CN203402041U - Unmanned aerial vehicle transportation guaranteeing system - Google Patents
Unmanned aerial vehicle transportation guaranteeing system Download PDFInfo
- Publication number
- CN203402041U CN203402041U CN201320485062.7U CN201320485062U CN203402041U CN 203402041 U CN203402041 U CN 203402041U CN 201320485062 U CN201320485062 U CN 201320485062U CN 203402041 U CN203402041 U CN 203402041U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- base plate
- guarantee system
- empty cabin
- described base
- 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 - Lifetime
Links
Images
Abstract
The utility model discloses an unmanned aerial vehicle transportation guaranteeing system. The unmanned aerial vehicle transportation guaranteeing system comprises a void compartment installed on a truck, wherein the void compartment comprises a bottom plate, guide rail devices are installed on the bottom plate and provided with guide grooves, fixing devices used for fixing sled plates of an unmanned aerial vehicle are installed along the guide grooves, and a supporting device used for fixing the tail of the unmanned aerial vehicle is further installed on the bottom plate. The unmanned aerial vehicle transportation guaranteeing system can reliably fix the unmanned aerial vehicle and associated equipment, thereby being beneficial to a good guarantee of the transportation of the unmanned aerial vehicle and the associated equipment.
Description
Technical field
The utility model relates to a kind of unmanned plane transportation guarantee system.
Background technology
China's electrical network existing ultra-high-tension power transmission line O&M pattern and routine inspection mode, by service personnel, rely on ground traffic tools or pad it, utilize hand-held instrument or the naked eyes facility of patrolling to process defect, not only labour intensity is large, service conditions is arduous, and efficiency is low, particularly mountain area and large cross line are patrolled and examined, and at ice damage, earthquake, floods, landslide, night condition line walking inspection, the length of taking time, cost is high, difficulty is large, can not meet disaster patrols and examines, important leverage power supply patrol and examine and electrical network emergency condition under emergent needs of patrolling and examining, development and the safe operation needs that can not adapt to modernization electrical network.
For adapting to new power circuit polling demand, the alternative scheme of the domestic and international various manual inspection of active development, helicopter routing inspection is one of feasible scheme.Helicopter routing inspection is divided into again the man-machine and large class of unmanned plane two, has man-machine patrolling and examining because cost is high, has limited field of application; Unmanned plane is patrolled and examined because aircraft cost is relatively cheap, and aeroplane performance and flight control technology are all greatly improved in recent years, become gradually study hotspot.
For reducing the unmanned plane waste in service life, reduce flight risk, a whole set of Unmanned Aircraft Systems (UAS) need to be transported to after formulating place and carry out again safety patrol inspection work.A whole set of Unmanned Aircraft Systems (UAS) has all proposed very high requirement at aspects such as protection, size, attendant equipments to storage and transportation conditions.Because large load unmanned plane electric power circuit safety patrol inspection work is in the starting stage at present, there is no can be for direct integrated unmanned plane transportation guarantee system.
Summary of the invention
Based on this, the utility model is to overcome the defect of prior art, and a kind of unmanned plane transportation guarantee system is provided, this transportation guarantee system can be reliably fixedly unmanned plane and relevant device, be conducive to ensure preferably the transportation to unmanned plane and relevant device.
Its technical scheme is as follows:
A kind of unmanned plane transportation guarantee system, comprise the empty cabin being arranged on truck, this sky cabin comprises base plate, on described base plate, track-type facilities is installed, this track-type facilities is provided with guide groove, along described guide groove, be provided with for the fixing anchor fitting of unmanned plane ski, on described base plate, be also provided with for the fixing bracing or strutting arrangement of unmanned plane afterbody.
Fixedly during unmanned plane, first mobile unmanned plane enters the inner space in described empty cabin, make unmanned plane ski move into the guide groove of described track-type facilities, then with anchor fitting, fix unmanned plane ski, then, with the fixing unmanned plane afterbody of bracing or strutting arrangement, can substantially realize fixing this unmanned plane, therefore, this unmanned plane transportation guarantee system can be reliably fixing unmanned plane, be conducive to ensure preferably the transportation to unmanned plane, prevent that collision from occurring.In addition, described empty cabin has good sealing property, can effectively completely cut off the impact of the rain that may run in transit, mist, dust etc.
Preferably, described empty cabin also comprises top board, header board, double door, the first side wall plate and the second sidewall paneling, and described top board, header board, double door, the first side wall plate and the second sidewall paneling surround described inner space.Wherein, this double door is located at the afterbody in described empty cabin, and double door adopts the railway carriage or compartment door of container-type.
Preferably, described track-type facilities and anchor fitting are installed in the front portion of described base plate, and described bracing or strutting arrangement is arranged on the rear portion of described base plate.Because unmanned plane is to move into this sky cabin from the rear in described empty cabin, such structure be arranged so that unmanned plane when moving into head towards the place ahead in described empty cabin, thereby can by described guide groove, to unmanned plane, position fixing better.
Preferably, described anchor fitting is returning buckle, and returning buckle comprises rotating junction, and returning buckle is hinged on described base plate by its rotating junction.Thereby, when unmanned plane ski being moved into after described guide-track groove, as long as pull returning buckle, returning buckle is buckled in described unmanned plane ski, can be rapidly fixing unmanned plane ski.
Preferably, described bracing or strutting arrangement is pillar stiffener, this pillar stiffener comprises cylinder and overturn cover, the bottom-hinged of described cylinder is on described base plate, the top of this cylinder is provided with the first groove, in overturn cover, be provided with the second groove, described overturn cover is hinged on the tip position of cylinder, makes the first groove and the second groove complement each other to form accommodating conduit.Thereby, fixing with anchor fitting after unmanned plane ski, described pillar stiffener is holded up, make the first groove be enclosed within the below of unmanned plane afterbody, cover overturn cover, can make accommodating conduit entangle described unmanned plane afterbody, thus can be well the fixing afterbody of unmanned plane.
Preferably, on described base plate, the first side wall plate and the second sidewall paneling, be respectively arranged with grab.Thereby, can connect grab and unmanned plane by drag-line, can be further fixing unmanned plane, to ensure better the transportation of unmanned plane.
Preferably, described empty cabin comprises hydraulic lifting tailgate, and this hydraulic lifting tailgate is arranged on the afterbody in described empty cabin.Thereby, when by unmanned plane and inside, the described empty cabin of relevant device immigration, first hydraulic lifting tailgate is reduced to subaerial height, and with less inclination angle kiss the earth, then open the double door of described empty cabin afterbody, by unmanned plane and relevant device from specifying the movement of landing place to hydraulic lifting tailgate, make again hydraulic lifting tailgate raise and with empty ceiling board with high, and be horizontal, now the relevant position from tailgate movement to inside, empty cabin by unmanned plane and relevant device, can move into described empty cabin by unmanned plane and relevant device; And in the time unmanned plane and relevant device will being shifted out to sky cabin, first hydraulic lifting tailgate is put down, make hydraulic lifting tailgate be horizontal positioned and be reduced to and the same height of described base plate, then open the double door of sky cabin afterbody, by unmanned plane and relevant device movement to hydraulic lifting tailgate, then again hydraulic lifting tailgate is reduced to subaerial height, and with less inclination angle kiss the earth, now can by unmanned plane and relevant device from tailgate movement to the place of taking off of appointment.Therefore, this hydraulic lifting tailgate can conveniently move into or shift out described inside, empty cabin by unmanned plane and relevant device.
Preferably, described empty cabin is connected with counterpoise grounding, and this counterpoise grounding is connected to the below of described base plate.Its objective is for fear of unmanned plane and the airborne sensor thereof of inside, empty cabin disturbed by extraneous intense electromagnetic, its principle is described empty cabin bulkhead, the header board, double door, top board, base plate, the first side wall plate and the second sidewall paneling that are empty cabin are all to be made by metallic material, therefore by counterpoise grounding ground connection, can play good electromagnetic shielding action.
Preferably, be provided with air intake fan and work hatch door on described the first side wall plate, this work hatch door is provided with observation window, on the second described sidewall paneling, is provided with exhaust fan.
Preferably, the top of described air intake fan, exhaust fan and work hatch door is separately installed with rain visor.Thereby, by rain visor is set, can further play rainproof effect.
Preferably, a rotor case and two wheel carriers are installed on described base plate, these two wheel carriers lay respectively at the both sides of described rotor case.Therefore, before unmanned plane being moved into inside, described empty cabin, can first the main rotor of unmanned plane be pulled down, and prevent from, in rotor case, can reduce taking up room of unmanned plane, and rotor accessing appropriate placement; Meanwhile, before unmanned plane being moved into inside, described empty cabin, should first from wheel carrier, pull down wheels, be installed on unmanned plane, so that mobile unmanned plane better.
The beneficial effects of the utility model are:
(1) described unmanned plane transportation guarantee system can, by fixedly unmanned plane and the relevant device reliably such as anchor fitting, bracing or strutting arrangement and rotor case, prevent impaction lesion, thereby be conducive to ensure preferably the transportation to unmanned plane and relevant device.
(2) described unmanned plane transportation guarantee system has good hermetically-sealed construction, and is provided with rain visor, can effectively completely cut off the impact of the rain that may run in transit, mist, dust etc.
(3) described unmanned plane transportation guarantee system connects counterpoise grounding by the base plate in empty cabin, can avoid unmanned plane sky cabin in and airborne sensor thereof to receive the impact of extraneous intense electromagnetic interference.
(4) described inner space, empty cabin is larger, can hold unmanned plane safety patrol inspection system patrol unmanned machine used and auxiliary unmanned plane.
Accompanying drawing explanation
Fig. 1 is the front view of the unmanned plane transportation guarantee system described in the utility model embodiment;
Fig. 2 is the back view of the unmanned plane transportation guarantee system described in the utility model embodiment;
Fig. 3 is unmanned plane transportation guarantee system described in the utility model embodiment structural representation in unmanned plane is fixed on sky cabin time;
Fig. 4 is the lateral plan of Fig. 3.
Fig. 5 is the inside birds-eye view in the empty cabin described in the utility model embodiment;
Fig. 6 is the structural representation of the pillar stiffener described in the utility model embodiment;
Fig. 7 is the schematic diagram of the dependency structure while being suspended on sky cabin afterbody of the hydraulic lifting plate described in the utility model embodiment;
Fig. 8 is hydraulic lifting tailgate described in the utility model embodiment in the dependency structure schematic diagram during with height and maintenance level with empty ceiling board;
Fig. 9 is hydraulic lifting tailgate described in the utility model embodiment in approaching floor level and the dependency structure schematic diagram when ground is low-angle and contacts.
Description of reference numerals:
10, empty cabin, 11, header board, 12, double door, 13, the first side wall plate, 14, the second sidewall paneling, 15, top board, 16, base plate, 20, track-type facilities, 30, returning buckle, 40, pillar stiffener, 41, cylinder, 411, the first groove, 42, overturn cover, 421, the second groove, 43, accommodating conduit, 50, hydraulic lifting tailgate, 60, air intake fan, 70, exhaust fan, 80, work hatch door, 81, observation window, 90, rain visor, 100, rotor case, 110, wheel carrier, 130, direct current emergency light, 140, explosion proof lamp switch, 150, cabinet, 160, the first built-in oil drum, 170, the second built-in oil drum, 180, external fuel tank, 190, hand-oil pump, 200, building instrument placing device, 210, drag-line, 220, tool box, 230, grab, 240, truck, 250, unmanned plane.
The specific embodiment
Below embodiment of the present utility model is elaborated:
As shown in Figures 1 to 9, a kind of unmanned plane transportation guarantee system, comprise the empty cabin 10 being arranged on truck 240, this sky cabin 10 comprises base plate 16, on described base plate 16, track-type facilities 20 is installed, this track-type facilities 20 is provided with guide groove, along described guide groove, is provided with for the fixing anchor fitting of unmanned plane ski, is also provided with for the fixing bracing or strutting arrangement of unmanned plane afterbody on described base plate 16.
Wherein, described empty cabin 10 also comprises top board 15, header board 11, double door 12, the first side wall plate 13 and the second sidewall paneling 14, and described top board 15, header board 11, double door 12, the first side wall plate 13 and the second sidewall paneling 14 surround described inner space.Described double door 12 is located at the afterbody in sky cabin 10, and double door 12 adopts the railway carriage or compartment door of container-type.Described anchor fitting is returning buckle 30, and returning buckle 30 comprises rotating junction, and returning buckle 30 is hinged on described base plate 16 by its rotating junction.Described bracing or strutting arrangement is pillar stiffener 40, this pillar stiffener 40 comprises cylinder 41 and overturn cover 42, the bottom-hinged of described cylinder 41 is on described base plate 16, the top of this cylinder 41 is provided with the first groove 411, in overturn cover 42, be provided with the second groove 421, described overturn cover 42 is hinged on the tip position of cylinder 41, makes the first groove 411 and the second groove 421 complement each other to form accommodating conduit 43.Described track-type facilities 20 and returning buckle 30 are installed in the front portion of described base plate 16, and described pillar stiffener 40 is arranged on the rear portion of described base plate 16.On described base plate 16, the first side wall plate 13 and the second sidewall paneling 14, be respectively arranged with grab 230.Grab 230 on base plate 16 is made as four, and these four grabs 230 are distributed in four corner location of described base plate 16.Grab 230 on the first side wall plate 13 is made as three, and arranges from front to back along this first side wall plate 13, consistent with on the first side wall plate 13 of the setting of the grab 230 on the second sidewall paneling 14.Described empty cabin 10 comprises hydraulic lifting tailgate 50, and this hydraulic lifting tailgate 50 is arranged on the afterbody in described empty cabin 10.On described the first side wall plate 13, be provided with air intake fan 60 and work hatch door 80, this work hatch door 80 is provided with observation window 81, on the second described sidewall paneling 14, is provided with exhaust fan 70.The top of described air intake fan 60, exhaust fan 70 and work hatch door 80 is separately installed with rain visor 90.A rotor case 100 and two wheel carriers 110 are installed on described base plate 16, and these two wheel carriers 110 lay respectively at the both sides of described rotor case 100.Described 10 belows, empty cabin are equiped with external fuel tank 180, and this external fuel tank 180 is arranged on the position, chassis of truck 240, and external fuel tank 180 is equipped with counterpoise grounding.The base plate 16 in described empty cabin 10 is by this counterpoise grounding ground connection.Below described empty cabin 10, being also equiped with 220，Gai tool box, a tool box 220 is arranged on truck 240 chassis.On described the first side wall plate 13, direct current emergency light 130 is also installed.The explosion proof lamp switch 140 that described 10 inside, empty cabin are also provided with explosion proof lamp and this explosion proof lamp is controlled, explosion proof lamp switch 140 is made as two, and one of them arranges near described work hatch door 80, and another arranges near described double door 12.Described empty cabin 10 anterior position are also provided with the built-in oil drum 170 of the built-in oil drum 160, second of cabinet 150, first, hand-oil pump 190 and building instrument placing device 200.
Using described header board outer wall or described truck 240 head towards direction as " the place ahead ".
The present embodiment has the following advantages or principle:
1, fixedly during unmanned plane 250, first after unmanned plane 250 dead halts, pull down main rotor, main rotor is positioned in rotor case 100 and is fixed, then from wheel carrier 110, pulling down wheels is installed on unmanned plane 250, follow the inner space that mobile unmanned plane 250 enters described empty cabin 10, make unmanned plane ski move into the guide groove of described track-type facilities 20, then pull the quick fixedly unmanned plane ski of returning buckle 30, then use fixedly unmanned plane 250 afterbodys of pillar stiffener 40, can substantially realize fixing this unmanned plane 250, finally from unmanned plane 250, wheels are disassembled and are fixed on wheel carrier 110 again.Therefore, this unmanned plane transportation guarantee system can be reliably fixing unmanned plane 250, be conducive to ensure preferably the transportation to unmanned plane 250, prevent that collision from occurring.Above-mentioned fixing means is applicable to transport unmanned plane 250 when good road conditions or short-distance transport.If under bad road conditions or when unmanned plane 250 is transported long-distance transport, also need to do by 210 pairs of unmanned planes of drag-line 250 further fixing, concrete grammar is: by pillar stiffener 40 fixedly after the afterbody of unmanned plane 250, unmanned plane 250 rotor supports are turned in the direction perpendicular with truck 240 working direction, then use drag-line 210 through the fixed orifice of rotor support both sides, and the two ends of drag-line 210 are connected on the grab 230 on the first side wall plate 13 or the second sidewall paneling 14, drag-line 210 is not strained, then recycle the grab 230 that other drag-line 210 connects on unmanned plane 250 alighting gear roots and described empty ceiling board, this drag-line 210 needs tension.Specifically as shown in Figure 3 and Figure 4.Therefore, by drag-line, connect unmanned plane 250 and grab 230, can be better fixing unmanned plane 250.
2, described empty cabin 10 has good sealing property, can effectively completely cut off the impact of the rain that may run in transit, mist, dust etc.
3, described track-type facilities 20 and returning buckle 30 are installed in the front portion of described base plate 16, and described pillar stiffener 40 is arranged on the rear portion of described base plate 16.Because unmanned plane 250 is to move into this sky cabin 10 from the rear in described empty cabin 10, such structure be arranged so that unmanned plane 250 when moving into head towards the place ahead in described empty cabin 10, thereby can by described guide groove, to unmanned plane 250, position fixing better.
4, the top of this cylinder 41 is provided with the first groove 411, is provided with the second groove 421 in overturn cover 42, and described overturn cover 42 is hinged on the tip position of cylinder 41, makes the first groove 411 and the second groove 421 complement each other to form accommodating conduit 43.Thereby, with anchor fitting, fixing after unmanned plane ski, described pillar stiffener 40 is holded up, make the first groove 411 be enclosed within the below of unmanned plane 250 afterbodys, cover overturn cover 42, can make accommodating conduit 43 entangle described unmanned plane 250 afterbodys, thus can be well the fixing afterbody of unmanned plane 250.In addition, because the bottom-hinged of cylinder 41 is on described base plate 16, therefore, when fixing unmanned aerial vehicle, this pillar stiffener 40 can be taken in lodging, is conducive to save take up room.
5, described empty cabin 10 comprises hydraulic lifting tailgate 50, and this hydraulic lifting tailgate 50 is arranged on the afterbody in described empty cabin 10.Thereby, when by unmanned plane 250 and 10 inside, the described empty cabin of relevant device immigration, first hydraulic lifting tailgate 50 is reduced to subaerial height, and with less inclination angle kiss the earth, then open the double door 12 of described empty cabin 10 afterbodys, by unmanned plane 250 and relevant device from specifying the movement of landing place to hydraulic lifting tailgate 50, make again hydraulic lifting tailgate 50 raise and with empty cabin 10 base plates 16 with high, and be horizontal, the relevant position from tailgate movement to 10 inside, empty cabin by unmanned plane 250 and relevant device now, unmanned plane 250 and relevant device can be moved into described empty cabin 10, and in the time unmanned plane 250 and relevant device will being shifted out to sky cabin 10, first hydraulic lifting tailgate 50 is put down, make hydraulic lifting tailgate 50 be horizontal positioned and be reduced to and the same height of described base plate 16, then open the double door 12 of sky cabin 10 afterbodys, by unmanned plane 250 and relevant device movement to hydraulic lifting tailgate 50, then again hydraulic lifting tailgate 50 is reduced to subaerial height, and with less inclination angle kiss the earth, now can by unmanned plane 250 and relevant device from tailgate movement to the place of taking off of appointment.Therefore, this hydraulic lifting tailgate 50 can conveniently move into or shift out described 10 inside, empty cabin by unmanned plane 250 and relevant device.Wherein, the lifting process of hydraulic lifting tailgate is as shown in Figs. 7-9.
6, described empty cabin 10 is connected with counterpoise grounding, and this counterpoise grounding is connected to the below of described base plate 16.Its objective is for fear of unmanned plane 250 and the airborne sensor thereof of 10 inside, empty cabin disturbed by extraneous intense electromagnetic, its principle is described empty cabin 10 bulkheads, the header board 11, double door 12, top board 15, base plate 16, the first side wall plate 13 and the second sidewall paneling 14 that are empty cabin 10 are all to be made by metallic material, therefore by counterpoise grounding ground connection, can play good electromagnetic shielding action.
7, the top of described air intake fan 60, exhaust fan 70 and work hatch door 80 is separately installed with rain visor 90.Thereby, by rain visor 90 is set, can further play rainproof effect.
8, a rotor case 100 and two wheel carriers 110 are installed on described base plate 16, these two wheel carriers 110 lay respectively at the both sides of described rotor case 100.Therefore,, before unmanned plane 250 is moved into 10 inside, described empty cabin, can first the main rotor of unmanned plane 250 be pulled down, and prevent from, in rotor case 100, can reduce taking up room of unmanned plane 250, and rotor accessing appropriate placement; Meanwhile, before unmanned plane 250 is moved into 10 inside, described empty cabin, should first from wheel carrier 110, pull down wheels, be installed on unmanned plane 250, so that mobile unmanned plane 250 better.
9, described empty cabin 10 internal needles are provided with special set-point, cabinet 150 or placing device to all kinds of attendant equipments, can effectively avoid contingent various damaged in collision events in transportation.
10, described 10 inside, empty cabin have been equipped with all kinds of unmanned plane 250 annexes, Work tool and fuel oil, can effectively guarantee completing smoothly of unmanned plane 250 patrol tasks.
11, described 10 inner spaces, empty cabin are larger, can hold unmanned plane 250 safety patrol inspection systems patrol unmanned machine 250 used and auxiliary unmanned plane 250.
12, the first described built-in oil drum 160 and the second built-in oil drum 170 load respectively different fuel oils, to meet the fuel oil needs of patrol unmanned machine and auxiliary unmanned plane.
The above embodiment has only expressed the specific embodiment of the present utility model, and it describes comparatively concrete and detailed, but can not therefore be interpreted as the restriction to the utility model the scope of the claims.It should be pointed out that for the person of ordinary skill of the art, without departing from the concept of the premise utility, can also make some distortion and improvement, these all belong to protection domain of the present utility model.
Claims (10)
1. a unmanned plane transportation guarantee system, it is characterized in that, comprise the empty cabin being arranged on truck, this sky cabin comprises base plate, on described base plate, track-type facilities is installed, this track-type facilities is provided with guide groove, along described guide groove, is provided with for the fixing anchor fitting of unmanned plane ski, is also provided with for the fixing bracing or strutting arrangement of unmanned plane afterbody on described base plate.
2. unmanned plane transportation guarantee system according to claim 1, is characterized in that, described track-type facilities and anchor fitting are installed in the front portion of described base plate, and described bracing or strutting arrangement is arranged on the rear portion of described base plate.
3. unmanned plane transportation guarantee system according to claim 1 and 2, is characterized in that, described anchor fitting is returning buckle, and returning buckle comprises rotating junction, and returning buckle is hinged on described base plate by its rotating junction.
4. unmanned plane transportation guarantee system according to claim 1 and 2, it is characterized in that, described bracing or strutting arrangement is pillar stiffener, this pillar stiffener comprises cylinder and overturn cover, the bottom-hinged of described cylinder is on described base plate, and the top of this cylinder is provided with the first groove, is provided with the second groove in overturn cover, described overturn cover is hinged on the tip position of cylinder, makes the first groove and the second groove complement each other to form accommodating conduit.
5. unmanned plane transportation guarantee system according to claim 1, is characterized in that, described empty cabin comprises the first side wall plate and the second sidewall paneling, on described base plate, the first side wall plate and the second sidewall paneling, is respectively arranged with grab.
6. unmanned plane transportation guarantee system according to claim 1, is characterized in that, described empty cabin comprises hydraulic lifting tailgate, and this hydraulic lifting tailgate is arranged on the afterbody in described empty cabin.
7. unmanned plane transportation guarantee system according to claim 1, is characterized in that, described empty cabin is connected with counterpoise grounding, and this counterpoise grounding is connected to the below of described base plate.
8. unmanned plane transportation guarantee system according to claim 1, it is characterized in that, described empty cabin comprises the first side wall plate and the second sidewall paneling, on described the first side wall plate, be provided with air intake fan and work hatch door, this work hatch door is provided with observation window, on the second described sidewall paneling, is provided with exhaust fan.
9. unmanned plane transportation guarantee system according to claim 8, is characterized in that, the top of described air intake fan, exhaust fan and work hatch door is separately installed with rain visor.
10. unmanned plane transportation guarantee system according to claim 1, is characterized in that, a rotor case and two wheel carriers are installed on described base plate, and these two wheel carriers lay respectively at the both sides of described rotor case.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320485062.7U CN203402041U (en) | 2013-08-08 | 2013-08-08 | Unmanned aerial vehicle transportation guaranteeing system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320485062.7U CN203402041U (en) | 2013-08-08 | 2013-08-08 | Unmanned aerial vehicle transportation guaranteeing system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203402041U true CN203402041U (en) | 2014-01-22 |
Family
ID=49937981
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320485062.7U Expired - Lifetime CN203402041U (en) | 2013-08-08 | 2013-08-08 | Unmanned aerial vehicle transportation guaranteeing system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203402041U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103914076A (en) * | 2014-03-28 | 2014-07-09 | 浙江吉利控股集团有限公司 | Cargo transferring system and method based on unmanned aerial vehicle |
| CN106080349A (en) * | 2016-07-06 | 2016-11-09 | 陈慧愿 | A kind of express delivery dispensing vehicle being configured with unmanned plane cargo handling platform |
| CN109244943A (en) * | 2018-11-08 | 2019-01-18 | 广东电网有限责任公司 | A kind of hanging wire unmanned plane and its control method and device |
-
2013
- 2013-08-08 CN CN201320485062.7U patent/CN203402041U/en not_active Expired - Lifetime
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103914076A (en) * | 2014-03-28 | 2014-07-09 | 浙江吉利控股集团有限公司 | Cargo transferring system and method based on unmanned aerial vehicle |
| CN103914076B (en) * | 2014-03-28 | 2017-02-15 | 浙江吉利控股集团有限公司 | Cargo transferring system and method based on unmanned aerial vehicle |
| US9817405B2 (en) | 2014-03-28 | 2017-11-14 | Zhejiang Geely Holding Group Co., Ltd. | Cargo transport system and method based on unmanned aerial vehicle |
| CN106080349A (en) * | 2016-07-06 | 2016-11-09 | 陈慧愿 | A kind of express delivery dispensing vehicle being configured with unmanned plane cargo handling platform |
| CN109244943A (en) * | 2018-11-08 | 2019-01-18 | 广东电网有限责任公司 | A kind of hanging wire unmanned plane and its control method and device |
| CN109244943B (en) * | 2018-11-08 | 2020-02-07 | 广东电网有限责任公司 | Line-hanging unmanned aerial vehicle and control method and device thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203402041U (en) | Unmanned aerial vehicle transportation guaranteeing system | |
| CN204895882U (en) | Multi -functional flying platform based on unmanned aerial vehicle | |
| CN211442770U (en) | Automatic unmanned aerial vehicle of puting in goods | |
| CN110058224A (en) | Tunnel-liner detection method based on robot automatic tracing technology and radar detection technique | |
| CN105035340A (en) | Multifunctional flying platform based on unmanned aerial vehicle | |
| CN103935382A (en) | City train and operating method thereof | |
| CN202896375U (en) | Unmanned plane integral ground station system | |
| CN104972854A (en) | Hovercar | |
| CN102530233A (en) | Front part of an aircraft fuselage incorporating a bay for stowing landing gear | |
| CN209351619U (en) | A kind of unmanned plane draw off gear based on sliding rail | |
| CN211711018U (en) | Novel shipborne unmanned equipment rapid carrying, retracting and releasing device | |
| CN210653684U (en) | Unmanned aerial vehicle receive and releases system | |
| CN201808502U (en) | Emergency rescue drainage vehicle | |
| CN205256478U (en) | On -vehicle air park | |
| CN203473249U (en) | Ground station system for unmanned helicopter safety routing inspection | |
| CN106274506A (en) | A kind of urban air public transportation system | |
| CN216186132U (en) | Unmanned aerial vehicle machine nest and multi-functional lamp pole | |
| CN203581386U (en) | Rotating mechanism for mounting and maintaining aero-engine | |
| CN212083660U (en) | Side slope earth surface micro-deformation multipurpose mobile radar monitoring vehicle | |
| CN207536125U (en) | A kind of parafoil umbrella rope protective device for umbrella wing unmanned plane | |
| CN205545264U (en) | Emergent satellite communication cabin | |
| CN205256124U (en) | Multi -functional logging truck | |
| CN106427735A (en) | Automobile with self-organized local area network cluster detection function | |
| CN110884677A (en) | A winding and unwinding devices for mooring unmanned aerial vehicle | |
| CN203681702U (en) | Helicopter tow truck with take-off and landing and guarantee functions |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140122 |
|
| CX01 | Expiry of patent term |