CN205273870U - Novel aircraft of taking photo by plane - Google Patents
Novel aircraft of taking photo by plane Download PDFInfo
- Publication number
- CN205273870U CN205273870U CN201521136451.4U CN201521136451U CN205273870U CN 205273870 U CN205273870 U CN 205273870U CN 201521136451 U CN201521136451 U CN 201521136451U CN 205273870 U CN205273870 U CN 205273870U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- camera
- cell box
- aerial photography
- right cylinder
- 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
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Abstract
The utility model discloses a novel aircraft of taking photo by plane, including fuselage main part and fan blade, fuselage main part outside comprises last fuselage and lower fuselage, it corresponds middlely for square to go up fuselage and lower fuselage, outwards extend in the four corners, the outer end is vertical cylinder, it is hollow with the fuselage is inside down to go up the fuselage, operating the computer on one's body, the portion is equipped with the opening, the opening both ends are equipped with two draw -in grooves, the inside intermediate position of fuselage main part is equipped with the battery box, the battery box top is equipped with the camera subassembly, camera subassembly top is equipped with the pilot lamp, the battery box passes through the power supply of pin type plug intercommunication with the camera subassembly, the battery box below is equipped with the flight control PCB board, battery box and the power supply of flight control PCB board intercommunication, the downside is arranged in to the switch of flight control PCB board, switch department is equipped with switch cap. The utility model provides a novel aircraft of taking photo by plane equipment is simple, and the structure is firm, and multiple functional, relatively is fit for masses' taste, makes more people experience the enjoyment of taking photo by plane.
Description
Technical field
The utility model relates to a kind of aircraft, particularly relates to a kind of novel aerial photography aircraft.
Background technology
Along with the development in epoch, high-tech constantly incorporates our life, and this kind of new things of taking photo by plane have incorporated our life gradually, but existing aerial photography aircraft assembling trouble commercially, structure is unstable, it is easy to assembles unsuccessfully or awing damages.
Practical novel content
For above-mentioned deficiency, the purpose of this utility model is to provide the novel aerial photography aircraft of a kind of simple and convenient assembly, Stability Analysis of Structures.
The utility model is the technical scheme adopted that achieves the above object:
A kind of novel aerial photography aircraft, comprise fuselage main body and wind leaf, fuselage body exterior is made up of upper fuselage and lower fuselage, it is square in the middle of upper fuselage is corresponding with lower fuselage, corner outwards extends, outer end is for erecting to right cylinder, upper fuselage and lower fuselage interior are hollow, upper fuselage top is provided with opening, opening two ends are provided with two card grooves, fuselage body interior mid-way is provided with cell box, CCD camera assembly it is provided with above cell box, pilot lamp it is provided with above CCD camera assembly, cell box is connected power supply with CCD camera assembly by Pin contact, flight controlling pcb board it is provided with below cell box, cell box is connected power supply with flight controlling pcb board, the switch of flight controlling pcb board is placed in downside, switch place is provided with switch cap.
Described fuselage body top is provided with fuselage cover, and fuselage cover two ends are provided with card convex, interlocks with the card groove on upper fuselage, and fuselage cover is provided with transparent place, display pilot lamp.
Described CCD camera assembly comprises by camera, camera casting die, camera mounting block and camera control circuit board, camera be placed in shooting control circuit board before section, camera mounting block is in camera front, and camera casting die is above camera.
Described cell box covers under comprising cell box upper cover and cell box, and middle placement lithium cell, is fixed on cell box by battery button bit accessory.
The right cylinder inside of described fuselage main body corner is equipped with hollow cup motor, and hollow cup motor upper and lower is equipped with silica gel shock absorbing ring.
Described wind leaf is located at right cylinder top, fuselage corner, is connected with the hollow cup motor of right cylinder inside, fuselage main body corner, and four pieces of wind leaves comprise two pieces of motors and rotate forward wind leaf and two pieces of motor reversal maple leaves.
The right cylinder top of described fuselage corner is also respectively equipped with the protection frame extended to fuselage outer side.
The right cylinder front-end and back-end of described fuselage main body corner, are equipped with Transparent lamp shade.
Compared with prior art, the beneficial effects of the utility model are:
The novel aerial photography aircraft that the utility model provides uses upper fuselage, lower fuselage, cell box, CCD camera assembly, flight controlling pcb board, hollow cup motor, fan blade set to become aerial photography aircraft, structure left-hand seat simple, easy; More have that card is buckled concurrently, the combination of card groove, screw, lampshade and protection frame, this Flight Vehicle Structure is stablized; And the use of CCD camera assembly and flying vehicles control pcb board, enable aircraft realize the functions such as real-time photography, transmission, APP control flight.
The novel aerial photography aircraft assembling that the utility model provides is simple, and structure is firm, and function is perfect, is relatively applicable to popular taste, makes more people experience the enjoyment taken photo by plane.
Above-mentioned is the general introduction of practical new technique scheme, below in conjunction with accompanying drawing and embodiment, is described further by the utility model.
Accompanying drawing explanation
Fig. 1 is one-piece construction schematic diagram of the present utility model;
Fig. 2 is fuselage face cover structure schematic diagram of the present utility model;
Fig. 3 is CCD camera assembly structural representation of the present utility model;
Fig. 4 is battery pack structure schematic diagram of the present utility model.
In figure: 1, fuselage main body; 2, wind leaf; 3, frame is protected; 11, upper fuselage; 12, lower fuselage; 13, cell box; 14, CCD camera assembly; 15, flight controlling pcb board; 16, switch cap; 17, hollow cup motor; 18, silica gel shock absorbing ring; 19, fuselage cover; 20, pilot lamp; 21, lampshade; 111, card groove; 131, cell box upper cover; 132, cover under cell box; 133, lithium cell; 134, battery button bit accessory; 141, camera; 142, camera mounting block; 143, camera casting die; 144, camera control circuit board; 191, card convex 1; 192, card convex 2.
Embodiment
It is reach technique means and effect that predetermined object is taked for further setting forth the utility model, below in conjunction with accompanying drawing and better embodiment, embodiment of the present utility model is illustrated in detail.
As shown in Figure 1, a kind of novel aerial photography aircraft that the utility model provides, comprise fuselage main body (1) and wind leaf (2), fuselage main body (1) outside is made up of upper fuselage (11) and lower fuselage (12), use card to be buckled in bottle screw conjunction to lock together, it is square in the middle of upper fuselage (11) is corresponding with lower fuselage (12), corner outwards extends, outer end is for erecting to right cylinder, upper fuselage (11) and lower fuselage (12) inside are hollow, upper fuselage (11) top is provided with opening, opening two ends are provided with two card grooves (111), close with fuselage cover (19) button and use, fuselage main body (1) bosom position is provided with cell box (13), cell box (13) top is provided with CCD camera assembly (14), CCD camera assembly (14) top is provided with pilot lamp (20), whether pilot lamp (20) is used for display power supply and connects, cell box (13) is connected power supply with CCD camera assembly (14) by Pin contact, cell box (13) lower section is provided with flight controlling pcb board (15), flight controlling pcb board (15) is fixed in fuselage main body by four screws, cell box (13) is connected power supply with flight controlling pcb board (15), flight controlling pcb board (15) is possible not only to be connected with telepilot, can also be connected with mobile phone A PP by bluetooth or access of radio network, aircraft flight is controlled by mobile phone A PP. the switch of flight controlling pcb board (15) is placed in downside, and switch place is provided with switch cap (16). series of cells (13) is closely connected with flight controlling pcb board (15) with CCD camera assembly (14), avoids owing to fuselage rocks, collides the open circuit of generation. fuselage main body (1) top is provided with fuselage cover (19), conveniently check fuselage interior situation when not opening fuselage main body, fuselage cover (19) two ends are provided with card convex, as shown in Figure 2, the card convex 1(191 of front fuselage) horizontal forward, the card convex 2(192 of rear end) it is tilted to down, by fuselage panel (19) front end card convex 1(191) buckle conjunction with card groove (111), pressing fuselage panel (19) rear end, fuselage panel (19) and fuselage are buckled well, click again, fuselage panel (19) and fuselage are opened, fuselage cover (19) is provided with transparent place, it is used for showing pilot lamp (20). as shown in Figure 3, CCD camera assembly (14) comprises by camera (141), camera casting die (143), camera mounting block (142) and camera control circuit board (144), camera (141) is placed in shooting control circuit board (144) front section, camera mounting block (142) is in camera (141) front, camera casting die (143) is in camera (141) top, CCD camera assembly (14) is combined in Stability Analysis of Structures together, shooting control circuit board (144) has shooting and stores and transfer function, it may be achieved the real-time Transmission of shooting content. as shown in Figure 4, cell box (13) covers (132) under comprising cell box upper cover (131) and cell box, middle placement lithium cell (133), it is fixed on cell box (13) by battery button bit accessory (134), cell box (13) is positioned at position in the middle of fuselage main body (1), location security and being closely connected with needing power pack. the right cylinder inside of fuselage main body (1) corner is equipped with the hollow cup motor (17) of right cylinder, the internal space that hollow cup motor (17) is divided by fuselage outwardly extending portion is connected with flight controlling pcb board (15) with cell box (13), and hollow cup motor (17) upper and lower is equipped with silica gel shock absorbing ring (18), effectively for fuselage main body reaches the effect of damping.Wind leaf (2) is located at right cylinder top, fuselage corner, it is connected with the hollow cup motor (17) of right cylinder inside, fuselage main body (1) corner, four pieces of wind leaves (2) comprise two pieces of motors and rotate forward wind leaf and two pieces of motor reversal maple leaves, by rotating and reverse of wind leaf (2), increase convection of air, reach the effect of stable flight. The right cylinder top of fuselage main body (1) corner is also respectively equipped with the protection frame (3) extended to fuselage outer side; protection frame (3) is by the outside extension triangular in shape of right cylinder top; exceeding and turn on two jiaos outside wind leaf rotation scope rear triangle, available protecting wind leaf is not collided by foreign matter. The right cylinder front-end and back-end of fuselage main body (1) corner; it is equipped with Transparent lamp shade (21); lampshade (21) is buckled in fuselage (11) and lower fuselage (12) buckle well after respectively account for general circular hole place; bulb, transmission light can not only be protected, it is also possible to the stability that in increase, fuselage (11) and lower fuselage (12) button close.
The above; it it is only better embodiment of the present utility model; not technical scope of the present utility model is imposed any restrictions; therefore adopt the technology feature identical or approximate with the utility model above-described embodiment; and other the novel aerial photography aircraft obtained, all within protection domain of the present utility model.
Claims (8)
1. a novel aerial photography aircraft, comprise fuselage main body and wind leaf, it is characterized in that, fuselage body exterior is made up of upper fuselage and lower fuselage, it is square in the middle of upper fuselage is corresponding with lower fuselage, corner outwards extends, outer end is for erecting to right cylinder, upper fuselage and lower fuselage interior are hollow, upper fuselage top is provided with opening, opening two ends are provided with two card grooves, fuselage body interior mid-way is provided with cell box, CCD camera assembly it is provided with above cell box, pilot lamp it is provided with above CCD camera assembly, cell box is connected power supply with CCD camera assembly by Pin contact, flight controlling pcb board it is provided with below cell box, cell box is connected power supply with flight controlling pcb board, the switch of flight controlling pcb board is placed in downside, switch place is provided with switch cap.
2. novel aerial photography aircraft according to claim 1, it is characterised in that, described fuselage body top is provided with fuselage cover, and fuselage cover two ends are provided with card convex, interlocks with the card groove on upper fuselage, and fuselage cover is provided with transparent place, display pilot lamp.
3. novel aerial photography aircraft according to claim 1, it is characterized in that, described CCD camera assembly comprises by camera, camera casting die, camera mounting block and camera control circuit board, camera be placed in shooting control circuit board before section, camera mounting block is in camera front, and camera casting die is above camera.
4. novel aerial photography aircraft according to claim 1, it is characterised in that, described cell box covers under comprising cell box upper cover and cell box, and middle placement lithium cell, is fixed on cell box by battery button bit accessory.
5. novel aerial photography aircraft according to claim 1, it is characterised in that, the right cylinder inside of described fuselage main body corner is equipped with hollow cup motor, and hollow cup motor upper and lower is equipped with silica gel shock absorbing ring.
6. novel aerial photography aircraft according to claim 1, it is characterized in that, described wind leaf is located at right cylinder top, fuselage corner, is connected with the hollow cup motor of right cylinder inside, fuselage main body corner, and four pieces of wind leaves comprise two pieces of motors and rotate forward wind leaf and two pieces of motor reversal maple leaves.
7. novel aerial photography aircraft according to claim 1, it is characterised in that, the right cylinder top of described fuselage corner is also respectively equipped with the protection frame extended to fuselage outer side.
8. novel aerial photography aircraft according to claim 1, it is characterised in that, the right cylinder front-end and back-end of described fuselage main body corner, are equipped with Transparent lamp shade.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521136451.4U CN205273870U (en) | 2015-12-31 | 2015-12-31 | Novel aircraft of taking photo by plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521136451.4U CN205273870U (en) | 2015-12-31 | 2015-12-31 | Novel aircraft of taking photo by plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205273870U true CN205273870U (en) | 2016-06-01 |
Family
ID=56058471
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521136451.4U Expired - Fee Related CN205273870U (en) | 2015-12-31 | 2015-12-31 | Novel aircraft of taking photo by plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205273870U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105923143A (en) * | 2016-06-16 | 2016-09-07 | 深圳高科新农技术有限公司 | Stable and reliable four-rotor plant protection aircraft |
-
2015
- 2015-12-31 CN CN201521136451.4U patent/CN205273870U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105923143A (en) * | 2016-06-16 | 2016-09-07 | 深圳高科新农技术有限公司 | Stable and reliable four-rotor plant protection aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| 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: 20160601 Termination date: 20181231 |