CN203666990U - Unmanned plane carrying photographing device - Google Patents
Unmanned plane carrying photographing device Download PDFInfo
- Publication number
- CN203666990U CN203666990U CN201320736151.4U CN201320736151U CN203666990U CN 203666990 U CN203666990 U CN 203666990U CN 201320736151 U CN201320736151 U CN 201320736151U CN 203666990 U CN203666990 U CN 203666990U
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- photographing device
- fuselage
- unmanned plane
- tail
- plane body
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Abstract
The utility model provides an unmanned plane carrying a photographing device. The unmanned plane comprises a plane body, wings, a V-shaped tail wing, a tail pipe and a power device, wherein the wings are integrally formed with the plane body; the tail pipe is used for connecting the plane body with the V-shaped tail wing; the power device is positioned at the front part of the plane body; smooth round corners are arranged at the joints of the plane body and the wings; the tail pipe is a hollow metal pipe, one end of the tail pipe is fixedly connected with the tail end of the plane body, and the other end of the tail pipe is provided with the V-shaped tail wing; a photographing device carrying device is arranged inside the plane body; a photographing device lens carried inside the photographing device carrying device can be used for photographing the ground through a through hole formed in the bottom surface of the plane body. The unmanned plane has the advantages and benefits that the plane body is specially designed for reducing weight in order to carry the relatively heavy photographing device; the modified structural design of the plane body and the stabilized structure of the photographing device facilitate photographing ground pictures with high stability for a long time.
Description
Technical field
The utility model belongs to aerospace flight vehicle field, especially relates to a kind of unmanned plane that carries photographing device.
Background technology
Robot airplane is called for short " unmanned plane ", is the not manned aircraft that utilizes radio robot and the process controller of providing for oneself to handle.On machine, without driving compartment, but the equipment such as autopilot, process controller is installed.
Mainly bearing landforms for the unmanned plane of civil area and taking, mapping, the functions such as environment mapping.The unmanned aerial vehicle of the lift-launch photographing device that particularly mapping is used, present stage development rapidly, is widely used.It has the moderate feature of flight area coverage with low cost, but because the photographing device of its lift-launch of problem of power is easy camera or digital camera mostly.Quality after taking pictures and the flying power of taking pictures are all poor, are not suitable for the mapping of high definition on a large scale.And there is no good adaptive capacity for complicated weather condition yet.
Summary of the invention
Problem to be solved in the utility model is a kind of unmanned plane that carries photographing device, is particularly suitable for carrying the take pictures slr camera of ability of high-resolution and takes photo by plane.
For solving the problems of the technologies described above, the technical solution adopted in the utility model is:
A unmanned plane that carries photographing device, comprising:
Fuselage;
With the integrated wing of fuselage;
Vee tail;
Connect the tail pipe of fuselage and vee tail;
Be positioned at the engine installation that forebody divides;
The joint of described fuselage and wing is provided with level and smooth fillet;
Described tail pipe is the metal tube of a hollow, and its one end and tail cone are affixed, and the other end is connected with vee tail;
In described fuselage, be provided with photographing device loading device, the inner photographing device camera lens carrying of photographing device loading device can be taken ground by the through hole of establishing on body bottom surface.
Further, described photographing device loading device comprises:
Carrying equipment main body, its inside is the step trough with two ladders;
The first long-pending step trough of below small cross sections connects carrying equipment main body, and it places photographing device camera lens;
The second step trough of top larger sectional area is placed photographing device fuselage.
Further, described engine installation comprises engine petrol and screw propeller, and engine petrol drives screw propeller to rotate aircraft power is provided.
Further, described fuselage is carbon fibre material, and tail pipe is titanium alloy material.
Further, also comprise photographing device buffer unit; It is located in photographing device fuselage and carrying equipment main body between the second step trough end face.
Further, described photographing device buffer unit is rubber pad or foam-rubber cushion.
Advantage and the good effect that the utlity model has are: fuselage through customized design the weight by alleviating body for carrying heavier photographing device, the airframe structure design and the photographing device rock-steady structure that add improvement, make the shooting ground picture of high stability for a long time.
Accompanying drawing explanation
Fig. 1 is the front view of this utility model;
Fig. 2 is the birds-eye view of this utility model;
Fig. 3 is the photographing device loading device Local map of this utility model.
In figure:
1-fuselage; 2-wing; 3-engine installation; 4-tail pipe; 5-V type tail; 6-fuselage and wing upper bond place; 7-fuselage and wing lower bond place; 9-aileron; 10-elevating rudder and yaw rudder; 11-photographing device loading device; 1101-carrying equipment main body; 1102-photographing device camera lens; 1103-photographing device fuselage; 1105-photographing device buffer unit; 1106-photographing device secure component.
The specific embodiment
As illustrated in fig. 1 and 2, a kind of unmanned plane that carries photographing device, comprising:
Fuselage 1, is mainly used in arranging photographing device and some functional mapping equipments in fuselage 1.
With the integrated wing 2 of fuselage 1.Fuselage 1 in this embodiment by the moulding of mould time processing, does not adopt separable assembled form with wing 2.The advantage of this installation form is: in evil flight environment of vehicle slightly, and the not fragile fracture of connecting bridge, thus increase the service life.
The tail pipe 4 that connects fuselage 1 and vee tail 5, should be divided into front end fuselage 1 rear end tail pipe 4, the then combination of Joint by as a whole body by former.Can reduce to greatest extent the weight of unmanned plane entirety, the load-carrying ability of this part is used for carrying the accurate equipment of taking photo by plane of taking pictures.
Be positioned at the engine installation 3 of fuselage 1 leading portion, for the power of aircraft flight is provided.
Described fuselage 1 is provided with level and smooth fillet with the joint of wing 2, as the fuselage in figure and wing upper bond place 6 and fuselage and wing lower bond place 7.Air resistance when round and smooth surface can reduce to fly, improves the stability in aircraft flight.Less resistance can also improve the flying power of aircraft simultaneously, extends the flight time.
Described tail pipe 4 is the metal tube of a hollow, and its one end and fuselage 1 end are affixed, and the other end is connected with vee tail 5.
As shown in Figure 3, be provided with photographing device loading device 11 in fuselage 1, the inner photographing device camera lens 1102 carrying of photographing device loading device 11 can be taken ground by the through hole of establishing on fuselage 1 bottom surface.By pre-set shooting control software, can control automatically photographing device loading device 11 and take, take surface state and complete the operation of taking photo by plane.
Described photographing device loading device 11 comprises:
Carrying equipment main body 1101, is arranged on the bottom of fuselage 1, and in the present embodiment, it is arranged on the lower end of fuselage 1, and protrudes body bottom surface.Arranging of protruding can better be carried out non-blind area and take photo by plane.
Carrying equipment main body 1101, inside is the step trough with two ladders.
The first long-pending step trough of below small cross sections connects carrying equipment main body 1101, and it places photographing device camera lens 1102;
The second step trough of top larger sectional area is placed photographing device fuselage 1103.
Described engine installation 3 comprises engine petrol and screw propeller, and engine petrol drives screw propeller to rotate aircraft power is provided.
Described fuselage 1 is carbon fibre material, and tail pipe 4 is titanium alloy material.Can reduce overall aircraft weight and increase useful weight.
Also comprise photographing device buffer unit 1105; It is located in photographing device fuselage 1103 and carrying equipment main body 1101 between the second step trough end face.
Described photographing device buffer unit 1105 is rubber pad or foam-rubber cushion.And be also provided with as shown in Figure 3, the photographing device secure component 1106 of fixing photographing device fuselage 1103.Making to take photo by plane while taking pictures, photographing device fuselage 1103 is stable not to be rocked, and improves the quality of taking pictures.
In sum, this scheme adopts vee tail 5 forms, and the coursekeeping performance of aircraft promotes greatly.The mode that adopts wing body to merge, the glide ability of aircraft promotes greatly.Present the trend of downward drum from the bottom of front elevation fuselage, this designs for the head that adapts to similar 5DII digital camera etc.The design of this mode has fully demonstrated the theory that reduces aircraft weight, has saved the space that there is no need use, and the large radian rounding off at fuselage and wing place has fully demonstrated the feature that wing body merges.The part that fuselage the latter half is outstanding is smaller comparatively speaking, and radian and the smoothness of wing fusion part are relatively good, have so just increased lifting area.The rear half of fuselage 1 substitutes with tail pipe 4, alleviated aircraft overall weight, increased load carrying ability, while having increased the boat of aircraft, improved work efficiency.
Above embodiment of the present utility model is had been described in detail, but described content is only preferred embodiment of the present utility model, can not be considered to for limiting practical range of the present invention.All equalization variation and improvement etc. of doing according to the utility model scope, within all should still belonging to this patent covering scope.
Claims (6)
1. a unmanned plane that carries photographing device, comprising:
Fuselage (1);
With the integrated wing of fuselage (1) (2);
Vee tail (5);
Connect the tail pipe (4) of fuselage (1) and vee tail (5);
Be positioned at the engine installation (3) of fuselage (1) leading portion;
It is characterized in that:
Described fuselage (1) is provided with level and smooth fillet with the joint of wing (2);
Described tail pipe (4) is the metal tube of a hollow, and its one end and fuselage (1) end is affixed, and the other end is connected with described vee tail (5);
In described fuselage (1), be provided with photographing device loading device (11), the inner photographing device camera lens (1102) carrying of photographing device loading device (11) can be taken ground by the through hole of establishing on fuselage (1) bottom surface.
2. a kind of unmanned plane that carries photographing device according to claim 1, is characterized in that, described photographing device loading device (11) comprising:
Carrying equipment main body (1101), its inside arranges the step trough of two ladders;
The first long-pending step trough of below small cross sections connects carrying equipment main body (1101), and it places photographing device camera lens (1102);
The second step trough of top larger sectional area is placed photographing device fuselage (1103).
3. a kind of unmanned plane that carries photographing device according to claim 1, is characterized in that, described engine installation (3) comprises engine petrol and screw propeller, and engine petrol drives screw propeller to rotate aircraft power is provided.
4. a kind of unmanned plane that carries photographing device according to claim 1, is characterized in that: described fuselage (1) is carbon fibre material, and tail pipe (4) is titanium alloy material.
5. a kind of unmanned plane that carries photographing device according to claim 1, is characterized in that: also comprise photographing device buffer unit (1105); It is located in photographing device fuselage (1103) and carrying equipment main body (1101) between the second step trough end face.
6. a kind of unmanned plane that carries photographing device according to claim 5, is characterized in that: described photographing device buffer unit (1105) is rubber pad or foam-rubber cushion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320736151.4U CN203666990U (en) | 2013-11-20 | 2013-11-20 | Unmanned plane carrying photographing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320736151.4U CN203666990U (en) | 2013-11-20 | 2013-11-20 | Unmanned plane carrying photographing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203666990U true CN203666990U (en) | 2014-06-25 |
Family
ID=50963310
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320736151.4U Expired - Fee Related CN203666990U (en) | 2013-11-20 | 2013-11-20 | Unmanned plane carrying photographing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203666990U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104443417A (en) * | 2014-11-20 | 2015-03-25 | 广西大学 | Aerial photographing aircraft |
| CN105314085A (en) * | 2015-10-30 | 2016-02-10 | 湖北易瓦特科技股份有限公司 | Hand-throwing unmanned aerial vehicle |
-
2013
- 2013-11-20 CN CN201320736151.4U patent/CN203666990U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104443417A (en) * | 2014-11-20 | 2015-03-25 | 广西大学 | Aerial photographing aircraft |
| CN105314085A (en) * | 2015-10-30 | 2016-02-10 | 湖北易瓦特科技股份有限公司 | Hand-throwing unmanned aerial vehicle |
| CN105314085B (en) * | 2015-10-30 | 2018-11-20 | 易瓦特科技股份公司 | Hand throws unmanned plane |
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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: 20140625 Termination date: 20181120 |