CN206520749U - One kind is taken photo by plane unmanned plane - Google Patents
One kind is taken photo by plane unmanned plane Download PDFInfo
- Publication number
- CN206520749U CN206520749U CN201720130571.6U CN201720130571U CN206520749U CN 206520749 U CN206520749 U CN 206520749U CN 201720130571 U CN201720130571 U CN 201720130571U CN 206520749 U CN206520749 U CN 206520749U
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- Prior art keywords
- plane
- shell
- motor
- unmanned plane
- gear
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Abstract
Taken photo by plane unmanned plane, including shell, support arm, support frame, impeller, damping device and camera the utility model discloses one kind, the two ends of described shell are provided with support arm, one end of described support arm is provided with motor I, described motor I driving impeller rotations；The inside of described shell is provided with housing, and the motor shaft that described lower housing portion is provided with motor II, described motor II is located at enclosure interior, and described motor shaft is provided with gear II, and described gear II both sides are engaged with gear I；Described gear I and sleeve connection, described sleeve are connected with suspension rod, and the bottom of described suspension rod is provided with damping device, and the bottom of described damping device is provided with camera；The bottom of described shell is provided with two symmetrical support frames.The utility model can under different wind conditions smooth flight and camera not by shaking and impulsive force is influenceed.
Description
Technical field
The utility model is related to unmanned plane field, more particularly to one kind is taken photo by plane unmanned plane.
Background technology
Unmanned plane of taking photo by plane be by radio robot or airborne computer stored program controlled manipulated it is not manned fly
Row device.With the development and the raising of living standards of the people of science and technology, unmanned plane of taking photo by plane is because its own motion is flexible, shoot resolution ratio
High, the low feature of cost is more widely applied.But unmanned plane of the prior art of taking photo by plane still have easily by wind speed, the rainy day because
Element influence, camera such as are easily shaken at the phenomenon.
Utility model content
The purpose of this utility model is intended to improve the weak point that prior art is present and taken photo by plane unmanned plane, energy there is provided one kind
Enough smooth flights under different wind conditions and camera be not by shaking and impulsive force is influenceed.
To achieve the above object, the utility model uses following technical proposals：
One kind is taken photo by plane unmanned plane, including shell, support arm, support frame, impeller, damping device and camera, and described is outer
The two ends of shell are provided with support arm, and one end of described support arm drives impeller rotation provided with motor I, described motor I；Described
The other end of support arm is connected with screw rod, and described screw rod is engaged with gear III, and described gear III is connected by gear shaft
Motor；The inside of described shell is provided with housing, and described housing is connected by the inwall of connecting plate and shell；Described housing
The motor shaft that bottom is provided with motor II, described motor II is located at enclosure interior, and described motor shaft is provided with gear II, institute
Engaged with gear I the gear II stated both sides；Described gear I and sleeve connection, described sleeve are connected with suspension rod, described
The bottom of suspension rod is provided with damping device, and the bottom of described damping device is provided with camera；The bottom of described shell is provided with two
Individual symmetrical support frame.
Further, described screw rod is located at the inside of shell, and the inside of described support arm is hollow structure, described
To be threadedly coupled between screw rod and support arm, rotated by motor-driven gear III, drive screw rod to rotate, so as to pass through screw rod
The length adjustment for screwing in support arm stretches out the support arm lengths of housing exterior.
Further, described motor I is connected with rotary shaft, and described rotary shaft is provided with impeller.
Further, the outside of described impeller is provided with impeller bracket, and the upper surface of described impeller bracket covers one layer
Waterproof paper, impeller bracket prevents that impeller is influenceed by barrier in flight course, and waterproof paper can avoid rainwater to nothing of taking photo by plane
The influence of man-machine flight.
Further, the inside of described sleeve is hollow structure, and described sleeve inner is provided with internal thread, and described hangs
Bar is provided with external screw thread, is rotated by motor II drive gears II, and sleeve is turned by gear II and gear I engagement
It is dynamic, so that suspension rod realizes elongating or shortening in sleeve length.
Further, described damping device includes upper plate, lower plate and spring, and bullet is passed through between described upper plate and lower plate
Spring is connected, and damping device can avoid in flight course the camera shooting effect caused that shakes not good.
Further, described shell includes shell upper and outer casing underpart, described shell upper and outer casing underpart shape
Into spheroid structure.
Further, the bottom of described outer casing underpart is provided with circular hole, and camera can stretch out from circular hole.
Further, described enclosure is additionally provided with control module and power supply, and described camera is respectively with controlling mould
Block and power electric connection.
Further, described housing bottom is provided with two through holes, and described sleeve passes through through hole；Described housing is circle
Cylinder or rectangular parallelepiped structure.
The beneficial effects of the utility model：
(1) distance stretched into by screw rod in support arm adjusts the length that support arm is located at housing exterior, to realize not
With can smooth flight under wind conditions；
(2) suspension rod and sleeve composition telescoping mechanism, make that enclosure can be retracted to without using camera, are preventing shooting
Head is chronically at outside and causes damage；
(3) spring vibration damper can reduce influence of the vibration to shooting quality of camera.
Brief description of the drawings
Fig. 1 is overall structure diagram of the present utility model；
Fig. 2 is internal structure schematic diagram of the present utility model；
Fig. 3 is top view of the present utility model；
Wherein, 1- shells, 2- support arms, 3- impellers, 4- motors I, 5- support frame, 6- suspension rods, 7- damping devices, 8- shootings
Head, 9- gears I, 10- sleeve, 11- gears II, 12- motor shaft, 13- housings, 14- motors II, 15- connecting plate, 16- screw rods,
17- gears III, 18- gear shaft, 19- waterproof papers, 20- impeller brackets, 21- housings.
Embodiment
The utility model is described in detail below in conjunction with the accompanying drawings：
As shown in Figure 1-Figure 3, one kind is taken photo by plane unmanned plane, including shell 1, support arm 2, support frame 5, impeller 3, damping device
7 and camera 8, the two ends of described shell 1 are provided with support arm 2, and one end of described support arm 2 is described provided with motor I4
Motor I4 driving impellers 3 rotate；The other end of described support arm 2 is connected with screw rod 16, described screw rod 16 and gear III17
Engagement, described gear III17 connects motor by gear shaft 18；The inside of described shell 1 is provided with housing 13, described shell
Body 13 is connected by connecting plate 15 with the inwall of shell 1；The described bottom of housing 13 is provided with motor II14, described motor
II14 motor shaft 12 is inside the housing 13, and described motor shaft 12 is provided with gear II11, and the two of described gear II11
Engaged with gear I9 side；Described gear I9 is connected with sleeve 10, and described sleeve 10 is connected with suspension rod 6, described suspension rod 6
Bottom is provided with damping device 7, and the bottom of described damping device 7 is provided with camera 8；The bottom of described shell 1 is provided with two
Symmetrical support frame 5.
Further, described screw rod 16 is located at the inside of shell 1, and the inside of described support arm 2 is hollow structure, institute
To be threadedly coupled between the screw rod 16 stated and support arm 2, rotated by motor-driven gear III17, drive screw rod 16 to rotate, from
And the length of support arm 2 that the length adjustment for screwing in support arm 2 by screw rod 16 is stretched out outside shell 1.
Further, described motor I4 is connected with rotary shaft, and described rotary shaft is provided with impeller 3.
Further, the outside of described impeller 3 is provided with impeller bracket 20, and the upper surface of described impeller bracket 20 is covered
One layer of waterproof paper 19, impeller bracket 20 prevents that impeller 3 is influenceed by barrier in flight course, and waterproof paper 19 can avoid rain
Influence of the water to unmanned plane during flying of taking photo by plane.
Further, the inside of described sleeve 10 is hollow structure, and the described inside of sleeve 10 is provided with internal thread, described
Suspension rod 6 be provided with external screw thread, rotated by motor II14 drive gears II11, work engaged by gear II11 and gear I9
With rotating sleeve 10, so that suspension rod 6 realizes elongating or shortening in sleeve 10 length.
Further, described damping device 7 includes upper plate, lower plate and spring, passes through between described upper plate and lower plate
Spring is connected, and damping device 7 can avoid in flight course the camera shooting effect caused that shakes not good.
Further, described shell 1 includes shell upper and outer casing underpart, described shell upper and outer casing underpart shape
Into spheroid structure.
Further, the bottom of described outer casing underpart is provided with circular hole, and camera 8 can stretch out from circular hole.
Further, be additionally provided with control module and power supply inside described shell 1, described camera 8 respectively with control
Module and power electric connection.
Further, the described bottom of housing 13 is provided with two through holes, and described sleeve 10 passes through through hole；Described housing
13 be cylinder or rectangular parallelepiped structure.
Operation principle of the present utility model is：
Before use, testing the length scope of application of support arm 2 according to different wind conditions；When in use, by starting
Motor II14 makes camera 8 stretch out shell 1, and the length of support arm 2 is adjusted according to wind regime, starts unmanned plane by remote control, enters
Row shooting operation；When not in use, camera 8 is packed up, is easy to the placement and carrying of unmanned plane.
It is not new to this practicality although above-mentioned embodiment of the present utility model is described with reference to accompanying drawing
The limitation of type protection domain, one of ordinary skill in the art should be understood that on the basis of the technical solution of the utility model, ability
Field technique personnel need not pay the various modifications that creative work can make or deform still in protection model of the present utility model
Within enclosing.
Claims (10)
- The unmanned plane 1. one kind is taken photo by plane, it is characterised in that including shell, support arm, support frame, impeller, damping device and camera, The two ends of described shell are provided with support arm, and one end of described support arm drives impeller rotation provided with motor I, described motor I Turn；The other end of described support arm is connected with screw rod, and described screw rod is engaged with gear III, and described gear III passes through tooth Wheel shaft connects motor；The inside of described shell is provided with housing, and described housing is connected by the inwall of connecting plate and shell；Institute The lower housing portion stated is provided with motor II, and described motor II motor shaft is located at enclosure interior, and described motor shaft is provided with Gear II, described gear II both sides are engaged with gear I；Described gear I and sleeve connection, described sleeve connect with suspension rod Connect, the bottom of described suspension rod is provided with damping device, and the bottom of described damping device is provided with camera；The bottom of described shell Portion is provided with two symmetrical support frames.
- The unmanned plane 2. one kind as claimed in claim 1 is taken photo by plane, it is characterised in that described screw rod is located at the inside of shell, institute The inside for the support arm stated is hollow structure, is to be threadedly coupled between described screw rod and support arm.
- The unmanned plane 3. one kind as claimed in claim 1 is taken photo by plane, it is characterised in that described motor I is connected with rotary shaft, described Rotary shaft be provided with impeller.
- The unmanned plane 4. one kind as claimed in claim 3 is taken photo by plane, it is characterised in that the outside of described impeller is provided with impeller branch Frame, the upper surface of described impeller bracket covers one layer of waterproof paper.
- The unmanned plane 5. one kind as claimed in claim 1 is taken photo by plane, it is characterised in that the inside of described sleeve is hollow structure, Described sleeve inner is provided with internal thread, and described suspension rod is provided with external screw thread.
- The unmanned plane 6. one kind as claimed in claim 1 is taken photo by plane, it is characterised in that described damping device includes upper plate, lower plate And spring, connected between described upper plate and lower plate by spring.
- The unmanned plane 7. one kind as claimed in claim 1 is taken photo by plane, it is characterised in that described shell includes shell upper and shell Bottom, described shell upper and outer casing underpart formation spheroid structure.
- The unmanned plane 8. one kind as claimed in claim 7 is taken photo by plane, it is characterised in that the bottom of described outer casing underpart is provided with circle Hole.
- The unmanned plane 9. one kind as claimed in claim 1 is taken photo by plane, it is characterised in that described enclosure is additionally provided with control module And power supply, described camera respectively with control module and power electric connection.
- The unmanned plane 10. one kind as claimed in claim 1 is taken photo by plane, it is characterised in that described housing bottom is provided with two through holes, Described housing is cylinder or rectangular parallelepiped structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720130571.6U CN206520749U (en) | 2017-02-13 | 2017-02-13 | One kind is taken photo by plane unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720130571.6U CN206520749U (en) | 2017-02-13 | 2017-02-13 | One kind is taken photo by plane unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206520749U true CN206520749U (en) | 2017-09-26 |
Family
ID=59891692
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720130571.6U Expired - Fee Related CN206520749U (en) | 2017-02-13 | 2017-02-13 | One kind is taken photo by plane unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206520749U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108216605A (en) * | 2018-01-23 | 2018-06-29 | 徐嘉辉 | A kind of power transmission line unmanned machine distance-measuring device |
| CN108248877A (en) * | 2018-01-17 | 2018-07-06 | 西安九天无限智能科技有限公司 | A kind of aerial survey unmanned plane task device protective device |
| CN108528744A (en) * | 2018-06-13 | 2018-09-14 | 安徽新祥信息技术有限公司 | One kind is taken photo by plane camera damping |
-
2017
- 2017-02-13 CN CN201720130571.6U patent/CN206520749U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108248877A (en) * | 2018-01-17 | 2018-07-06 | 西安九天无限智能科技有限公司 | A kind of aerial survey unmanned plane task device protective device |
| CN108216605A (en) * | 2018-01-23 | 2018-06-29 | 徐嘉辉 | A kind of power transmission line unmanned machine distance-measuring device |
| CN108528744A (en) * | 2018-06-13 | 2018-09-14 | 安徽新祥信息技术有限公司 | One kind is taken photo by plane camera damping |
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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: 20170926 Termination date: 20180213 |