CN107757884A - A kind of unmanned plane take-off and landing device for being applicable to sizes - Google Patents
A kind of unmanned plane take-off and landing device for being applicable to sizes Download PDFInfo
- Publication number
- CN107757884A CN107757884A CN201711145053.2A CN201711145053A CN107757884A CN 107757884 A CN107757884 A CN 107757884A CN 201711145053 A CN201711145053 A CN 201711145053A CN 107757884 A CN107757884 A CN 107757884A
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- China
- Prior art keywords
- unmanned plane
- supporting plate
- plate
- fixedly connected
- applicable
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Classifications
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- 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
-
- 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
- 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
- B64C25/64—Spring shock-absorbers; Springs using rubber or like elements
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of unmanned plane take-off and landing device for being applicable to sizes, including the first supporting plate, the left and right sides of first support plate upper surface offers through hole, and the left and right sides of two through-hole walls are fixedly connected by two the first slide bars respectively, and the surface of two the first slide bars is socketed with the first sliding sleeve, and two the first sliding sleeves are respectively engaged with the opposite face of two the first fixed plates.This is applicable to the unmanned plane take-off and landing device of sizes, by setting the first supporting plate, loading plate, the first fixed plate, threaded post, thread barrel, dual-axle motor, electric pushrod, expansion link and spring, so as to be preferably adjusted to the position of loading plate, on the ground the bottom of unmanned plane is caused to wear so as to avoid unmanned plane from parking, the position of loading plate can be adjusted simultaneously, loading plate is adapted to rising and falling for a variety of unmanned planes, avoid influenceing the use to unmanned plane.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, specially a kind of unmanned plane take-off and landing device for being applicable to sizes.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently independently operated by car-mounted computer.Compared with manned aircraft, nobody
Machine is often more suitable for those too slow-witted, dirty or dangerous tasks.Unmanned plane presses application field, can be divided into it is military with it is civilian.Army
With aspect, unmanned plane is divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane sector application, it is that unmanned plane has really just needed.At present
Take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news
Report, electric inspection process, the disaster relief, movies-making and the application in manufacture romance etc. field, unmanned plane is greatly expanded in itself
Purposes, developed country is also in actively extension sector application and development unmanned air vehicle technique.
Current unmanned plane is mostly directly to park on the ground, and impulsive force can be produced when decline due to unmanned plane, with
Ground easily causes to wear when contacting to the bottom of unmanned plane, can cause the damage of unmanned plane in the past for a long time, and currently for nothing
Man-machine take-off and landing device can only be applicable a kind of unmanned plane of size, be unfavorable for rising and falling for unmanned plane, influence the use to unmanned plane.
The content of the invention
(1) technical problem solved
In view of the shortcomings of the prior art, the invention provides a kind of unmanned plane take-off and landing device for being applicable to sizes,
It is mostly directly to park on the ground to solve current unmanned plane, impulsive force can be produced when decline due to unmanned plane, with ground
Face easily causes to wear when contacting to the bottom of unmanned plane, can cause the damage of unmanned plane in the past for a long time, and currently for nobody
The take-off and landing device of machine can only be applicable a kind of unmanned plane of size, be unfavorable for rising and falling for unmanned plane, and influence to use unmanned plane asks
Topic.
(2) technical scheme
To achieve the above object, the present invention provides following technical scheme：A kind of unmanned plane for being applicable to sizes rises
Dropping control device, including the first supporting plate, the left and right sides of first support plate upper surface offer through hole, and in two through holes
The left and right sides of wall are fixedly connected by two the first slide bars respectively, and the surface of two the first slide bars is socketed with the first cunning
Set, and two the first sliding sleeves are respectively engaged with the opposite face of two the first fixed plates, and the positive and back of the body of two the first fixed plates
Face overlaps with the front and back of two through-hole walls respectively, and the upper surface of two the first fixed plates respectively with two loading plates
Lower surface be fixedly connected, and the lower surface of two loading plates overlaps with the upper surface of the first supporting plate, and two loading plates
Opposite face overlapped respectively with the two sides of support bar, and the lower surface of two loading plates is fixedly connected with the second fixed plate, and
One end that the opposite face of two the second fixed plates is located remotely from each other with two the second slide bars respectively is fixedly connected, and two the second slide bars
Surface be socketed with the second sliding sleeve, and two the second sliding sleeves are respectively engaged with the opposite face of two the 3rd fixed plates, and two
Lower surface of the upper surface of 3rd fixed plate with the first supporting plate is fixedly connected.
The opposite face of two the 3rd fixed plates is connected with bearing, and rotating shaft is socketed with two bearings, and two axles
Hold the lower section for being respectively positioned on two the second sliding sleeves, and one end that the relative one end of two rotating shafts is located remotely from each other with two threaded posts respectively
Be fixedly connected, and two threaded posts hand of spiral on the contrary, and the surfaces of two threaded posts be socketed with thread barrel, and two spiral shells
Line cylinder is respectively engaged with the opposite face of two the first fixed plates, and the relative one end of two threaded posts respectively with dual-axle motor two
Individual output shaft is fixedly connected, and the fuselage of the dual-axle motor is fixedly connected with the lower surface of the first supporting plate, first support
Plate lower surface is provided with electric pushrod close to the position of corner, and the bottom of four electric pushrods has been fixedly connected with second
Supporting plate, and the front and rear sides of the front and rear sides of lower surface and right side loading plate right side lower surface pass through on the left of the loading plate of left side
Expansion link is fixedly connected with the upper surface of the 3rd supporting plate, and the surface of four expansion links is socketed with spring, and four springs
Opposite face of the both ends respectively with loading plate and the 3rd supporting plate be fixedly connected.
Preferably, the surface of the 3rd supporting plate is provided with slipmat, the shape of the 3rd supporting plate and slipmat
It is circle.
Preferably, the described one end of second slide bar away from the second fixed plate is fixedly connected with baffle plate, the shape of the baffle plate
For circle.
Preferably, the front of the support bar is provided with battery, the output end of the battery and control panel it is defeated
Enter end electrical connection.
Preferably, the control panel is arranged on the front of support bar, and the control panel is located at the left side of battery, institute
Input of the output end of control panel respectively with dual-axle motor and electric pushrod is stated to electrically connect.
Preferably, the width of first supporting plate is 0.7 times of loading plate width, the width of the loading plate and support
The width of bar is identical.
(3) beneficial effect
The invention provides a kind of unmanned plane take-off and landing device for being applicable to sizes, possesses following beneficial effect：
(1), unmanned plane take-off and landing device for being applicable to sizes, by setting the first supporting plate, loading plate, first
Fixed plate, threaded post, thread barrel, dual-axle motor, electric pushrod, expansion link and spring, carried out when needing the position to loading plate
During adjustment, the work of dual-axle motor is controlled by control panel, two output shafts of dual-axle motor can drive two threaded posts
Rotate, so as to so that two thread barrels are close to each other or remote, so as to when slipmat is with surface separation to holding
The position of support plate is adjusted, and controls the work of electric pushrod, electric pushrod can make when working the first supporting plate rise or
Decline, so as to control being contacting and separating for slipmat and ground, so as to preferably be adjusted to the position of loading plate
It is whole, on the ground the bottom of unmanned plane is caused to wear so as to avoid unmanned plane from parking, while can be to the position of loading plate
Put and be adjusted, loading plate is adapted to rising and falling for a variety of unmanned planes, avoid influenceing the use to unmanned plane.
(2), unmanned plane take-off and landing device for being applicable to sizes, by setting spring, when unmanned plane falls on carrying
When on plate, spring shortens, and can enter row buffering to impulsive force caused by unmanned plane landing.
(3), the unmanned plane take-off and landing device for being applicable to sizes, can by setting the first slide bar and the second slide bar
So that loading plate movement is more stable, and the present invention is compact-sized, reasonable in design, practical.
Brief description of the drawings
Fig. 1 is the cross-sectional view that the present invention faces；
Fig. 2 is the structural representation that the present invention faces.
In figure：1 first supporting plate, 2 through holes, 3 first slide bars, 4 first sliding sleeves, 5 first fixed plates, 6 loading plates, 7 supports
Bar, 8 second fixed plates, 9 second slide bars, 10 second sliding sleeves, 11 the 3rd fixed plates, 12 bearings, 13 rotating shafts, 14 threaded posts, 15 spiral shells
It is line cylinder, 16 dual-axle motors, 17 electric pushrods, 18 second supporting plates, 19 expansion links, 20 the 3rd supporting plates, 21 springs, 22 anti-skidding
Pad, 23 baffle plates, 24 batteries, 25 control panels.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, rather than whole embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other under the premise of creative work is not made
Embodiment, belong to the scope of protection of the invention.
As shown in Figure 1-2, the present invention provides a kind of technical scheme：A kind of unmanned plane for being applicable to sizes rises and falls dress
Put, including the first supporting plate 1, the width of the first supporting plate 1 are 0.7 times of the width of loading plate 6, by setting the first supporting plate 1,
Loading plate 6 can be supported, while preferably the position of loading plate 6 can be adjusted, allow loading plate 6 more preferable
Adaptation sizes unmanned plane, the width of loading plate 6 is identical with the width of support bar 7, a left side for the upper surface of the first supporting plate 1
Right both sides offer through hole 2, and the left and right sides of two inwalls of through hole 2 are fixedly connected by two the first slide bars 3 respectively,
And the surface of two the first slide bars 3 is socketed with the first sliding sleeve 4, and two the first sliding sleeves 4 are respectively engaged with two first fixations
The opposite face of plate 5, and front and back of the front and back of two the first fixed plates 5 respectively with two inwalls of through hole 2 overlaps,
By setting the first fixed plate 5, when thread barrel 15 when the surface of threaded post 14 is moved can the first fixed plate 5 of band move, from
And loading plate 6 can be driven to move, and the upper surface of two the first fixed plates 5 lower surface with two loading plates 6 respectively
It is fixedly connected, and the lower surface of two loading plates 6 overlaps with the upper surface of the first supporting plate 1, and two loading plates 6 is relative
Face overlaps with the two sides of support bar 7 respectively, and the front of support bar 7 is provided with battery 24, by setting battery 24, is easy to
Dual-axle motor 16 and the electricity consumption of electric pushrod 17 are operated, and the output end and the input of control panel 25 of battery 24 are electrically connected
Connect, control panel 25 is arranged on the front of support bar 7, and control panel 25 is located at the left side of battery 24, by setting chain of command
Plate 25, can preferably control dual-axle motor 16 and electric pushrod 17 to be operated, the output end of control panel 25 respectively with it is double
The input of spindle motor 16 and electric pushrod 17 electrically connects, and the lower surface of two loading plates 6 is fixedly connected with the second fixed plate
8, and one end that the opposite face of two the second fixed plates 8 is located remotely from each other with two the second slide bars 9 respectively is fixedly connected, the second slide bar
9 one end away from the second fixed plate 8 are fixedly connected with baffle plate 23, and baffle plate 23 is shaped as circle, can be with by setting baffle plate 23
Prevent the second slide bar 9 from being separated with the second sliding sleeve 10, and the surface of two the second slide bars 9 is socketed with the second sliding sleeve 10, by setting
The first slide bar 3 and the second slide bar 9 are put, can move the first fixed plate 5 more stable, while the second slide bar 9 can be to holding
The fixation of support plate 6, and two the second sliding sleeves 10 are respectively engaged with the opposite face of two the 3rd fixed plates 11, and two the 3rd fixations
Lower surface of the upper surface of plate 11 with the first supporting plate 1 is fixedly connected.
The opposite face of two the 3rd fixed plates 11 is connected with bearing 12, and is socketed with rotating shaft 13 in two bearings 12,
And two bearings 12 are respectively positioned on the lower section of two the second sliding sleeves 10, and the relative one end of two rotating shafts 13 respectively with two threaded posts
14 one end being located remotely from each other are fixedly connected, and two threaded posts 14 hand of spiral on the contrary, and two threaded posts 14 surface it is equal
Thread barrel 15 is socketed with, by being threaded post 14 and thread barrel 15, when dual-axle motor 16 works, two of dual-axle motor 16
Output shaft can drive two threaded posts 14 to rotate, so as to by the direction controlling to 16 two output shaft rotations of dual-axle motor,
Two thread barrels 15 can be controlled to be located remotely from each other or close to each other, and two thread barrels 15 are respectively engaged with two first fixations
The opposite face of plate 5, and the relative one end of two threaded posts 14 is fixedly connected with two output shafts of dual-axle motor 16 respectively, twin shaft
The fuselage of motor 16 is fixedly connected with the lower surface of the first supporting plate 1, by setting dual-axle motor 16, control dual-axle motor 16
Work, the output shaft of dual-axle motor 16 can drive threaded post 14 to rotate, so as to so that thread barrel 15 on the surface of threaded post 14
Moving, the lower surface of the first supporting plate 1 is provided with electric pushrod 17 close to the position of corner, and four electric pushrods 17
Bottom has been fixedly connected with the second supporting plate 18, by setting electric pushrod 17, controls the work of electric pushrod 17, electronic to push away
When elongating or shortening first supporting plate 1 can move up and down bar 17, so as to preferably be adjusted to the position of loading plate 6
It is whole, and the front and rear sides of the front and rear sides of the left side lower surface of left side loading plate 6 and the right side lower surface of right side loading plate 6 are by stretching
Contracting bar 19 is fixedly connected with the upper surface of the 3rd supporting plate 20, and the surface of four expansion links 19 is socketed with spring 21, passes through
Set expansion link 19 and spring 21, expansion link 19 to be supported to loading plate 6, while spring 21 can be fixed,
When unmanned plane is fallen on loading plate 6, spring 21 shortens, and can enter row buffering to impulsive force caused by unmanned plane landing, and
Opposite face of the both ends of four springs 21 respectively with the supporting plate 20 of loading plate 6 and the 3rd is fixedly connected, the table of the 3rd supporting plate 20
Face is provided with slipmat 22, and the shape of the 3rd supporting plate 20 and slipmat 22 is circle, by setting slipmat 22, Ke Yizeng
Add the 3rd supporting plate 20 and the frictional force on ground, preferably loading plate 6 can be fixed.
Operation principle：Electric pushrod 17 is controlled to work by control panel 25, the elongation of electric pushrod 17 makes the second supporting plate
18 move down, and are raised above the first supporting plate 1 when the second supporting plate 18 contacts with ground, when slipmat 22 and ground distributor
From when by control panel 25 control electric pushrod 17 be stopped, then pass through control panel 25 control the work of dual-axle motor 16
Make, so as to which two threaded posts 14 are located remotely from each other two thread barrels 15, so as to which two thread barrels 15 drive two the first fixed plates 5
It is located remotely from each other, so that two loading plates 6 are located remotely from each other, while two loading plates 6 are located remotely from each other two the second fixed plates 8,
Two the second fixed plates 8 drive two the second slide bars 9 to be located remotely from each other simultaneously, so as to be carried out to the position of two loading plates 6
Adjustment, control dual-axle motor 16 to be stopped by control panel 25 when reaching required result, then pass through chain of command
Plate 25 controls electric pushrod 17 to work, and electric pushrod 17, which shortens, moves down the first supporting plate 1, when slipmat 22 connects with ground
After touch, then electric pushrod 17 is controlled to be stopped by control panel 25, when needing the position of loading plate 6 to set back,
Electric pushrod 17 is controlled to work by control panel 25, the elongation of electric pushrod 17 moves down the second supporting plate 18, when second
When supporting plate 18 contacts with ground and slipmat 22 is with surface separation, electric pushrod 17 is controlled to stop work by control panel 25
Make, then control dual-axle motor 16 to work by control panel 25, two output shafts of dual-axle motor 16 drive two threaded posts
14 rotate backward, so that two thread barrels 15 are close to each other, so that two the first fixed plates 5 are close to each other, so that two
Individual loading plate 6 is close to each other, passes through control panel 25 when the opposite face of two loading plates 6 overlaps with the two sides of support bar 7
Control dual-axle motor 16 is stopped, and then controls electric pushrod 17 to work by control panel 25, and electric pushrod 17, which shortens, to be made
First supporting plate 1 moves down, and when slipmat 22 contacts with ground and the second supporting plate 18 is with surface separation, passes through chain of command
Plate 25 controls electric pushrod 17 to be stopped, meanwhile, when the second supporting plate 18 is falling on loading plate 6 with surface separation and unmanned plane
When upper, loading plate 6 is moved down, and spring 21 and expansion link 19 shorten, and caused punching on loading plate 6 can be fallen on to unmanned plane
Hit power and enter row buffering.
It can to sum up obtain, this is applicable to the unmanned plane take-off and landing device of sizes, by setting the first supporting plate 1, carrying
Plate 6, the first fixed plate 5, threaded post 14, thread barrel 15, dual-axle motor 16, electric pushrod 17, expansion link 19 and spring 21, when need
When being adjusted to the position of loading plate 6, by control panel 25 control dual-axle motor 16 work, the two of dual-axle motor 16
Individual output shaft can drive two threaded posts 14 to rotate, so as to so that two thread barrels 15 are close to each other or remote, so as to
So that in slipmat 22, with being adjusted when surface separation to the position of loading plate 6, the work of control electric pushrod 17 is electronic
Push rod 17 can make the first supporting plate 1 rise or decline when working, so as to control contact of the slipmat 22 with ground and
Separation, so as to be preferably adjusted to the position of loading plate 6, so as to avoid unmanned plane from parking on the ground to nothing
Man-machine bottom is caused to wear, while the position of loading plate 6 can be adjusted, make loading plate 6 be adapted to it is a variety of nobody
Machine rises and falls, and avoids influenceing the use to unmanned plane.
Meanwhile this is applicable to the unmanned plane take-off and landing device of sizes, by setting spring 21, held when unmanned plane is fallen on
When on support plate 6, spring 21 shortens, and can enter row buffering to impulsive force caused by unmanned plane landing.
Meanwhile this is applicable to the unmanned plane take-off and landing device of sizes, by setting the first slide bar 3 and the second slide bar 9,
It can move loading plate 6 more stable, and the present invention is compact-sized, it is reasonable in design, it is practical.
Although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of changes, modification can be carried out to these embodiments, replace without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of unmanned plane take-off and landing device for being applicable to sizes, including the first supporting plate (1), it is characterised in that：It is described
The left and right sides of the first supporting plate (1) upper surface offers through hole (2), and the left and right sides of two through hole (2) inwalls point
It is not fixedly connected by two the first slide bars (3), and the surface of two the first slide bars (3) is socketed with the first sliding sleeve (4), and two
Individual first sliding sleeve (4) is respectively engaged with the opposite face of two the first fixed plates (5), and the front of two the first fixed plates (5) and
The back side overlaps with the front and back of two through hole (2) inwalls respectively, and the upper surface of two the first fixed plates (5) is respectively with two
The lower surface of individual loading plate (6) is fixedly connected, and upper surface of the lower surface of two loading plates (6) with the first supporting plate (1)
Overlap joint, and two sides of the opposite face of two loading plates (6) respectively with support bar (7) overlap, and the following table of two loading plates (6)
Face is fixedly connected with the second fixed plate (8), and the opposite face of two the second fixed plates (8) respectively with two the second slide bar (9) phases
Mutually remote one end is fixedly connected, and the surface of two the second slide bars (9) is socketed with the second sliding sleeve (10), and two second cunnings
Set (10) is respectively engaged with the opposite faces of two the 3rd fixed plates (11), and the upper surface of two the 3rd fixed plates (11) is with the
The lower surface of one supporting plate (1) is fixedly connected；
The opposite face of two the 3rd fixed plates (11) is connected with bearing (12), and is socketed with rotating shaft in two bearings (12)
(13), and two bearings (12) are respectively positioned on the lower section of two the second sliding sleeves (10), and one end difference that two rotating shafts (13) are relative
The one end being located remotely from each other with two threaded posts (14) is fixedly connected, and the hand of spiral of two threaded posts (14) is on the contrary, and two
The surface of threaded post (14) is socketed with thread barrel (15), and two thread barrels (15) are respectively engaged with two the first fixed plates
(5) opposite face, and the relative one end of two threaded posts (14) is fixedly connected with two output shafts of dual-axle motor (16) respectively,
The fuselage of the dual-axle motor (16) is fixedly connected with the lower surface of the first supporting plate (1), the first supporting plate (1) lower surface
Electric pushrod (17) is provided with close to the position of corner, and the bottom of four electric pushrods (17) has been fixedly connected with second
Supporting plate (18), and on the left of left side loading plate (6) front and rear sides of lower surface and lower surface on the right side of right side loading plate (6) it is front and rear
Both sides are fixedly connected by expansion link (19) with the upper surface of the 3rd supporting plate (20), and the surface of four expansion links (19) is equal
Spring (21) is socketed with, and opposite face of the both ends of four springs (21) respectively with loading plate (6) and the 3rd supporting plate (20) is consolidated
Fixed connection.
A kind of 2. unmanned plane take-off and landing device for being applicable to sizes according to claim 1, it is characterised in that：It is described
The surface of 3rd supporting plate (20) is provided with slipmat (22), and the shape of the 3rd supporting plate (20) and slipmat (22) is
It is circular.
A kind of 3. unmanned plane take-off and landing device for being applicable to sizes according to claim 1, it is characterised in that：It is described
The one end of second slide bar (9) away from the second fixed plate (8) is fixedly connected with baffle plate (23), and the baffle plate (23) is shaped as justifying
Shape.
A kind of 4. unmanned plane take-off and landing device for being applicable to sizes according to claim 1, it is characterised in that：It is described
The front of support bar (7) is provided with battery (24), the output end of the battery (24) and the input of control panel (25)
Electrical connection.
A kind of 5. unmanned plane take-off and landing device for being applicable to sizes according to claim 4, it is characterised in that：It is described
Control panel (25) is arranged on the front of support bar (7), and the control panel (25) is located at the left side of battery (24), the control
Input of the output end of panel (25) processed respectively with dual-axle motor (16) and electric pushrod (17) electrically connects.
A kind of 6. unmanned plane take-off and landing device for being applicable to sizes according to claim 1, it is characterised in that：It is described
The width of first supporting plate (1) is 0.7 times of loading plate (6) width, the width of the loading plate (6) and the width of support bar (7)
Spend identical.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711145053.2A CN107757884A (en) | 2017-11-17 | 2017-11-17 | A kind of unmanned plane take-off and landing device for being applicable to sizes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711145053.2A CN107757884A (en) | 2017-11-17 | 2017-11-17 | A kind of unmanned plane take-off and landing device for being applicable to sizes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107757884A true CN107757884A (en) | 2018-03-06 |
Family
ID=61279772
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711145053.2A Withdrawn CN107757884A (en) | 2017-11-17 | 2017-11-17 | A kind of unmanned plane take-off and landing device for being applicable to sizes |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107757884A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108791833A (en) * | 2018-06-19 | 2018-11-13 | 郑州秉茂达电子科技有限公司 | A kind of unmanned plane amphibious landing gear |
| CN110329493A (en) * | 2019-07-29 | 2019-10-15 | 江苏虹彩航空科技有限公司 | A kind of monitoring unmanned equipment stable supporting device |
| CN110395401A (en) * | 2019-07-16 | 2019-11-01 | 董杭民 | A kind of adjustable unmanned plane of taking photo by plane rises and falls platform |
-
2017
- 2017-11-17 CN CN201711145053.2A patent/CN107757884A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108791833A (en) * | 2018-06-19 | 2018-11-13 | 郑州秉茂达电子科技有限公司 | A kind of unmanned plane amphibious landing gear |
| CN110395401A (en) * | 2019-07-16 | 2019-11-01 | 董杭民 | A kind of adjustable unmanned plane of taking photo by plane rises and falls platform |
| CN110329493A (en) * | 2019-07-29 | 2019-10-15 | 江苏虹彩航空科技有限公司 | A kind of monitoring unmanned equipment stable supporting device |
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Application publication date: 20180306 |