CN108528741A - A kind of drop-proof Aerial photography unmanned plane - Google Patents
A kind of drop-proof Aerial photography unmanned plane Download PDFInfo
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- CN108528741A CN108528741A CN201810291825.1A CN201810291825A CN108528741A CN 108528741 A CN108528741 A CN 108528741A CN 201810291825 A CN201810291825 A CN 201810291825A CN 108528741 A CN108528741 A CN 108528741A
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- unmanned plane
- fixedly connected
- aerial photography
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- 230000008602 contraction Effects 0.000 claims description 28
- 230000001105 regulatory effect Effects 0.000 claims description 13
- 238000003860 storage Methods 0.000 claims description 10
- 239000007787 solid Substances 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 8
- 230000002633 protecting effect Effects 0.000 abstract description 7
- 238000000034 method Methods 0.000 description 6
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Studio Devices (AREA)
Abstract
The invention discloses a kind of drop-proof Aerial photography unmanned planes, including Aerial photography unmanned plane, the Aerial photography unmanned plane includes unmanned plane engine base, the top of unmanned plane engine base has been fixedly connected with unmanned aerial vehicle rack with the bottom of unmanned plane engine base, and the lateral surface of unmanned aerial vehicle rack is fixedly connected with unmanned plane wing frame.The present invention is by shrinking adjustment spring, improve the resiliency between tripod, facilitate the difference according to landform, change the angle of tripod, unmanned plane is facilitated to land, and since the support foot lever at the top of tripod with unmanned plane engine base is to be flexibly connected, according to different landform, so that the support direction of tripod is different, improve the stability when landing of Aerial photography unmanned plane, improve support effect, prevent side to fall, improve the protecting effect to unmanned plane, the advantages of reaching shatter-resistant, existing unmanned plane is solved in descent, due to the difference of landform, so that unmanned plane is easy to happen collision in descent, to influence the problem of unmanned plane uses.
Description
Technical field
The present invention relates to space flight and aviation technical field, specially a kind of drop-proof Aerial photography unmanned plane.
Background technology
UAV abbreviation unmanned plane, unmanned plane are to utilize radio robot and the presetting apparatus provided for oneself
The not manned aircraft manipulated, or fully or intermittently automatically operated by car-mounted computer.Compared with manned aircraft,
Unmanned plane is often more suitable for those too slow-witted, dirty or dangerous tasks.Unmanned plane presses application field, can be divided into the military and people
With.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+sector application are that unmanned plane is really rigid
It needs；It taking photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, surveying at present
Paint, news report, electric inspection process, the disaster relief, the application of movies-making, manufacture romance etc. field, greatly expanded unmanned plane
The purposes of itself, developed country is also in actively extension sector application and development unmanned air vehicle technique.
When in use, since unmanned plane is in descent, landform is different, can be caused to unmanned plane in various degree for unmanned plane
Collide with, the damage of unmanned plane is easy to cause, to influence the use of unmanned plane.
Invention content
The purpose of the present invention is to provide a kind of drop-proof Aerial photography unmanned planes, have the advantages of shatter-resistant, solve existing
There is unmanned plane in descent, due to the difference of landform so that unmanned plane is easy to happen collision in descent, to shadow
Ring the problem of unmanned plane uses.
To achieve the above object, the present invention provides the following technical solutions：A kind of drop-proof Aerial photography unmanned plane, including boat
Sky shooting unmanned plane, the Aerial photography unmanned plane includes unmanned plane engine base, top and the unmanned plane machine of the unmanned plane engine base
The bottom of seat has been fixedly connected with unmanned aerial vehicle rack, and the lateral surface of the unmanned aerial vehicle rack is fixedly connected with unmanned plane wing frame,
It is fixedly connected with power seat at the top of the unmanned plane wing frame, line shaft is fixedly connected at the top of the power seat, it is described
Be fixedly connected with restricted cap at the top of line shaft, be fixedly connected with locking cap at the top of the limitation cap, the line shaft it is outer
Side fixing sleeve is connected to fixed ring, and the lateral surface of the fixed ring is fixedly connected with unmanned plane machine leaf, the unmanned plane engine base
Top is fixedly connected with fixed frame, and the quantity of the fixed frame is two, and storing is fixedly connected between two fixed frames
Cylinder, one side of the fixed frame far from storage tube are connected with telescopic adjustment frame, and the lateral surface of the telescopic adjustment frame is lived
Dynamic to be connected with fastening plates, the outer surface of the unmanned plane engine base offers angular adjustment slot, and the inside of the angular adjustment slot is solid
Surely it is connected with fixed link, the outside movable sleeve of the fixed link is connected to support leg bar, and the bottom of the support foot lever is fixedly connected
There is curved support foot rest, the quantity of unmanned plane engine base outer surface angle regulating tank is four, two angular adjustment slots
Positioned at the left side of unmanned plane engine base, angular adjustment slot described in another two is located at the right side of unmanned plane engine base, the curved branch
The quantity of kickstand is two, and the quantity of two curved support foot rest top braces foot levers is two, two songs
Support plate it has been fixedly connected at the top of type support foot rest, the adjacent one sides of two support plates has been fixedly connected with slow
The other end of jumper bar, the buffer bar is fixedly connected with fixed seat, is equipped between two fixed seats and shrinks adjustment spring, and two
The adjacent one side of a fixed seat is fixedly connected with extension rod, and the other end of the extension rod extends to contraction adjustment spring
Inside.
Preferably, the inside of the storage tube offers contraction chamber, and the inside of the fixed frame offers extension opening, institute
The medial surface for stating contraction chamber offers adjusting opening, and the contraction chamber is by adjusting opening and being connected on the outside of storage tube, institute
It states adjusting opening and extends opening and be located at the same horizontal position, the contraction chamber is by adjusting opening and extending opening and fixed frame
Outside be connected.
Preferably, one end that the telescopic adjustment frame is connected with fixed frame is extended to by extending to be open and adjust to be open
The inside of contraction chamber, one end that the telescopic adjustment frame is located inside contraction chamber are fixedly connected with restricted baffle.
Preferably, the quantity of the telescopic adjustment frame is two, and the contraction chamber is internally provided with support spring, the branch
The both ends for supportting spring are fixedly connected with the outer surface of two limitation baffles respectively.
Preferably, the front and the back side of telescopic adjustment frame of the telescopic adjustment frame offer rotation regulating tank, described
The inside of rotation regulating tank is fixedly connected with fixing axle, one end and the fixing axle activity inside rotation regulating tank of the fastening plates
It being socketed, the quantity of fastening plates is two on the outside of a telescopic adjustment frame, and the other end of two fastening plates is connected, two
The other end of a fastening plates is plugged by fixing screws, and the other end of the fixing screws is threaded with fixed spiral shell
Cap.
Preferably, the quantity of unmanned plane wing frame is four on the outside of the Aerial photography unmanned plane, four unmanned planes
Wing frame is arranged in the left side and right side of unmanned aerial vehicle rack in the form of symmetrical.
Preferably, the width value of the contraction chamber be more than adjust opening width value, it is described adjust opening width value with
The width value for extending opening is equal, and the width value of the limitation baffle is more than the width value for adjusting opening.
Preferably, the both ends for shrinking adjustment spring are fixedly connected with the outer surface of two fixed seats respectively, and two
It is formed with permanent opening between the fastening plates.
Compared with prior art, beneficial effects of the present invention are as follows：
1, the present invention facilitates the telescopic adjustment of control telescopic adjustment frame, to facilitate fastening plates to exist by the way that telescopic adjustment frame is arranged
When fixed picture pick-up device, the difference of weight can be answered, the position of both sides telescopic adjustment frame is adjusted, to facilitate guarantee Aerial photography
The balance of unmanned plane both sides ensures the stability of Aerial photography unmanned plane during flying, prevents one end overweight, cause the pendant of unmanned plane
It falls.
2, the present invention is supported Aerial photography unmanned plane by curved support foot rest, and song is designed as due to tripod
Type can land when unmanned plane lands under different landform, due to flattening effect it is preferable, be not susceptible to unmanned plane
Rollover prevent Aerial photography unmanned plane from side occurs to improve to the protecting effect of unmanned plane and fall, improve the guarantor to unmanned plane
Shield.
3, the present invention improves the resiliency between tripod, facilitates the difference according to landform, change by shrinking adjustment spring
The angle of tripod, facilitates unmanned plane to land, and since the support foot lever at the top of tripod with unmanned plane engine base is to be flexibly connected,
To facilitate the angle for changing tripod, to according to different landform so that the support direction of tripod is different, improves Aerial photography
Stability when unmanned plane lands improves support effect, prevents side and fall, and improves the protecting effect to unmanned plane, reaches anti-
The advantages of falling solves existing unmanned plane in descent, due to the difference of landform so that unmanned plane holds in descent
It easily collides, to influence the problem of unmanned plane uses.
Description of the drawings
Fig. 1 is structure of the invention vertical view；
Fig. 2 is structure of the invention side view；
Fig. 3 is structure internal view at A in Fig. 1 of the present invention；
Fig. 4 is structural schematic diagram at B in Fig. 2 of the present invention；
Fig. 5 is partial structurtes side view of the present invention.
In figure：1 Aerial photography unmanned plane, 2 unmanned plane engine bases, 3 unmanned aerial vehicle racks, 4 unmanned plane wing framves, 5 limitation caps, 6
Spiral shell is fixed in locking cap, 7 unmanned plane machine leaves, 8 fixed frames, 9 storage tubes, 10 telescopic adjustment framves, 11 fastening plates, 12 fixing screws, 13
Cap, 14 rotation regulating tanks, 15 fixing axles, 16 power seats, 17 line shafts, 18 fixed rings, 19 support foot levers, 20 curved support legs
Frame, 21 buffer bars, 22 fixed seats, 23 shrink adjustment springs, 24 extension rods, 25 extend openings, 26 contraction chambers, 27 adjust be open,
28 limitation baffles, 29 support springs, 30 angular adjustment slots, 31 fixed links, 32 support plates.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Please refer to Fig.1-5, a kind of drop-proof Aerial photography unmanned plane, including Aerial photography unmanned plane 1, Aerial photography nobody
Machine 1 includes unmanned plane engine base 2, and the top of unmanned plane engine base 2 has been fixedly connected with unmanned aerial vehicle rack with the bottom of unmanned plane engine base 2
3, the lateral surface of unmanned aerial vehicle rack 3 is fixedly connected with unmanned plane wing frame 4,1 outside unmanned plane wing frame 4 of Aerial photography unmanned plane
Quantity be four, four unmanned plane wing framves 4 are arranged in the left side and right side of unmanned aerial vehicle rack 3 in the form of symmetrical, nobody
The top of machine wing frame 4 is fixedly connected with power seat 16, and the top of power seat 16 is fixedly connected with line shaft 17, line shaft 17
Top is fixedly connected with restricted cap 5, and the top of limitation cap 5 is fixedly connected with locking cap 6, and the lateral surface of line shaft 17 is fixedly attached
There are fixed ring 18, the lateral surface of fixed ring 18 to be fixedly connected with unmanned plane machine leaf 7, the top of unmanned plane engine base 2 is fixedly connected with
The quantity of fixed frame 8, fixed frame 8 is two, is fixedly connected with storage tube 9 between two fixed frames 8, fixed frame 8 is far from storing
The one side of cylinder 9 is connected with telescopic adjustment frame 10, and the inside of storage tube 9 offers contraction chamber 26, and the inside of fixed frame 8 is opened
Equipped with opening 25 is extended, the medial surface of contraction chamber 26 offers adjusting opening 27, and contraction chamber 26 is by adjusting opening 27 and storing
The outside of cylinder 9 is connected, and adjusts opening 27 with opening 25 is extended and is located at the same horizontal position, contraction chamber 26 is by adjusting opening 27
It is connected with the outside of fixed frame 8 with opening 25 is extended, one end that telescopic adjustment frame 10 is connected with fixed frame 8 is opened by extending
Mouth 25 and adjusting opening 27 extend to the inside of contraction chamber 26, and telescopic adjustment frame 10 is located at one end inside contraction chamber 26 and fixes company
It is connected to limitation baffle 28, the quantity of telescopic adjustment frame 10 is two, and contraction chamber 26 is internally provided with support spring 29, support spring
29 both ends are fixedly connected with the outer surface of two limitation baffles 28 respectively, and the width value of contraction chamber 26, which is more than, adjusts opening 27
Width value, the width value for adjusting opening 27 is equal with the width value for extending opening 25, and the width value of limitation baffle 28, which is more than, to be adjusted
The width value of opening 27, the lateral surface of telescopic adjustment frame 10 are connected with fastening plates 11, the front of telescopic adjustment frame 10 with stretch
The back side of contracting adjusting bracket 10 offers rotation regulating tank 14, and the inside of rotation regulating tank 14 is fixedly connected with fixing axle 15, tightly
One end of solid plate 11 and 15 pivot bush unit of fixing axle inside rotation regulating tank 14, a 10 outside fastening plates 11 of telescopic adjustment frame
Quantity be two, the other end of two fastening plates 11 is connected, and the other end of two fastening plates 11 passes through 12 phase of fixing screws
The other end of grafting, fixing screws 12 is threaded with hold-doun nut 13, by the way that telescopic adjustment frame 10 is arranged, facilitates control flexible
The telescopic adjustment of adjusting bracket 10 can answer the difference of weight, adjust both sides to facilitate fastening plates 11 in fixed picture pick-up device
The position of telescopic adjustment frame 10 ensures Aerial photography unmanned plane to facilitate the balance for ensureing 1 both sides of Aerial photography unmanned plane
The stability of 1 flight, prevents one end overweight, falling for unmanned plane, the outer surface of unmanned plane engine base 2 is caused to offer angular adjustment
The inside of slot 30, angular adjustment slot 30 is fixedly connected with fixed link 31, and the outside movable sleeve of fixed link 31 is connected to support leg bar 19,
The bottom of support foot lever 19 is fixedly connected with curved support foot rest 20, by curved support foot rest 20 to Aerial photography unmanned plane 1
It is supported, is designed as curved due to tripod, when unmanned plane lands, can land under different landform, due to
Flattening effect is preferable, is not susceptible to the rollover of unmanned plane, to improve to the protecting effect of unmanned plane, prevent Aerial photography nobody
Machine 1 occurs side and falls, and improves the protection to unmanned plane, the quantity of 2 outer surface angle regulating tank 30 of unmanned plane engine base is four, two
Angular adjustment slot 30 is located at the left side of unmanned plane engine base 2, and another two angular adjustment slot 30 is located at the right side of unmanned plane engine base 2
The quantity in face, curved support foot rest 20 is two, and the quantity of two 20 top braces foot levers 19 of curved support foot rest is two,
The top of two curved support foot rests 20 has been fixedly connected with support plate 32, and the adjacent one side of two support plates 32 is fixed
It is connected with buffer bar 21, the other end of buffer bar 21 is fixedly connected with fixed seat 22, is equipped with to shrink between two fixed seats 22 and adjust
Spring 23 is saved, two adjacent one sides of fixed seat 22 are fixedly connected with extension rod 24, and the other end of extension rod 24 extends to receipts
The inside of contracting adjustment spring 23, the both ends for shrinking adjustment spring 23 are fixedly connected with the outer surface of two fixed seats 22 respectively, and
It is formed with permanent opening between two fastening plates 11, by shrinking adjustment spring 23, the resiliency between tripod is improved, facilitates root
According to the difference of landform, change the angle of tripod, unmanned plane is facilitated to land, and due to the support foot lever 19 and nothing at the top of tripod
Man-machine engine base 2 is flexible connection, to facilitate the angle for changing tripod, to according to different landform so that the support of tripod
Direction is different, improves stability when Aerial photography unmanned plane 1 lands, improves support effect, prevent side and fall, improves to nothing
Man-machine protecting effect, solves existing unmanned plane in descent, due to the difference of landform, makes the advantages of reaching shatter-resistant
It obtains unmanned plane and is easy to happen collision in descent, to influence the problem of unmanned plane uses.
In summary：The drop-proof Aerial photography unmanned plane facilitates control telescopic adjustment by the way that telescopic adjustment frame 10 is arranged
The telescopic adjustment of frame 10 can answer the difference of weight, it is flexible to adjust both sides to facilitate fastening plates 11 in fixed picture pick-up device
The position of adjusting bracket 10 ensures that Aerial photography unmanned plane 1 flies to facilitate the balance for ensureing 1 both sides of Aerial photography unmanned plane
Capable stability prevents one end overweight, causes falling for unmanned plane, by curved support foot rest 20 to Aerial photography unmanned plane 1
It is supported, is designed as curved due to tripod, when unmanned plane lands, can land under different landform, due to
Flattening effect is preferable, is not susceptible to the rollover of unmanned plane, to improve to the protecting effect of unmanned plane, prevent Aerial photography nobody
Machine 1 occurs side and falls, and improves the protection to unmanned plane, by shrinking adjustment spring 23, improves the resiliency between tripod, facilitates root
According to the difference of landform, change the angle of tripod, unmanned plane is facilitated to land, and due to the support foot lever 19 and nothing at the top of tripod
Man-machine engine base 2 is flexible connection, to facilitate the angle for changing tripod, to according to different landform so that the support of tripod
Direction is different, improves stability when Aerial photography unmanned plane 1 lands, improves support effect, prevent side and fall, improves to nothing
Man-machine protecting effect, solves existing unmanned plane in descent, due to the difference of landform, makes the advantages of reaching shatter-resistant
It obtains unmanned plane and is easy to happen collision in descent, to influence the problem of unmanned plane uses.
It should be noted that herein, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also include other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.In the absence of more restrictions.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (8)
1. a kind of drop-proof Aerial photography unmanned plane, including Aerial photography unmanned plane（1）, it is characterised in that：The Aerial photography
Unmanned plane（1）Including unmanned plane engine base（2）, the unmanned plane engine base（2）Top and unmanned plane engine base（2）Bottom it is fixed
It is connected with unmanned aerial vehicle rack（3）, the unmanned aerial vehicle rack（3）Lateral surface be fixedly connected with unmanned plane wing frame（4）, the nothing
Man-machine wing frame（4）Top be fixedly connected with power seat（16）, the power seat（16）Top be fixedly connected with line shaft
（17）, the line shaft（17）Top be fixedly connected with restricted cap（5）, the limitation cap（5）Top be fixedly connected with
Determine cap（6）, the line shaft（17）Lateral surface fixing sleeve be connected to fixed ring（18）, the fixed ring（18）Lateral surface fix
It is connected with unmanned plane machine leaf（7）, the unmanned plane engine base（2）Top be fixedly connected with fixed frame（8）, the fixed frame（8）
Quantity be two, two fixed frames（8）Between be fixedly connected with storage tube（9）, the fixed frame（8）Far from storage tube
（9）One side be connected with telescopic adjustment frame（10）, the telescopic adjustment frame（10）Lateral surface be connected with fastening
Plate（11）, the unmanned plane engine base（2）Outer surface offer angular adjustment slot（30）, the angular adjustment slot（30）Inside
It is fixedly connected with fixed link（31）, the fixed link（31）Outside movable sleeve be connected to support leg bar（19）, the support foot lever
（19）Bottom be fixedly connected with curved support foot rest（20）, the unmanned plane engine base（2）Outer surface angle regulating tank（30）'s
Quantity is four, two angular adjustment slots（30）Positioned at unmanned plane engine base（2）Left side, angular adjustment described in another two
Slot（30）Positioned at unmanned plane engine base（2）Right side, the curved support foot rest（20）Quantity be two, two are described curved
Support foot rest（20）Top braces foot lever（19）Quantity be two, two curved support foot rests（20）Top it is solid
Surely it is connected with support plate（32）, two support plates（32）Adjacent one side be fixedly connected with buffer bar（21）, institute
State buffer bar（21）The other end be fixedly connected with fixed seat（22）, two fixed seats（22）Between be equipped with shrink adjust bullet
Spring（23）, two fixed seats（22）Adjacent one side is fixedly connected with extension rod（24）, the extension rod（24）It is another
One end extends to contraction adjustment spring（23）Inside.
2. a kind of drop-proof Aerial photography unmanned plane according to claim 1, it is characterised in that：The storage tube（9）'s
Inside offers contraction chamber（26）, the fixed frame（8）Inside offer extension opening（25）, the contraction chamber（26）It is interior
Side offers adjusting opening（27）, the contraction chamber（26）It is open by adjusting（27）With storage tube（9）Outside be connected,
The adjusting opening（27）It is open with extending（25）Positioned at the same horizontal position, the contraction chamber（26）It is open by adjusting（27）
It is open with extending（25）With fixed frame（8）Outside be connected.
3. a kind of drop-proof Aerial photography unmanned plane according to claim 1, it is characterised in that：The telescopic adjustment frame
（10）With fixed frame（8）The one end being connected is open by extending（25）It is open with adjusting（27）Extend to contraction chamber（26）It is interior
Portion, the telescopic adjustment frame（10）Positioned at contraction chamber（26）Internal one end is fixedly connected with restricted baffle（28）.
4. a kind of drop-proof Aerial photography unmanned plane according to claim 1 or 2, it is characterised in that：The telescopic adjustment
Frame（10）Quantity be two, the contraction chamber（26）Be internally provided with support spring（29）, the support spring（29）Two
End limits baffles with two respectively（28）Outer surface be fixedly connected.
5. a kind of drop-proof Aerial photography unmanned plane according to claim 1, it is characterised in that：The telescopic adjustment frame
（10）Front with telescopic adjustment frame（10）The back side offer rotation regulating tank（14）, the rotation regulating tank（14）It is interior
Portion is fixedly connected with fixing axle（15）, the fastening plates（11）One end with rotation regulating tank（14）Internal fixing axle（15）It is living
Dynamic socket, a telescopic adjustment frame（10）Outside fastening plates（11）Quantity be two, two fastening plates（11）'s
The other end is connected, two fastening plates（11）The other end pass through fixing screws（12）It plugs, the fixing screws
（12）The other end be threaded with hold-doun nut（13）.
6. a kind of drop-proof Aerial photography unmanned plane according to claim 1, it is characterised in that：The Aerial photography nobody
Machine（1）Outside unmanned plane wing frame（4）Quantity be four, four unmanned plane wing framves（4）It is arranged in the form of symmetrical
In unmanned aerial vehicle rack（3）Left side and right side.
7. a kind of drop-proof Aerial photography unmanned plane according to claim 1, it is characterised in that：The contraction chamber（26）'s
Width value, which is more than to adjust, to be open（27）Width value, adjusting opening（27）Width value with extend be open（25）Width value
It is equal, the limitation baffle（28）Width value be more than adjust be open（27）Width value.
8. a kind of drop-proof Aerial photography unmanned plane according to claim 1, it is characterised in that：The contraction adjustment spring
（23）Both ends respectively with two fixed seats（22）Outer surface be fixedly connected, and two fastening plates（11）Between be formed with
Permanent opening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810291825.1A CN108528741A (en) | 2018-04-03 | 2018-04-03 | A kind of drop-proof Aerial photography unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810291825.1A CN108528741A (en) | 2018-04-03 | 2018-04-03 | A kind of drop-proof Aerial photography unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108528741A true CN108528741A (en) | 2018-09-14 |
Family
ID=63482347
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810291825.1A Withdrawn CN108528741A (en) | 2018-04-03 | 2018-04-03 | A kind of drop-proof Aerial photography unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108528741A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109436326A (en) * | 2018-11-16 | 2019-03-08 | 浙江云来集科技有限公司 | A kind of cruise automatic protection unmanned plane |
| CN117028811A (en) * | 2023-09-08 | 2023-11-10 | 顺德职业技术学院 | Monitoring device based on artificial intelligence and application method thereof |
-
2018
- 2018-04-03 CN CN201810291825.1A patent/CN108528741A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109436326A (en) * | 2018-11-16 | 2019-03-08 | 浙江云来集科技有限公司 | A kind of cruise automatic protection unmanned plane |
| CN109436326B (en) * | 2018-11-16 | 2024-04-26 | 浙江云来集科技有限公司 | Automatic protection unmanned aerial vehicle cruises |
| CN117028811A (en) * | 2023-09-08 | 2023-11-10 | 顺德职业技术学院 | Monitoring device based on artificial intelligence and application method thereof |
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Effective date of registration: 20191225 Address after: Collective household, 114 Qingnian Road, Baohe District, Hefei City, Anhui Province, 230000 Applicant after: Li Yanyan Address before: 241000 room 1401, office building, block C, Huaqiang Plaza, Jinghu District, Wuhu, Anhui. Applicant before: Wuhu superke mechanical and Electrical Equipment Co., Ltd. |
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Application publication date: 20180914 |