bottom of the unmanned plane first half 9 in summary, and performance is more preferable,
It is worth advocating.
The advantages of general principle and principal character of the present utility model and the utility model has been shown and described above, for
For those skilled in the art, it is clear that the utility model is not limited to the details of above-mentioned one exemplary embodiment, 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, embodiment all should be regarded as exemplary, and be nonrestrictive, the scope of the utility model is by institute
Attached claim rather than described above limit, it is intended that will fall in the implication and scope of the equivalency of claim
All changes are included in the utility model.Any reference in claim should not be considered as to the involved right of limitation
It is required that.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that those skilled in the art should for clarity
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms this area note technology people
The other embodiment that member is appreciated that.
Claims (5)
1. a kind of carrier gas unmanned plane, its structure includes filming apparatus (1), adjusting rod (2), power supply indicator (3), bolt (4), nothing
Man-machine lower half (5), rotor blade (6), rotating shaft (7), power connector block (8), the unmanned plane first half (9), gas tank (10), support
Frame (11), welded with the unmanned plane first half (9) bottom at the top of the unmanned plane lower half (5), the power connector block (8) according to
Square structure is sequentially arranged on the unmanned plane first half (9), and rotating shaft (7) bottom is connected to power connector block (8) inside,
Rotating shaft (7) side is equipped with rotor blade (6), it is characterised in that：
Bolt (4) bottom is connected to unmanned plane lower half (5), the unmanned plane lower half through the unmanned plane first half (9)
(5) bottom is connected with adjusting rod (2) plan vertical, and adjusting rod (2) bottom is welded with filming apparatus (1) back, the bat
Device (1) bottom is taken the photograph with being fixedly connected at the top of support frame (11), is hung down at the top of the gas tank (10) with unmanned plane lower half (5) bottom
Direct-connected to connect, support frame as described above (11) side is welded with gas tank (10) side, and the unmanned plane first half (9) front end refers to provided with power supply
Show lamp (3)；
The filming apparatus (1) is by high-definition camera (101), safety glass (102), lens barrel (103), fixed block (104), shooting
Body (105) forms, video camera body (105) front end and lens barrel (103) connecting as one structure, the lens barrel (103)
Inside is equipped with high-definition camera (101), and the safety glass (102) is embedded in lens barrel (103) front end, the video camera body
(105) side is welded with fixed block (104) side, and fixed block (104) bottom side at the top of support frame (11) with being fixedly connected.
A kind of 2. carrier gas unmanned plane according to claim 1, it is characterised in that：The unmanned plane first half (9) is provided with
Through hole, the through hole and bolt (4) are concentric circles.
A kind of 3. carrier gas unmanned plane according to claim 1, it is characterised in that：On bolt (4) side and unmanned plane
Using mechanical connection inside half portion (9).
A kind of 4. carrier gas unmanned plane according to claim 1, it is characterised in that：The gas tank (10) is cylindrical structure.
A kind of 5. carrier gas unmanned plane according to claim 1, it is characterised in that：The gas tank (10) is symmetric.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720992975.6U CN207129144U (en) | 2017-08-09 | 2017-08-09 | A kind of carrier gas unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720992975.6U CN207129144U (en) | 2017-08-09 | 2017-08-09 | A kind of carrier gas unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207129144U true CN207129144U (en) | 2018-03-23 |
Family
ID=61640850
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720992975.6U Expired - Fee Related CN207129144U (en) | 2017-08-09 | 2017-08-09 | A kind of carrier gas unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207129144U (en) |
-
2017
- 2017-08-09 CN CN201720992975.6U patent/CN207129144U/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: 20180323 Termination date: 20180809 |