CN107757864A - One kind is taken photo by plane unmanned plane - Google Patents
One kind is taken photo by plane unmanned plane Download PDFInfo
- Publication number
- CN107757864A CN107757864A CN201710973556.2A CN201710973556A CN107757864A CN 107757864 A CN107757864 A CN 107757864A CN 201710973556 A CN201710973556 A CN 201710973556A CN 107757864 A CN107757864 A CN 107757864A
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- China
- Prior art keywords
- gear
- bar
- connecting rod
- motor
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
Abstract
Taken photo by plane unmanned plane the invention discloses one kind, including fuselage, and two wing installations for being respectively arranged on fuselage both sides, the wing installation includes the rail brackets for being fixed on fuselage side, the rail brackets is provided with guide rail, slider guide is slidably fitted with the guide rail, mounting bracket is connected with the outside of the slider guide, the mounting bracket is provided with a groove, be placed with the groove can confronting grooves slide rack, rack setting parallel with guide rail, the mounting bracket also rotates axis connection first gear by first, the mounting bracket also rotates axis connection second gear by second, the first gear and second gear are respectively positioned on the inside of rack and engaged with rack.The wing installation of the present invention can be folded in rail brackets when not in use, not only save the space of occupancy, and wing-body can be protected not damaged；The landing gear of the present invention can be folded in the nacelle of fuselage in flight, and flight resistance is reduced with this.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, particularly relate to one kind and take photo by plane unmanned plane.
Background technology
The fixed-wing length of run of the unmanned plane of prior art is oversize, and space-consuming is huge, it has not been convenient to deposit, and due to machine
Wing structure is frivolous, easily impaired；Other landing gear lacks folding storage mechanism, and resistance is added in flight；Furthermore nothing
Watering device function on man-machine is simple, it is difficult to meet demand.
The content of the invention
The technical problems to be solved by the invention are to provide one kind and taken photo by plane unmanned plane, to solve unmanned plane in the prior art
Fixed-wing length of run is oversize, and is easily lost in storage, and landing gear lacks fold mechanism, and watering dress
It is simple to put function, it is difficult to the technical problem of meet demand.
Taken photo by plane unmanned plane, including fuselage, and two points in order to solve the above technical problems, embodiments of the invention provide one kind
Not She Yu fuselage both sides wing installation, the wing installation includes being fixed on the rail brackets of fuselage side, the guide rail branch
Frame is provided with guide rail, and slider guide is slidably fitted with the guide rail, mounting bracket, the mounting bracket are connected with the outside of the slider guide
Be provided with a groove, be placed with the groove can confronting grooves slide rack, rack setting parallel with guide rail, institute
To state mounting bracket and also rotate axis connection first gear by first, the mounting bracket also rotates axis connection second gear by second,
The first gear and second gear are respectively positioned on the inside of rack and engaged with rack, and the outer end of first rotary shaft is hung down at it
Nogata has connected up guide rod, and the side of the rail brackets is provided with slipping groove stent, is provided with the slipping groove stent and is grown along guide rail
The straight runner for spending direction setting and the oblique chute for the front end for being communicated in straight runner, the outer end of the guide rod is provided with pulley, institute
State pulley to be installed in straight runner, second rotary shaft is connected with wing fixed plate in vertical direction, and the wing is fixed
Plate is provided with wing-body, and the slider guide middle part is provided with screw rod along rail length direction, and described screw rod one end is connected with screw rod
Motor, the screw motor drive screw turns are so as to driving slider guide to be slided along guide rail；
The underbelly is provided with landing gear, and the landing gear includes the nacelle below fuselage and set
Installing plate in the nacelle both sides, the installing plate are provided with the straight sliding groove of a vertical direction, are located on the installing plate
The medium position of the straight sliding groove is extended with an arc groove, the center of circle of the arc groove and the bottom of straight sliding groove to side
Coincide, slided on the straight sliding groove and be provided with upper slide-bar and lower slide-bar, pass through connecting plate between the upper slide-bar and lower slide-bar
It is connected, the half that the spacing between the upper slide-bar and lower slide-bar is equal to straight sliding groove is grown, the one end connection of the connecting plate
There is setter plate, the setter plate and straight sliding groove are perpendicular, and the setter plate is provided with wheel shaft, and the wheel shaft both ends are provided with and landed
Wheel, is rotatedly connected, the universal driving shaft is coaxially disposed with upper slide-bar, the installation between the connecting plate of both sides by universal driving shaft
Plate side is provided with and risen and fallen motor, and the output shaft of the motor that rises and falls is connected to one end of first connecting rod, the first connecting rod it is another
One end is rotationally connected with one end of second connecting rod, and the other end of the second connecting rod is rotationally connected with the universal driving shaft, described
Wheel shaft and universal driving shaft are parallel；
The body upper is provided with watering device, and the watering device includes lifting platform, water tank and fountain head, the lifting
Platform includes the cup dolly and lifter plate located at body upper, and the outer ring of the cup dolly is provided with endless glide, the annular
Be slidably connected an annulus on slide rail, and the annulus upper surface is provided with gear ring, and cup dolly upper surface circle shows 4 axles
Mounting seat, each axle mounting seat are provided with installation axle, and one end of each installation axle is provided with the gear ring gear with gear ring, often
The other end of the individual installation axle is provided with third connecting rod, and the other end of each third connecting rod is rotatablely connected a fourth link,
The third connecting rod and fourth link are isometric, and each fourth link is connected on same lifter plate by connecting shaft, institute
State cup dolly central part and be used for accommodating third connecting rod, fourth link and the lifting of up and down motion rotated provided with storage tank
Plate, wherein the outer face of a gear ring gear, which is provided with motor input shaft, is used to connect power input motor for driving a wherein tooth
Enclose gear rotation；The lifter plate is provided with the water tank, and the water tank is provided with the fountain head；
Camera device is additionally provided with below the fuselage, the camera device includes the first U-shaped support, and described first is U-shaped
First motor is installed, first motor connects the first semi-circle gear, the first U-shaped branch by the first little gear in support
Cross is rotatably connected at the two side outer end of frame, the other both ends of the cross are connected to the two of the second U-shaped support
At side wall outer end, the second motor is installed in the second U-shaped support, second motor connects second by the second little gear
Semi-circle gear, first semi-circle gear and the second semi-circle gear are respectively arranged in the both sides of cross, and both axis mutually hang down
Directly；Motion cameras is also equipped with the second U-shaped support.
Wherein, the distance between upper slide-bar and lower slide-bar are set to L, the length of the first connecting rod and second connecting rod is big
In L and less than 2 times of L, when upper slide-bar be located at the top of straight sliding groove, the output shaft of the upper slide-bar and the motor that rises and falls it
Between vertical range be L, and the tie point of the first connecting rod and second connecting rod is located at the top of upper slide-bar.
The above-mentioned technical proposal of the present invention has the beneficial effect that：
In such scheme, wing installation of the invention can be folded in rail brackets when not in use, not only saved and accounted for
Space, and wing-body can be protected not damaged；The landing gear of the present invention can be folded in fuselage in flight
In nacelle, flight resistance is reduced with this；The watering device of the present invention is installed on lifter plate, and lifter plate in the vertical direction is past
Multiple motion, can increase spray area, have practicality.
Brief description of the drawings
Fig. 1 is the structural representation one of the present invention, shows state during wing folding.
Fig. 2 is the structural representation two of the present invention, shows state during wing expansion.
Fig. 3 is the stereogram of the wing installation of the present invention.
Fig. 4 is the explosive view of the wing installation of the present invention.
Fig. 5 is the partial perspective view one of the wing installation of the present invention.
Fig. 6 is the partial perspective view two of the wing installation of the present invention.
Fig. 7 is the structure chart after the wing-body turning unfolding of the wing installation of the present invention.
Fig. 8 is the explosive view of the landing gear of the present invention.
Fig. 9 is the folding state figure of the landing gear of the present invention.
Figure 10 is the state diagram for being expanded to half of the landing gear of the present invention.
Figure 11 is the state diagram being fully deployed of the landing gear of the present invention.
Figure 12 is the side view of the watering device of the present invention.
Figure 13 is the top view of the watering device of the present invention.
Figure 14 is the stereogram of the watering device of the present invention.
Figure 15 is the structure chart of the camera device of the present invention.
Embodiment
To make the technical problem to be solved in the present invention, technical scheme and advantage clearer, below in conjunction with accompanying drawing and tool
Body embodiment is described in detail.
For convenience of description, before fuselage head direction is, direction of advance, front portion, front end, afterbody for after, rear portion, after
End, it is inner side close to fuselage side, is outside away from fuselage side.
As shown in Figures 1 to 7, the embodiment of the present invention provides one kind and taken photo by plane unmanned plane, including fuselage 1, and two set respectively
Wing installation 10 in the both sides of fuselage 1, the bottom of fuselage 1 are provided with landing gear 30, unmanned plane can use jet engine or
Turbo oar engine promotes, rail brackets 11 of the wing installation 10 including being fixed on the side of fuselage 1, on the rail brackets 11
Provided with guide rail 12, length direction of the guide rail 12 along fuselage 1 is installed, and slider guide 13, institute are slidably fitted with the guide rail 12
State the outside of slider guide 13 and be connected with mounting bracket 14, the mounting bracket 14 is provided with a groove 141, is placed with the groove 141
Can the rack 15 that slides of confronting grooves, the rack 15 and 12 parallel setting of guide rail, rack 15 is by the both sides margin of groove 141
Position, rack 15 can only move along the length direction of groove 141, and the mounting bracket 14 also connects first gear by the first rotary shaft 16
17, the mounting bracket 14 also connects second gear 19 by the second rotary shaft 18, and the first gear 17 and second gear 19 are equal
Engage positioned at the inner side of rack 15 and with rack 15, the outer end of first rotary shaft 16 is connected with guide rod in the perpendicular direction
20, the side of the rail brackets 11 is provided with slipping groove stent 21, is provided with the slipping groove stent 21 and is set along the length direction of guide rail 12
The straight runner 22 put and be communicated in straight runner 22 front end oblique chute 23, the oblique chute 23 is along the front end of straight runner 22
Direction is continued forward and extended laterally, and the outer end of the guide rod 20 is provided with pulley 24, and the pulley 24 is installed on straight runner
In 22, the rotary shaft 18 of the first rotary shaft 16 and second is each perpendicular to the length direction of guide rail 12, and it is front and rear separately set, institute
State the second rotary shaft 18 and be connected with wing fixed plate 25 in vertical direction, during initial position, i.e., pulley 24 is located at straight runner 22
Interior, wing fixed plate 25 is parallel with fuselage 1, and the wing fixed plate 25 is provided with wing-body 26, in the slider guide 13
Portion is provided with screw rod 27 along the length direction of guide rail 12, and described one end of screw rod 27 is connected with screw motor 28, and the screw motor 28 is driven
Dynamic screw rod 27 is rotated so as to drive slider guide 13 to be slided along guide rail 12.For wing in receiving state, slider guide is located at guide rail most
Rear end, screw motor start, and drive screw rod rotation, screw rod drives slider guide to be moved forwards along guide rail, due to first gear
Be engaged on rack, the first rotary shaft had not only connected first gear but also connection guide, when pulley is in straight runner, first rotate
Axle also can only do the translation of fore-and-aft direction, therefore first gear can not rotate, and can only be translated forward together with slipping groove stent,
Rack can not confronting grooves movement, therefore first gear, second gear, rack with slipping groove stent keep geo-stationary, when
During pulley motion to oblique chute, guide rod turns an angle, and so as to drive first gear to rotate, first gear band carry-over bar is backward
Motion, rack drives second gear rotate, and second gear drives wing fixed plate to rotate, and is moved so as to complete the turning unfolding of wing
Make.When needing folding, it is only necessary to slider guide is moved to guide rail rearmost end.
As shown in Figs. 8 to 11, the landing gear 30 is included located at the nacelle 31 of the lower section of fuselage 1 and located at described
The installing plate 32 of the both sides of nacelle 31, the installing plate 32 is provided with the straight sliding groove 33 of a vertical direction, on the installing plate 32
Medium position positioned at the straight sliding groove 33 is extended with an arc groove 34 to side, and the center of circle of the arc groove 34 is slided with straight
The bottom of groove 33 coincides, and is slided on the straight sliding groove 33 and is provided with upper slide-bar 35 and lower slide-bar 36, the upper He of slide-bar 35
It is connected between lower slide-bar 36 by connecting plate 37, the spacing between the upper slide-bar 35 and lower slide-bar 36 is equal to straight sliding groove 33
Half is grown, and the one end of the connecting plate 37 is connected with setter plate 38, and the setter plate 38 and straight sliding groove 33 are perpendicular, described
Setter plate 38 is provided with wheel shaft 39, and the both ends of wheel shaft 39 are provided with landing wheel 40, pass through connection between the connecting plate 37 of both sides
Moving axis 41 is rotatedly connected, and the universal driving shaft 41 is coaxially disposed with upper slide-bar 35, and the side of installing plate 32 is provided with the motor 42 that rises and falls,
The output shaft 421 of the motor 42 that rises and falls is connected to one end of first connecting rod 43, and the other end of the first connecting rod 43, which rotates, to be connected
One end of second connecting rod 44 is connected to, the other end of the second connecting rod 44 is rotationally connected with the universal driving shaft 41, the wheel shaft
39 and universal driving shaft 41 it is parallel；The distance between upper slide-bar 35 and lower slide-bar 36 are set to L, the first connecting rod 43 and second connects
The length of bar 44 is the L more than L and less than 2 times, when upper slide-bar 35 is located at the top of straight sliding groove 33, the upper slide-bar 35
Vertical range between the output shaft 421 for the motor 42 that rises and falls is L, and the tie point of the first connecting rod 43 and second connecting rod 44
434 are located at the top of upper slide-bar 35.When upper slide-bar is located at the top of straight sliding groove, landing wheel is in receiving state, setter plate
Parallel to ground, when unmanned plane needs to land, startup is risen and fallen motor, and output shaft drives first connecting rod to rotate, then by the
Two connecting rods drive universal driving shaft motion, because the upper slide-bar on connecting plate and downslide axle position are in straight sliding groove, second connecting rod output
Power to universal driving shaft passes to upper slide-bar, and because upper slide-bar is limited in straight sliding groove, upper slide-bar can only be along straight sliding groove
Move straight down, therefore universal driving shaft is to move straight down；When upper slide-bar is moved in the middle part of straight sliding groove, now lower slider
Axle has moved to straight slip trench bottom, because the length of first connecting rod and second connecting rod is the L more than L and less than 2 times, therefore
The angle α that first connecting rod and second connecting rod are formed be less than 90 °, therefore second connecting rod export to universal driving shaft power have make linkage
The axially component of straight sliding groove horizontal motion, therefore universal driving shaft can drive slide-bar to be moved along arc groove, therefore can realize
The upset of setter plate, setter plate is had angle with ground shape or parallel, complete the expansion action of landing wheel；When needing folding
When, overturn the motor that rises and falls.
As shown in Figure 1, Figure 2, shown in Figure 12 to Figure 14, the top of fuselage 1 is provided with watering device 2, and the watering device 2 includes
Lifting platform, water tank 78 and fountain head 77, the lifting platform include the cup dolly 81 and lifter plate 82 of body upper, the circle
The outer ring of base 81 is provided with endless glide (not shown), and be slidably connected an annulus 83 in the endless glide, on the annulus 83
Surface is provided with gear ring 831, and the upper surface circle of cup dolly 81 shows 4 axle mounting seats 84, each axle mounting seat
84 are provided with installation axle 85, and one end of each installation axle 85 is provided with the gear ring gear 86 with gear ring 83, each installation axle
85 other end is provided with third connecting rod 87, and the other end of each third connecting rod 87 is rotatablely connected a fourth link 88, described
Third connecting rod 87 and fourth link 88 are isometric, and each fourth link 88 is connected to same lifter plate 82 by connecting shaft 89
On, the central part of cup dolly 81 be provided with storage tank 811 be used for the accommodating third connecting rod 87 rotated, fourth link 88 and
The lifter plate 82 of lower motion, it is used to connect power input electricity wherein the outer face of a gear ring gear 86 is provided with motor input shaft 79
Machine is (not shown) to be used to drive a wherein gear ring gear 86 to rotate.Motor driven gear ring pinion rotation is inputted, then gear ring gear
It is meshed with gear ring and then drives annulus to rotate, therefore other 3 gear ring gears also rotates simultaneously, so as to drive 4 simultaneously the
Three connecting rods and fourth link motion, because third connecting rod and fourth link are isometric, and the third connecting rod and fourth link just
Beginning movement angle is identical, is each other the circumference array relation at the 90 ° of angles in interval, therefore lifter plate in the vertical direction can be driven past
Multiple motion；The lifter plate 82 is provided with the water tank 78, and the water tank 78 is provided with the fountain head 77.Because parabola is former
Reason, there is far and near difference the current pick-up point of the different ejection of high and low position, therefore can increase watering area.
As shown in figure 15, the lower section of the fuselage 1 is provided with camera device, and the camera device is included located at the lower section of fuselage 1
The first U-shaped support 403, the first motor 404 is installed in the first U-shaped support 403, first motor 404 passes through
One little gear 405 connects the first semi-circle gear 406, and ten are rotatably connected at the two side outer end of the first U-shaped support 403
Cabinet frame 407, the other both ends of the cross 407 are connected at the two side outer end of the second U-shaped support 408, and described second is U-shaped
Second motor 409 is installed, second motor 409 connects the second semi-circle gear by the second little gear 500 in support 408
501, the semi-circle gear 501 of the first semi-circle gear 406 and second is respectively arranged in the both sides of cross 407, and both axis
It is perpendicular；Motion cameras 502 is also equipped with the second U-shaped support 408.
Described above is the preferred embodiment of the present invention, it is noted that for those skilled in the art
For, on the premise of principle of the present invention is not departed from, some improvements and modifications can also be made, these improvements and modifications
It should be regarded as protection scope of the present invention.
Claims (2)
- The unmanned plane 1. one kind is taken photo by plane, including fuselage, and two wing installations for being respectively arranged on fuselage both sides, it is characterised in that institute The rail brackets that wing installation includes being fixed on fuselage side is stated, the rail brackets is provided with guide rail, slided on the guide rail Slider guide is installed, mounting bracket is connected with the outside of the slider guide, the mounting bracket is provided with a groove, placed in the groove Have can confronting grooves slide rack, rack setting parallel with guide rail, the mounting bracket also pass through the first rotary shaft company First gear is connect, the mounting bracket also rotates axis connection second gear, the equal position of first gear and second gear by second Engaged on the inside of rack and with rack, the outer end of first rotary shaft is connected with guide rod in the perpendicular direction, described to lead The side of rail support is provided with slipping groove stent, and the straight runner set along rail length direction and connection are provided with the slipping groove stent Oblique chute in the front end of straight runner, the outer end of the guide rod are provided with pulley, and the pulley is installed in straight runner, and described Two rotary shafts are connected with wing fixed plate in vertical direction, and the wing fixed plate is provided with wing-body, the slider guide Middle part is provided with screw rod along rail length direction, and described screw rod one end is connected with screw motor, and the screw motor drive screw turns Move so as to drive slider guide to be slided along guide rail；The underbelly is provided with landing gear, and the landing gear includes the nacelle being located at below fuselage and located at institute The installing plate of nacelle both sides is stated, the installing plate is provided with the straight sliding groove of a vertical direction, is located on the installing plate described The medium position of straight sliding groove is extended with an arc groove to side, and the center of circle of the arc groove is mutually overlapping with the bottom of straight sliding groove Close, slided on the straight sliding groove and be provided with upper slide-bar and lower slide-bar, be connected between the upper slide-bar and lower slide-bar by connecting plate, The half that spacing between the upper slide-bar and lower slide-bar is equal to straight sliding groove is grown, and the one end of the connecting plate is connected with placement Plate, the setter plate and straight sliding groove are perpendicular, and the setter plate is provided with wheel shaft, and the wheel shaft both ends are provided with landing wheel, position It is rotatedly connected between the connecting plate of both sides by universal driving shaft, the universal driving shaft is coaxially disposed with upper slide-bar, the installing plate one Side is provided with the motor that rises and falls, and the output shaft of the motor that rises and falls is connected to one end of first connecting rod, the other end of the first connecting rod One end of second connecting rod is rotationally connected with, the other end of the second connecting rod is rotationally connected with the universal driving shaft, the wheel shaft It is parallel with universal driving shaft；The body upper is provided with watering device, and the watering device includes lifting platform, water tank and fountain head, the lifting platform bag The cup dolly and lifter plate located at body upper are included, the outer ring of the cup dolly is provided with endless glide, the endless glide On be slidably connected an annulus, the annulus upper surface is provided with gear ring, and cup dolly upper surface circle shows 4 axles installations Seat, each axle mounting seat are provided with installation axle, and one end of each installation axle is provided with the gear ring gear with gear ring, Mei Gesuo The other end for stating installation axle is provided with third connecting rod, and the other end of each third connecting rod is rotatablely connected a fourth link, described Third connecting rod and fourth link are isometric, and each fourth link is connected on same lifter plate by connecting shaft, the circle Shape base center portion is provided with storage tank and is used for accommodating third connecting rod, fourth link and the lifter plate of up and down motion rotated, its In a gear ring gear outer face be provided with motor input shaft be used for connect a power input motor be used for drive a wherein gear ring tooth Wheel rotation；The lifter plate is provided with the water tank, and the water tank is provided with the fountain head；Camera device is additionally provided with below the fuselage, the camera device includes the first U-shaped support, the first U-shaped support First motor is inside installed, first motor connects the first semi-circle gear by the first little gear, the first U-shaped support Cross is rotatably connected at the outer end of two side, the other both ends of the cross are connected to the two side of the second U-shaped support At outer end, the second motor is installed in the second U-shaped support, second motor connects the second semicircle by the second little gear Gear, first semi-circle gear and the second semi-circle gear are respectively arranged in the both sides of cross, and both axis perpendiculars；Institute State and be also equipped with motion cameras on the second U-shaped support.
- 2. landing gear according to claim 1, it is characterised in that be set to the distance between upper slide-bar and lower slide-bar L, the length of the first connecting rod and second connecting rod is the L more than L and less than 2 times, when upper slide-bar is located at the most upper of straight sliding groove During end, the vertical range between the upper slide-bar and the output shaft for the motor that rises and falls is L, and the first connecting rod and second connecting rod Tie point is located at the top of upper slide-bar.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710973556.2A CN107757864A (en) | 2017-10-18 | 2017-10-18 | One kind is taken photo by plane unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710973556.2A CN107757864A (en) | 2017-10-18 | 2017-10-18 | One kind is taken photo by plane unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107757864A true CN107757864A (en) | 2018-03-06 |
Family
ID=61268372
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710973556.2A Withdrawn CN107757864A (en) | 2017-10-18 | 2017-10-18 | One kind is taken photo by plane unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107757864A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108423165A (en) * | 2018-05-09 | 2018-08-21 | 重庆零创屹立科技有限公司 | A kind of plant protection drone |
| CN113060272A (en) * | 2021-05-19 | 2021-07-02 | 宜宾职业技术学院 | Unmanned aerial vehicle horn beta structure |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101481015A (en) * | 2009-02-27 | 2009-07-15 | 北京航空航天大学 | Small-sized foldable multi-wheel multi-column support type landing gear |
| CN105620720A (en) * | 2016-03-17 | 2016-06-01 | 舒丹丹 | Aerial photography folding wing unmanned aerial vehicle |
| CN105905301A (en) * | 2016-04-12 | 2016-08-31 | 刘洋 | Intelligent irrigation unmanned aerial vehicle for agricultural production |
| CN107215406A (en) * | 2017-06-26 | 2017-09-29 | 洪幼芬 | One kind building municipal administration robot |
-
2017
- 2017-10-18 CN CN201710973556.2A patent/CN107757864A/en not_active Withdrawn
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101481015A (en) * | 2009-02-27 | 2009-07-15 | 北京航空航天大学 | Small-sized foldable multi-wheel multi-column support type landing gear |
| CN105620720A (en) * | 2016-03-17 | 2016-06-01 | 舒丹丹 | Aerial photography folding wing unmanned aerial vehicle |
| CN105905301A (en) * | 2016-04-12 | 2016-08-31 | 刘洋 | Intelligent irrigation unmanned aerial vehicle for agricultural production |
| CN107215406A (en) * | 2017-06-26 | 2017-09-29 | 洪幼芬 | One kind building municipal administration robot |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108423165A (en) * | 2018-05-09 | 2018-08-21 | 重庆零创屹立科技有限公司 | A kind of plant protection drone |
| CN108423165B (en) * | 2018-05-09 | 2023-06-06 | 重庆零创屹立科技有限公司 | Plant protection unmanned aerial vehicle |
| CN113060272A (en) * | 2021-05-19 | 2021-07-02 | 宜宾职业技术学院 | Unmanned aerial vehicle horn beta structure |
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