CN204527625U - Multifunctional individual unmanned plane - Google Patents
Multifunctional individual unmanned plane Download PDFInfo
- Publication number
- CN204527625U CN204527625U CN201520106607.8U CN201520106607U CN204527625U CN 204527625 U CN204527625 U CN 204527625U CN 201520106607 U CN201520106607 U CN 201520106607U CN 204527625 U CN204527625 U CN 204527625U
- Authority
- CN
- China
- Prior art keywords
- plate
- unmanned plane
- individual unmanned
- multifunctional individual
- upper plate
- 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
Links
Abstract
The utility model discloses a kind of Multifunctional individual unmanned plane, the foot rest comprising body, rotor driver and be arranged on below described body, described rotor driver is multiple and is connected to body surrounding, described body comprises the upper plate, intermediate plate and the lower plate that from top to bottom set gradually, the left side board for connecting upper plate and lower plate and right side board is provided with between described upper plate and lower plate, described intermediate plate is fixed on left side board and right side board, be provided with interstage sleeve between described upper plate and intermediate plate, between described intermediate plate and interstage sleeve, be provided with shock absorption device.The utility model aim to provide a kind of stabilized structure, lightweight, collapsible, shake little, that flying power is strong Multifunctional individual unmanned plane.
Description
Technical field
The utility model relates to unmanned plane field, particularly a kind of stabilized structure, lightweight, collapsible, shake little Multifunctional individual unmanned plane.
Background technology
Unmanned plane has very important effect in mapping, can airborne sensory equipment, as high resolution CCD digital camera, light optical camera, infrared scanner, the obtaining information such as laser scanner, magnetic determining device, with computing machine, graphicinformation is processed, and be made into image according to certain accuracy requirement.For adapting to the total demand of town development, provide comprehensive geographic, resource information.Correctly, complete information material is the basis of science decision.Each department, all departments are in unified plan, Agrocybe praecox, land management monitoring, construction of water conservancy works, infrastructure construction, factories and miness construction, residential quarter construction, environmental protection and ecological construction etc., invariably need up-to-date, most complete terrain and its features data, become government agencies at all levels and newly-built development zone problem anxious to be resolved.Kunming strength hawk unmanned plane specializes in the design of aerial survey unmanned plane equipment, producing and selling and the aerial survey service of taking photo by plane, be that the top aerial survey of Chinese technology is taken photo by plane unmanned aerial vehicle design manufacture and Hang Fei service provider, the integrated information of regional newfound historic site, newly-built street, bridge, airport, station and soil, resource utilization can be reflected with unmanned plane surveying and mapping technology exactly.
Unmanned plane surveying and mapping technology can be widely used in national ecological environmental protection, mineral resources exploration, marine environmental monitoring, land use survey, water resources development, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, city planning and municipal administration, forest disease and pest and protect and the field such as monitoring, public safety, Defence business, digital earth and advertisement photography, has the wide market demand.
But often there is flying power difference, mapping instability after existing UAV flight's GPS device, vibrate the problems such as large.
Utility model content
The purpose of this utility model be to provide a kind of stabilized structure, lightweight, collapsible, shake little, that flying power is strong Multifunctional individual unmanned plane.
The technical scheme that the utility model provides is: a kind of Multifunctional individual unmanned plane, comprise body, rotor driver and the foot rest be arranged on below described body, described rotor driver is multiple and is connected to body surrounding, described body comprises the upper plate from top to bottom set gradually, intermediate plate and lower plate, the left side board for connecting upper plate and lower plate and right side board is provided with between described upper plate and lower plate, described intermediate plate is fixed on left side board and right side board, be provided with between described upper plate and intermediate plate and be fixedly connected with interstage sleeve with upper plate, shock absorption device is provided with between described intermediate plate and interstage sleeve.
In above-mentioned Multifunctional individual unmanned plane, described shock absorption device comprises the lower vibration damper plate that the upper vibration damper plate that is connected with intermediate plate is connected with interstage sleeve and the multiple shock-absorbing balls be arranged between upper vibration damper plate and lower vibration damper plate.
In above-mentioned Multifunctional individual unmanned plane, described shock absorption device is two, is separately positioned on the two ends of intermediate plate, and the quantity of described shock-absorbing ball is 4.
In above-mentioned Multifunctional individual unmanned plane, between described intermediate plate and lower plate, being also provided with steering wheel, being also provided with many between described upper plate and lower plate for connecting the pillar stiffener of upper plate and lower plate.
In above-mentioned Multifunctional individual unmanned plane, described foot rest is 4, point to be located on four angles below body.
In above-mentioned Multifunctional individual unmanned plane, described foot rest comprises foot rest body and is arranged on many reinforced ribs around foot rest body, and the center of described foot rest body is provided with a container cavity, is provided with damping spring in described container cavity.
In above-mentioned Multifunctional individual unmanned plane, also comprise battery case, described battery case is arranged between intermediate plate and lower plate.
In above-mentioned Multifunctional individual unmanned plane, described rotor driver is connected with body by a pipe link, and one end that described pipe link is connected with body is provided with the articulation piece for being connected with body.
In above-mentioned Multifunctional individual unmanned plane, the top of described upper plate is connected with lid, and described lid comprises protecgulum and bonnet, and described bonnet is provided with the GPS support for fixing GPS device.
In above-mentioned Multifunctional individual unmanned plane, described GPS support comprises stirrup and rack body, described rack body comprises near-end and far-end, the far-end of described rack body is provided with the base for fixing GPS, one end of described stirrup is hinged on bonnet, the other end of described stirrup is hinged on described rack body, and one end of described bonnet is provided with the hold down groove for coordinating with the near-end of described rack body when described rack body is upright.
The main purpose of scheme of the present utility model be to provide stabilized structure, lightweight, collapsible, shake little Multifunctional individual unmanned plane, specifically, absorb the vibrations that rotor driver produces reduce impact on GPS by being provided with shock absorption device between intermediate plate and interstage sleeve.
Meanwhile, foot rest is arranged the steadiness that reinforced rib improves foot rest, the impact of vibrations on GPS device when damping spring can reduce landing is set in foot rest inside.
Red at the utility model, rotor driver connects body by the pipe link with articulation piece can realize the collapsible of pipe link, makes this Multifunctional individual unmanned plane more small and exquisite.
In order to improve the stability of the GPS device of this Multifunctional individual unmanned plane further, the GPS support adopting folding three-legged structure namely to comprise stirrup and rack body improves the stability of GPS when unmanned plane runs, can fold again when not using, make it volume further small and exquisite, more easily carry.
Accompanying drawing explanation
Fig. 1 is the structural representation of embodiment 1 of the present utility model;
Fig. 2 is the explosive decomposition figure of embodiment 1 of the present utility model;
Fig. 3 is the structural representation of the foot rest of embodiment 1 of the present utility model;
Fig. 4 is the front view of the shock absorption device of embodiment 1 of the present utility model;
Fig. 5 is the lateral plan of the shock absorption device of embodiment 1 of the present utility model;
Fig. 6 is the structural representation that the GPS support of embodiment 1 of the present utility model is accepted.
Detailed description of the invention
Below in conjunction with detailed description of the invention, the technical solution of the utility model is described in further detail, but does not form any restriction of the present utility model.
Embodiment 1
As shown in Figures 1 to 6, a kind of Multifunctional individual unmanned plane, comprise body 1, rotor driver 2 and the foot rest 3 be arranged on below described body 1, described rotor driver 2 is multiple and is connected to body 1 surrounding, in the present embodiment, rotor driver 2 is 4, certainly 6 or 8 can be also chosen as in actual applications, described body 1 comprises the upper plate 11 from top to bottom set gradually, intermediate plate 12 and lower plate 13, the left side board 14 for connecting upper plate 11 and lower plate 13 and right side board 15 is provided with between described upper plate 11 and lower plate 13, described intermediate plate 12 is fixed between left side board 14 and right side board 15, interstage sleeve 16 is provided with between described upper plate 11 and intermediate plate 12, shock absorption device 4 is provided with between described intermediate plate 12 and interstage sleeve 16, described interstage sleeve 16 is fixedly connected with upper plate 11, as illustrated in figures 4-5, described shock absorption device 4 comprises the upper vibration damper plate 41 be connected with intermediate plate 12, the lower vibration damper plate 42 be connected with interstage sleeve 16 and the multiple shock-absorbing balls 43 be arranged between upper vibration damper plate 41 and lower vibration damper plate 42, described shock absorption device 4 is two, be separately positioned on the two ends of intermediate plate 12, the quantity of described shock-absorbing ball 43 is preferably 4.Preferably, upper plate 11, intermediate plate 12, lower plate 13, left side board 14 and right side board 15 are all engraved structure, keep the fastness of body 1 while can effectively reducing body 1 weight like this.In order to improve its stability further, between described upper plate 11 and lower plate 12, be also provided with many pillar stiffeners 17.
In the present embodiment, steering wheel 5 is also provided with between described intermediate plate 12 and lower plate 13, it act as and controls unmanned plane during flying direction, described foot rest 3 is 4, point to be located on four angles below body 1, as shown in Figure 3, described foot rest 3 comprises foot rest body 31 and is arranged on the many reinforced ribs 32 around foot rest body 31, the center of described foot rest body 31 is provided with a container cavity 33, damping spring 34 is provided with in described container cavity 33, when unmanned plane lands, damping spring 34 effectively can absorb vibrations during landing.This Multifunctional individual unmanned plane also comprises battery case 6, described battery case 6 is arranged between intermediate plate 12 and lower plate 13, well known, this Multifunctional individual unmanned plane is also provided with a controller, in order to realize the control of GPS device, the Power supply and control to rotor driver 2, described rotor driver 2 is connected with body 1 by a pipe link 7, one end that described pipe link 7 is connected with body 1 is provided with the articulation piece for being connected with body 1, attached not shown, achieve the collapsible of pipe link 7 by articulation piece.
As further improvement of this embodiment, the top of described upper plate 11 is connected with lid 8, and described lid 8 comprises protecgulum 81 and bonnet 82, and described bonnet 82 is provided with the GPS support 9 for fixing GPS device; As shown in figures 1 to 6, Fig. 1 is the schematic diagram of GPS support 9 when opening, and Fig. 6 is the structural representation of GPS support 9 when packing up; Described GPS support 9 comprises stirrup 91 and rack body 92, described rack body 92 comprises near-end and far-end, the far-end of described rack body 92 is provided with the base 93 for fixing GPS, one end of described stirrup 91 is hinged on bonnet 82, the other end of described stirrup 91 is hinged on described rack body 92, and one end of described bonnet 82 is provided with the hold down groove 83 for coordinating with the near-end of described rack body 92 when described rack body 92 is upright.Described stirrup 91 is hinged on 1/2 ~ 1/6 place of rack body 92 near far-end, described bonnet 82 is provided with one for receiving described stirrup 91 and the holding tank 84 of rack body 92, described holding tank 84 length is consistent with stirrup 91 length, and described hold down groove 83 is arranged in holding tank 84.
In actual applications, when using this Multifunctional individual unmanned plane, open pipe link 7, switch on power, send takeoff order to controller, this Multifunctional individual unmanned plane starts flight, in flight course, carries out absorbing vibration and damping by shock absorption device 4.After flight terminates, impulsive force when absorbing landing by foot rest body 31 and damping spring 34 during landing, is then set to the state of contraction by pipe link 7.This Multifunctional individual unmanned plane compact structure, be easy to fold, lightweight, vibrate little, mapping accurately, be applicable to the mapping under various weather conditions and photography.
Above-describedly be only preferred embodiment of the present utility model, all do in spirit of the present utility model and spirit any amendment, equivalently to replace and improvement etc., all should be included within protection domain of the present utility model.
Claims (10)
1. a Multifunctional individual unmanned plane, comprise body (1), rotor driver (2) and the foot rest (3) be arranged on below described body (1), described rotor driver (2) is for multiple and be connected to body (1) surrounding, it is characterized in that: described body (1) comprises the upper plate (11) from top to bottom set gradually, intermediate plate (12) and lower plate (13), the left side board (14) for connecting upper plate (11) and lower plate (13) and right side board (15) is provided with between described upper plate (11) and lower plate (13), described intermediate plate (12) is fixed on left side board (14) and right side board (15), the interstage sleeve (16) be fixedly connected with upper plate (11) is provided with between described upper plate (11) and intermediate plate (12), shock absorption device (4) is provided with between described intermediate plate (12) and interstage sleeve (16).
2. Multifunctional individual unmanned plane according to claim 1, is characterized in that: multiple shock-absorbing balls (43) that described shock absorption device (4) comprises the upper vibration damper plate (41) be connected with intermediate plate (12), the lower vibration damper plate (42) be connected with interstage sleeve (16) and is arranged between upper vibration damper plate (41) and lower vibration damper plate (42).
3. Multifunctional individual unmanned plane according to claim 2, is characterized in that: described shock absorption device (4) is two, is separately positioned on the two ends of intermediate plate (12), and the quantity of described shock-absorbing ball (43) is 4.
4. Multifunctional individual unmanned plane according to claim 1, it is characterized in that: between described intermediate plate (12) and lower plate (13), be also provided with steering wheel (5), between described upper plate (11) and lower plate (13), being also provided with the many pillar stiffeners (17) for connecting upper plate (11) and lower plate (13).
5. Multifunctional individual unmanned plane according to claim 1, is characterized in that: described foot rest (3) is 4, point to be located on four angles of body (1) below.
6. Multifunctional individual unmanned plane according to claim 5, it is characterized in that: described foot rest (3) comprises foot rest body (31) and is arranged on foot rest body (31) many reinforced ribs (32) around, the center of described foot rest body (31) is provided with a container cavity (33), is provided with damping spring (34) in described container cavity (33).
7. Multifunctional individual unmanned plane according to claim 1, is characterized in that: also comprise battery case (6), and described battery case (6) is arranged between intermediate plate (12) and lower plate (13).
8. Multifunctional individual unmanned plane according to claim 1, it is characterized in that: described rotor driver (2) is connected with body (1) by a pipe link (7), one end that described pipe link (7) is connected with body (1) is provided with the articulation piece for being connected with body (1).
9. according to the arbitrary described Multifunctional individual unmanned plane of claim 1 to 8, it is characterized in that: the top of described upper plate (11) is connected with lid (8), described lid (8) comprises protecgulum (81) and bonnet (82), and described bonnet (82) is provided with the GPS support (9) for fixing GPS device.
10. Multifunctional individual unmanned plane according to claim 9, it is characterized in that: described GPS support (9) comprises stirrup (91) and rack body (92), described rack body (92) comprises near-end and far-end, the far-end of described rack body (92) is provided with the base (93) for fixing GPS, one end of described stirrup (91) is hinged on bonnet (82), the other end of described stirrup (91) is hinged on described rack body (92), one end of described bonnet (82) is provided with the hold down groove (83) for coordinating with the near-end of described rack body (92) when described rack body (92) is upright.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520106607.8U CN204527625U (en) | 2015-02-13 | 2015-02-13 | Multifunctional individual unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520106607.8U CN204527625U (en) | 2015-02-13 | 2015-02-13 | Multifunctional individual unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204527625U true CN204527625U (en) | 2015-08-05 |
Family
ID=53741653
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520106607.8U Expired - Fee Related CN204527625U (en) | 2015-02-13 | 2015-02-13 | Multifunctional individual unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204527625U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105035300A (en) * | 2015-08-27 | 2015-11-11 | 深圳市恩孚电子科技有限公司 | Vibration preventing system of unmanned aerial vehicle |
| CN105691625A (en) * | 2016-04-08 | 2016-06-22 | 吉林大学 | Vibration attenuation mechanism for unmanned aerial vehicle |
| CN105691589A (en) * | 2016-04-08 | 2016-06-22 | 北京博瑞爱飞科技发展有限公司 | Unmanned aerial vehicle |
| CN107108009A (en) * | 2016-09-05 | 2017-08-29 | 深圳市大疆创新科技有限公司 | Unmanned vehicle and its frame, frame assembling external member |
| CN108116671A (en) * | 2018-01-02 | 2018-06-05 | 海鹰航空通用装备有限责任公司 | A kind of multi-rotor unmanned aerial vehicle |
| US10017237B2 (en) | 2015-12-29 | 2018-07-10 | Qualcomm Incorporated | Unmanned aerial vehicle structures and methods |
| CN108313306A (en) * | 2018-03-23 | 2018-07-24 | 中科灵动航空科技成都有限公司 | A kind of rotor wing unmanned aerial vehicle platform |
| CN108341064A (en) * | 2018-03-23 | 2018-07-31 | 中科灵动航空科技成都有限公司 | A kind of rotor wing unmanned aerial vehicle |
-
2015
- 2015-02-13 CN CN201520106607.8U patent/CN204527625U/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105035300A (en) * | 2015-08-27 | 2015-11-11 | 深圳市恩孚电子科技有限公司 | Vibration preventing system of unmanned aerial vehicle |
| CN105035300B (en) * | 2015-08-27 | 2017-09-19 | 深圳市恩孚电子科技有限公司 | Unmanned plane suspension system |
| US10017237B2 (en) | 2015-12-29 | 2018-07-10 | Qualcomm Incorporated | Unmanned aerial vehicle structures and methods |
| CN105691625A (en) * | 2016-04-08 | 2016-06-22 | 吉林大学 | Vibration attenuation mechanism for unmanned aerial vehicle |
| CN105691589A (en) * | 2016-04-08 | 2016-06-22 | 北京博瑞爱飞科技发展有限公司 | Unmanned aerial vehicle |
| CN107108009A (en) * | 2016-09-05 | 2017-08-29 | 深圳市大疆创新科技有限公司 | Unmanned vehicle and its frame, frame assembling external member |
| CN108116671A (en) * | 2018-01-02 | 2018-06-05 | 海鹰航空通用装备有限责任公司 | A kind of multi-rotor unmanned aerial vehicle |
| CN108116671B (en) * | 2018-01-02 | 2021-02-05 | 海鹰航空通用装备有限责任公司 | Multi-rotor unmanned aerial vehicle |
| CN108313306A (en) * | 2018-03-23 | 2018-07-24 | 中科灵动航空科技成都有限公司 | A kind of rotor wing unmanned aerial vehicle platform |
| CN108341064A (en) * | 2018-03-23 | 2018-07-31 | 中科灵动航空科技成都有限公司 | A kind of rotor wing unmanned aerial vehicle |
| CN108313306B (en) * | 2018-03-23 | 2024-04-05 | 中科灵动航空科技成都有限公司 | Rotor unmanned aerial vehicle platform |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204527625U (en) | Multifunctional individual unmanned plane | |
| CN204527660U (en) | Many rotor wing unmanned aerial vehicles | |
| CN210000575U (en) | multifunctional mapping platform based on unmanned aerial vehicle remote sensing | |
| CN209956211U (en) | Balance-adjustable unmanned aerial vehicle undercarriage | |
| CN210441869U (en) | Remote sensing type multifunctional surveying instrument | |
| CN203294310U (en) | Retractable undercarriage of unmanned aerial vehicle | |
| CN105956081A (en) | Ground station map updating method and apparatus | |
| CN204575069U (en) | The airborne three-dimensional laser measurement mechanism of a kind of SUAV (small unmanned aerial vehicle) | |
| CN105914844A (en) | Multi-dimensional shock-absorbing unmanned aerial vehicle charging station | |
| CN208110040U (en) | A kind of aerial device with airborne laser radar | |
| CN205396570U (en) | Aerial survey unmanned aerial vehicle's camera installation device | |
| CN209988111U (en) | Plant protection unmanned aerial vehicle shock attenuation foot rest | |
| CN205440852U (en) | A unmanned aerial vehicle descending base for command car | |
| CN105857585B (en) | A kind of unmanned plane undercarriage suitable for mountain area flight | |
| CN212617133U (en) | Open-air portable topography mapping device | |
| CN206800230U (en) | It is a kind of can the unmanned plane of self-level(l)ing rise and fall platform | |
| CN210310880U (en) | Unmanned aerial vehicle topography survey device | |
| CN205030047U (en) | A shield cover for on multiaxis aircraft | |
| CN208344532U (en) | A kind of parachuting type unmanned plane recyclable device | |
| CN208070006U (en) | A kind of balancing pole of aerial photography aircraft | |
| CN206939106U (en) | A kind of Portable unmanned machine protects landing platform | |
| CN105909926A (en) | Vibration reducing device for unmanned aerial vehicle charging base station based on Stewart parallel mechanism | |
| CN211618071U (en) | Unmanned aerial vehicle that satisfies airworthiness requirement stabilizer blade structure that rises and falls | |
| Aber et al. | A comparison of the strengths and weaknesses of small-format aerial photography platforms | |
| CN110395408A (en) | A kind of interface structure of grid type load-carrying construction |
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: 20150805 Termination date: 20180213 |