CN207045777U - A kind of unmanned aerial vehicle ejecting frame - Google Patents
A kind of unmanned aerial vehicle ejecting frame Download PDFInfo
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- CN207045777U CN207045777U CN201721037620.8U CN201721037620U CN207045777U CN 207045777 U CN207045777 U CN 207045777U CN 201721037620 U CN201721037620 U CN 201721037620U CN 207045777 U CN207045777 U CN 207045777U
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- expelling plate
- rotary shaft
- aerial vehicle
- pedestal
- unmanned aerial
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Abstract
A kind of unmanned aerial vehicle ejecting frame involved by the utility model,Including pedestal and expelling plate,The expelling plate is placed in above pedestal,Contiguous block is welded with the left of the expelling plate,The contiguous block side is provided with connecting hole,Rotary shaft neck and fixing groove are provided with the top of the pedestal,The rotary shaft neck is placed on the inside of fixing groove,Rotary shaft is provided with the rotary shaft neck inner chamber,Launching seat is connected with the top of the rotary shaft,The launching seat two bottom sides are arranged with fixed column,The fixed column is respectively positioned in the fixing groove inner chamber,Fixed mount and ram pot are provided with the top of the launching seat,The fixed mount is located on the left of ram pot,Elevating lever is provided with the hydraulic pressure tube inner chamber,The launch angle of unmanned plane and the initial velocity of transmitting can arbitrarily be adjusted,Being capable of very intuitively measurement data by scale,The direction that transmitting needs is rotated at random while can need not moving transmitting station,Transmitting is steady,Ensure machine service life,It is simple to operate.
Description
Technical field
A kind of unmanned aerial vehicle ejecting frame is the utility model is related to, belongs to unmanned air vehicle technique field.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned vehicle that presetting apparatus manipulates, unmanned plane is actually the general designation of unmanned vehicle, from technical standpoint
Definition can be divided into, and this is several for depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol
Major class, compared with manned aircraft, it has small volume, low cost, easy to use, low to operational environment requirement, battlefield existence energy
The advantages that power is stronger, because UAV has great significance to Future Air Combat, each main military country of the world all exists
Step up to carry out the development work of UAV, the equipment of taking photo by plane used now come into the unmanned epoch, in fact without
Man-machine principle is very simple, and it is controlled by radio robot, makes to be arranged on not on manned vehicle
Equipment carry out work, under the situation that each Informatization construction develops rapidly in China, digital city, Major Figures, numeral
The digital Construction processes such as forestry, Digital Environmental Protection, digital public security, the digital energy are substantially accelerated, and have been achieved with certain achievement,
As needed, volume and renewal map are timely repaiied, is to be integrated with high-altitude shooting, remote control, telemetry, video image microwave transmission
With the new application technology of computer image information processing, carry out zonule remote sensing using unmanned plane and take photo by plane technology, in practice
Achieve significant results and experience, the miniature aerial remote sens ing technique using unmanned plane as aerial remote sensing platform, adapt to national economy and
The needs of cultural construction development, are provided effectively for the small and medium-sized cities particularly regional economy such as city, town, county, township and cultural construction
The remote sensing technology means of services, remote sensing technology of taking photo by plane has important facilitation to China's expanding economy, current nobody
Machine launcher, merely provide a flat pad, it is impossible to adjust angle and measure the transmitting initial velocity of unmanned plane, it is right
In the launcher that the performance of test unmanned plane is inconvenient, current, heavier, the different direction of the launch needs to carry out launcher
It is mobile to place, substantial amounts of manpower is expended, therefore, it is necessary to further improve.
Utility model content
The technical problems to be solved in the utility model overcomes the defects of existing, there is provided a kind of unmanned aerial vehicle ejecting frame, by setting
Some launching seats and rotary shaft, can arbitrarily adjust the direction of the launch, by provided with lifting scale and pulling force scale, can
Adjust different angles and different launch velocity degree, by provided with snubber block, sliding block can be protected, by setting
The external rope having, sliding block can be made to be pulled by the operating of chain, pass through expelling plate and elevating lever, ram pot and hair
The position relationship penetrated between seat, overall stability can be ensured, by provided with universal wheel, launcher movement side can be made
Just, by provided with fixed column and fixing groove, can ensure launcher work when stability, by provided with ram pot
And elevating lever, can be easy to adjust, and stability is more preferably, the problem of can solve the problem that in background technology.
In order to solve the above-mentioned technical problem, the utility model provides following technical scheme：
A kind of unmanned aerial vehicle ejecting frame involved by the utility model, including pedestal and expelling plate, the expelling plate are placed in base
Seat top, the expelling plate left side are welded with contiguous block, and the contiguous block side is provided with connecting hole, rotation is provided with the top of the pedestal
Rotating shaft neck and fixing groove, the rotary shaft neck are placed on the inside of fixing groove, and rotary shaft is provided with the rotary shaft neck inner chamber,
Launching seat is connected with the top of the rotary shaft, the launching seat two bottom sides are arranged with fixed column, and the fixed column is respectively positioned on
In the fixing groove inner chamber, fixed mount and ram pot are provided with the top of the launching seat, the fixed mount is located on the left of ram pot, institute
State and elevating lever is provided with hydraulic pressure tube inner chamber, the elevating lever outer wall is provided with lifting scale, and connection is provided with the inside of the fixed mount
Axle, the expelling plate are connected in connecting shaft by connecting hole, and the expelling plate bottom right is provided with expansion link neck, the hair
Penetrate plate outer wall side and be provided with pulling force scale, be provided with chute at the top of the expelling plate, sliding block is connected with the chute inner chamber, it is described
Slider top is provided with unmanned plane bracket, is connected with pulling force piece on the right side of the sliding block, described pulling force piece one end is connected with spring, described
Spring one end is connected to chute inwall right-hand member, and the chute inwall left end is provided with snubber block, and the chute front is provided with aperture,
Motor is provided with rear side of the expelling plate inner chamber, the motor side is respectively connected with electric machine rotational axis, described electric machine rotational axis one end
Gear is respectively connected with, and chain is surrounded with two top circle weeks, external rope, the external string are connected with the chain
Rope passes through pinking and is connected to the sliding block side, and the base bottom is provided with connection leg, and the connection leg bottom is provided with universal wheel.
Furthermore, position relationship triangular in shape between the expelling plate and elevating lever, ram pot and launching seat.
Furthermore, the width of the launching seat is 500mm, and the width of the pedestal is 600mm.
Furthermore, the gap between the pedestal and launching seat is 100mm.
Furthermore, the minimum altitude of the elevating lever is 200mm, and the level altitude of the fixed mount is 200mm.
Furthermore, the angle of regulation range between the expelling plate and launching seat is 0 ° -45 °.
The utility model beneficial effect：A kind of unmanned aerial vehicle ejecting frame involved by the utility model, by provided with transmitting
Seat and rotary shaft, can arbitrarily adjust the direction of the launch, by provided with lifting scale and pulling force scale, difference can be adjusted
Angle and different launch velocity degree, by provided with snubber block, sliding block can be protected, by provided with it is external
Rope, sliding block can be made to be pulled by the operating of chain, by between expelling plate and elevating lever, ram pot and launching seat
Position relationship, overall stability can be ensured, by provided with universal wheel, launcher conveniently moving can be made, by setting
Some fixed column and fixing groove, can ensure launcher work when stability, by provided with ram pot and lifting
Bar, can be easy to adjust, and stability is more preferably.
Brief description of the drawings
Accompanying drawing is used for providing further understanding to of the present utility model, and a part for constitution instruction, with this practicality
New embodiment is used to explain the utility model together, does not form to limitation of the present utility model.
Fig. 1 is a kind of unmanned aerial vehicle ejecting frame front view of the utility model.
Fig. 2 is a kind of unmanned aerial vehicle ejecting frame Local map of the utility model.
Fig. 3 is a kind of unmanned aerial vehicle ejecting frame pedestal top view of the utility model.
Fig. 4 is a kind of unmanned aerial vehicle ejecting frame expelling plate Local map of the utility model.
Fig. 5 is a kind of unmanned aerial vehicle ejecting frame pedestal fixed mount profile of the utility model.
Label in figure：1st, unmanned plane bracket；2nd, fixed mount；3rd, launching seat；4th, fixed column；5th, pedestal；6th, connection leg；7th, ten thousand
To wheel；8th, rotary shaft；9th, ram pot；10th, elevating lever；11st, scale is lifted；12nd, pulling force scale；13rd, expelling plate；14th, expansion link
Neck；15th, chute；16th, sliding block；17th, pulling force piece；18th, external rope；19th, contiguous block；20th, connecting hole；21st, spring；22nd, it is small
Hole；23rd, snubber block；24th, fixing groove；25th, rotary shaft neck；26th, connecting shaft；27th, motor；28th, chain；29th, electric machine rotational axis；
30th, gear.
Embodiment
Preferred embodiment of the present utility model is illustrated below in conjunction with accompanying drawing, it will be appreciated that described herein excellent
Select embodiment to be merely to illustrate and explain the utility model, be not used to limit the utility model.
As Figure 1-Figure 5, a kind of unmanned aerial vehicle ejecting frame, including pedestal 5 and expelling plate 13, the expelling plate 13 are placed in base
The top of seat 5, the left side of expelling plate 13 are welded with contiguous block 19, and the side of contiguous block 19 is provided with connecting hole 20, the pedestal 5
Top is provided with rotary shaft neck 25 and fixing groove 24, and the rotary shaft neck 25 is placed in the inner side of fixing groove 24, the rotary shaft card
Rotary shaft 8 is provided with the inner chamber of groove 25, the top of rotary shaft 8 is connected with launching seat 3, and the two bottom sides of launching seat 3 are symmetrically set
There is fixed column 4, the fixed column 4 is respectively positioned in the inner chamber of fixing groove 24, and the top of launching seat 3 is provided with fixed mount 2 and liquid
Pressure cylinder 9, the fixed mount 2 are located at the left side of ram pot 9, are provided with elevating lever 10 in the inner chamber of ram pot 9, outside the elevating lever 10
Wall is provided with lifting scale 11, and the inner side of fixed mount 2 is provided with connecting shaft 26, and the expelling plate 13 is connected to by connecting hole 20
In connecting shaft 26, the bottom right of expelling plate 13 is provided with expansion link neck 14, and the outer wall side of expelling plate 13 is provided with pulling force
Scale 12, the top of expelling plate 13 are provided with chute 15, and sliding block 16, the top of sliding block 16 are connected with the inner chamber of chute 15
Provided with unmanned plane bracket 1, the right side of sliding block 16 is connected with pulling force piece 17, and described one end of pulling force piece 17 is connected with spring 21, institute
State the one end of spring 21 and be connected to the inwall right-hand member of chute 15, the inwall left end of chute 15 is provided with snubber block 23, and the chute 15 is just
Face is provided with aperture 22, and motor 27 is provided with rear side of the inner chamber of expelling plate 13, and the side of motor 27 is respectively connected with motor rotation
Axle 29, described one end of electric machine rotational axis 29 is respectively connected with gear 30, and is surrounded with chain 28 on two excircles of gear 30, described
External rope 18 is connected with chain 28, the external rope 18 is connected to the side of sliding block 16, the base through aperture 22
5 bottoms of seat are provided with connection leg 6, and the bottom of connection leg 6 is provided with universal wheel 7.
More specifically, position triangular in shape between the expelling plate 13 and elevating lever 10, ram pot 9 and launching seat 3
Relation, the stability of triangle is more firm, and the width of the launching seat 3 is 500mm, and the width of the pedestal 5 is 600mm,
It is easy to rotation to adjust, the gap between the pedestal 5 and launching seat 3 is 100mm, and rotation will not cause to collide, the elevating lever
10 minimum altitude is 200mm, and the level altitude of the fixed mount 2 is 200mm, and distance is equivalent, and expelling plate 13 can be parallel
Place, the angle of regulation range between the expelling plate 13 and launching seat 3 is 0 ° -45 °, and 45 ° of launch angle is maximum distance.
Utility model works principle：A kind of unmanned aerial vehicle ejecting frame is being carried out in use, working as needs to launch unmanned plane
When, unmanned plane is positioned on unmanned plane bracket 1, the direction of the launch is regulated by pedestal 5 and launching seat 3, then passed through
Ram pot 9 and elevating lever 10 regulate the angle of transmitting, observe scale, in order to adjust accuracy, pass through the work of motor 27
Make, starting for chain 28 can be driven, external rope 18 is driven, sliding block 16 is pulled by spring 21, and be fixed on needs
The position of transmitting, it can either launch, and can enough observes data, and the maximum functional distance of spring 21 is equal to the minimum of external rope 18
Operating distance, when need not use, launcher can be moved away by universal wheel 7, simply, safety is convenient, real
With stability is strong.
It is above the preferable embodiment of the utility model, the utility model those skilled in the art can also be to upper
State embodiment to be changed and changed, therefore, the utility model is not limited to above-mentioned embodiment, every ability
Any conspicuously improved, replacement or modification that field technique personnel are made on the basis of the utility model belong to this practicality
New protection domain.
Claims (6)
1. a kind of unmanned aerial vehicle ejecting frame, including pedestal (5) and expelling plate (13), the expelling plate (13) are placed in above pedestal (5),
Characterized in that, being welded with contiguous block (19) on the left of the expelling plate (13), contiguous block (19) side is provided with connecting hole
(20) rotary shaft neck (25) and fixing groove (24), are provided with the top of the pedestal (5), the rotary shaft neck (25) is placed in fixation
On the inside of groove (24), rotary shaft (8) is provided with rotary shaft neck (25) inner chamber, transmitting is connected with the top of the rotary shaft (8)
Seat (3), launching seat (3) two bottom sides are arranged with fixed column (4), and the fixed column (4) is respectively positioned on the fixing groove
(24) in inner chamber, fixed mount (2) and ram pot (9) are provided with the top of the launching seat (3), the fixed mount (2) is located at ram pot
(9) on the left of, elevating lever (10) is provided with ram pot (9) inner chamber, elevating lever (10) outer wall is provided with lifting scale
(11) connecting shaft (26), is provided with the inside of the fixed mount (2), the expelling plate (13) is connected to connecting shaft by connecting hole (20)
(26) on, expelling plate (13) bottom right is provided with expansion link neck (14), and expelling plate (13) the outer wall side, which is provided with, draws
Power scale (12), expelling plate (13) top are provided with chute (15), sliding block (16), institute are connected with chute (15) inner chamber
State and unmanned plane bracket (1) is provided with the top of sliding block (16), pulling force piece (17), the pulling force piece are connected with the right side of the sliding block (16)
(17) one end is connected with spring (21), and described spring (21) one end is connected to chute (15) inwall right-hand member, and the chute (15) is interior
Wall left end is provided with snubber block (23), and chute (15) front is provided with aperture (22), set on rear side of expelling plate (13) inner chamber
There is motor (27), motor (27) side is respectively connected with electric machine rotational axis (29), and described electric machine rotational axis (29) one end connects
Gear (30) is connected to, and chain (28) is surrounded with two gear (30) excircles, external string is connected with the chain (28)
Rope (18), the external rope (18) are connected to the sliding block (16) side through aperture (22), and pedestal (5) bottom is provided with
Connection leg (6), connection leg (6) bottom are provided with universal wheel (7).
2. a kind of unmanned aerial vehicle ejecting frame according to claim 1, it is characterised in that the expelling plate (13) and elevating lever
(10), position relationship triangular in shape between ram pot (9) and launching seat (3).
3. a kind of unmanned aerial vehicle ejecting frame according to claim 1, it is characterised in that the width of the launching seat (3) is
500mm, the width of the pedestal (5) is 600mm.
4. a kind of unmanned aerial vehicle ejecting frame according to claim 1, it is characterised in that between the pedestal (5) and launching seat (3)
Gap be 100mm.
5. a kind of unmanned aerial vehicle ejecting frame according to claim 1, it is characterised in that the minimum altitude of the elevating lever (10) is
200mm, and the level altitude of the fixed mount (2) is 200mm.
6. a kind of unmanned aerial vehicle ejecting frame according to claim 1, it is characterised in that the expelling plate (13) and launching seat (3)
Between angle of regulation range be 0 ° -45 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721037620.8U CN207045777U (en) | 2017-08-18 | 2017-08-18 | A kind of unmanned aerial vehicle ejecting frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721037620.8U CN207045777U (en) | 2017-08-18 | 2017-08-18 | A kind of unmanned aerial vehicle ejecting frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207045777U true CN207045777U (en) | 2018-02-27 |
Family
ID=61503118
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721037620.8U Active CN207045777U (en) | 2017-08-18 | 2017-08-18 | A kind of unmanned aerial vehicle ejecting frame |
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| Country | Link |
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| CN (1) | CN207045777U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109048841A (en) * | 2018-09-10 | 2018-12-21 | 广东宏穗晶科技服务有限公司 | A kind of dangerous situation robot |
| CN109502043A (en) * | 2018-09-30 | 2019-03-22 | 沈阳戈达德智能装备科技有限公司 | A kind of long-range Quality Initiative driven motor ejector system of small drone |
| CN109896038A (en) * | 2019-03-22 | 2019-06-18 | 燕山大学 | Unmanned aerial vehicle ejecting system |
| CN114132522A (en) * | 2021-12-07 | 2022-03-04 | 黄杰 | Unmanned aerial vehicle and catapult thereof |
-
2017
- 2017-08-18 CN CN201721037620.8U patent/CN207045777U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109048841A (en) * | 2018-09-10 | 2018-12-21 | 广东宏穗晶科技服务有限公司 | A kind of dangerous situation robot |
| CN109502043A (en) * | 2018-09-30 | 2019-03-22 | 沈阳戈达德智能装备科技有限公司 | A kind of long-range Quality Initiative driven motor ejector system of small drone |
| CN109502043B (en) * | 2018-09-30 | 2023-08-08 | 沈阳戈达德智能装备科技有限公司 | Small unmanned aerial vehicle remote control chain transmission electric catapult system |
| CN109896038A (en) * | 2019-03-22 | 2019-06-18 | 燕山大学 | Unmanned aerial vehicle ejecting system |
| CN109896038B (en) * | 2019-03-22 | 2022-02-11 | 燕山大学 | Unmanned aerial vehicle ejection system |
| CN114132522A (en) * | 2021-12-07 | 2022-03-04 | 黄杰 | Unmanned aerial vehicle and catapult thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20181218 Address after: 050000 east door of No. 8 factory building of Ludao V Valley Industrial Park, 181 Shibainan Avenue, Luquan District, Shijiazhuang City, Hebei Province Patentee after: HEBEI XIANGTUO AVIATION TECHNOLOGY CO., LTD. Address before: 050000 east door of No. 8 factory building of Ludao V Valley Industrial Park, 181 Shibainan Avenue, Luquan District, Shijiazhuang City, Hebei Province Patentee before: Yu Adan |
|
| TR01 | Transfer of patent right |