CN207274985U - There is the unmanned plane that ejection is jettisoninged - Google Patents
There is the unmanned plane that ejection is jettisoninged Download PDFInfo
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- CN207274985U CN207274985U CN201721018522.XU CN201721018522U CN207274985U CN 207274985 U CN207274985 U CN 207274985U CN 201721018522 U CN201721018522 U CN 201721018522U CN 207274985 U CN207274985 U CN 207274985U
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Abstract
Unmanned plane field is the utility model is related to, discloses a kind of unmanned plane that there is ejection and jettisoning, it includes main body, load platform and ejection throwing device, the load platform and is arranged on the lower end of main body；Launched throwing device includes housing, rocket body, steering engine, trigger, spring, pull rod and connecting seat, rocket body is arranged on the front end of housing, and rocket body is equipped with hook, spring is arranged in housing and positioned at the rear of rocket body, pull rod is arranged on spring, and the propulsion end of pull rod is equipped with the pressure head for being used for compressing spring；One end of trigger is equipped with buckling parts, and the other end of trigger is connected on the pivoted arm of the steering engine, and during spring-compressed, spring is stated in buckling parts residence；Connecting seat is connected to the top of housing, and the upper end of connecting seat is connected to load platform.The utility model is connected to load platform by launching throwing device by connecting seat, unmanned plane is had the function of that ejection is jettisoninged, it is possible to achieve launches goods and materials at a distance, operating process convenient quickly is efficient.
Description
Technical field
Unmanned plane is the utility model is related to, more particularly to a kind of unmanned plane that there is ejection and jettisoning.
Background technology
Nowadays unmanned plane is applied to the multiple fields in life, bring great convenience for the life and work of people, very
To the operating type for changing the poorly efficient high labor cost of tradition, new solution is started and has used scheme.For example disappear in public security
, can be attached to rescuing by unmanned plane during flying when rescue personnel, which can not arrive at, a little to be participated in rescue in anti-, emergency management and rescue
Near overhead, is launched relief goods to rescue destination by unmanned plane.When unmanned plane can not be near destination, just
Need from remote relief goods of jettisoninging, and to realize this purpose, just require unmanned plane to have the function of to jettisoning at a distance, but mesh
Preceding that the unmanned plane jettisoninged at a distance can be achieved is complicated, it is impossible to relief goods easily and fast are sent to appointed place, are dropped
Low rescue efficiency.
Utility model content
The purpose of this utility model is to provide a kind of simple in structure, has the function of the unmanned plane that ejection is jettisoninged, to realize soon
Speed easily launches goods and materials at a distance.
To achieve these goals, the utility model provides a kind of unmanned plane for having the function of ejection and jettisoninging, it includes master
Body, load platform and ejection throwing device, the load platform are arranged on the lower end of the main body；The ejection throwing device includes
Housing, rocket body, steering engine, trigger, spring, pull rod and connecting seat, the rocket body are arranged on the front end of the housing, and the rocket body
Hook is equipped with, the spring is arranged in the housing and is arranged in the spring positioned at the rear of the rocket body, the pull rod
On, and the propulsion end of the pull rod is equipped with the pressure head for being used for compressing the spring；One end of the trigger is equipped with buckling parts, institute
The other end for stating trigger is connected on the pivoted arm of the steering engine, and during the spring-compressed, spring is stated in the buckling parts snapping residence；
The connecting seat is connected to the top of the housing, and the upper end of the connecting seat is connected to the load platform.
Preferably, the rear end of the rocket body is equipped with shock absorber part.
Preferably, the shock absorber part is rubber cushion.
Preferably, it is additionally provided with the lateral wall of the housing around line piece.
Preferably, the pull rod is equipped with handle.
Preferably, the ejection throwing device further includes position adjustment block, the position adjustment block connection
In on the housing and between the housing and the connecting seat.
Preferably, the connecting seat includes the first connecting plate, linking arm and the second connecting plate, first connection
Plate is connected to the upper end of the position adjustment block, and the lower end of the linking arm is connected to the upper end of first connecting plate, institute
State the upper end that the second connecting plate is connected to the linking arm.
Preferably, the linking arm is copper post, and the quantity of the copper post is 4.
The unmanned plane provided by the utility model for having the function of ejection and jettisoninging, it is flat that ejection throwing device is connected to load
Platform, the rocket body of the device are equipped with hook, can be with carry goods and materials, and spring is arranged in housing and is worn positioned at the rear of rocket body, pull rod
On spring and the propulsion end of pull rod is equipped with pressure head, and pressure head can compress spring to form the elastic potential energy of strength, trigger
One end be equipped with buckling parts, in spring-compressed, buckling parts can snapping live spring and enable spring to store substantial amounts of elasticity
Potential energy, the other end of trigger are connected on the pivoted arm of steering engine, and the pivoted arm of steering engine, which rotates, moves trigger so that buckling parts departs from bullet
Spring, elastic force release pushing drawing rod hit rocket body, the goods and materials that rocket body is carried on hook is flown to destination, so that unmanned plane
Have the function of that ejection is jettisoninged, it is possible to achieve launch goods and materials at a distance, operating process convenient quickly is efficient.
Brief description of the drawings
Fig. 1 is that the utility model embodiment has the function of the structure diagram for the unmanned plane that ejection is jettisoninged；
Fig. 2 is the structure diagram of the ejection throwing device of the utility model embodiment；
Fig. 3 is the internal structure schematic diagram of the ejection throwing device of the utility model embodiment.
Wherein, 1, main body；2nd, load platform；3rd, throwing device is launched；31st, housing；311st, around line piece；32nd, rocket body；321、
Hook；322nd, shock absorber part；33rd, steering engine；34th, trigger；341st, buckling parts；35th, spring；36th, pull rod；361st, pressure head；362nd, handle；
37th, connecting seat；371st, the first connecting plate；372nd, linking arm；373rd, the second connecting plate；38th, position adjustment block.
Embodiment
With reference to the accompanying drawings and examples, specific embodiment of the present utility model is described in further detail.Below
Embodiment is used to illustrate the utility model, but is not intended to limit the scope of the present invention.
As shown in Figure 1-Figure 3, the unmanned plane for having the function of ejection and jettisoninging of the preferred embodiment in the utility model, it includes master
Body 1, load platform 2 and ejection throwing device 3, load platform 2 are arranged on the lower end of main body 1, and ejection throwing device 3 includes housing
31st, rocket body 32, steering engine 33, trigger 34, spring 35, pull rod 36 and connecting seat 37, rocket body 32 are arranged on the front end of housing 31, and arrow
For body 32 equipped with hook 321, hook 321 can be used for carry goods and materials, and spring 35 is arranged in housing 31 and is located at the rear of rocket body 32,
Pull rod 36 is arranged on spring 35, and the propulsion end of pull rod 36 is equipped with the pressure head 361 for being used for compressing spring 35, and pressure head 361 is pressed
Contracting spring 35 makes the elastic potential energy of the formation strength of spring 35；One end of trigger 34 is equipped with buckling parts 341, when spring 35 compresses,
Buckling parts 341 can snapping live spring 35 and enable spring 35 to store substantial amounts of elastic potential energy, the other end connection of trigger 34
To the pivoted arm of steering engine 33, the pivoted arm of steering engine 33, which rotates, moves trigger 34 so that and buckling parts 341 departs from spring 35, so that, bullet
The elastic force release of spring 35 makes 35 pushing drawing rod 36 of spring hit rocket body 32, flies the goods and materials that rocket body 32 is carried on hook 321
To destination；Connecting seat 37 is connected to the top of housing 31, and the upper end of connecting seat 37 is connected to load platform 2 so that ejection
Throwing device 3 can be connected to load platform 2, so that unmanned plane can realize remote dispensing goods and materials, operating process is convenient
Quickly, it is efficient.
When impacting rocket body 32 due to pull rod 36, vibrations may be produced so that rocket body 32 deviates predetermined heading, be
Such case is avoided, is equipped with shock absorber part 322 in the rear end of rocket body 32, it is preferred that shock absorber part 322 is rubber cushion.
It is additionally provided with around line piece 311, can be located at traction rope etc. is rich in line piece 311 on the lateral wall of housing 31, in use,
One end of traction rope is bundled on the hook 321 of rocket body 32, so that it may traction rope is transported to destination by rocket body 32, specifically
, the shape around line piece 311 is cylinder.
In order to make pull rod 36 compress spring 35 to form elastic potential energy, when in use, it is necessary to which artificial pulling pull rod 36, is
Facilitate operation, in the rear end of pull rod 36 be equipped with handle 362, so that people grip pull rod 36.
Ejection throwing device 3 further includes position adjustment block 38, and position adjustment block 38 is connected on housing 31 and is located at
, can be with the position of adjustment housings 31, so that 32 energy of rocket body by position adjustment block 38 between housing 31 and connecting seat 37
Destination is enough aimed at, specifically, position adjustment block 38 includes electronic controlled height adjustment and angular adjustment module, it is preferred that angle
Adjustment module includes gear assembly and connecting rod, and one end of connecting rod is connected on housing 31, and the other end connection of connecting rod
To the output shaft of gear assembly, rotate connecting rod by gear operation, so as to drive the angle of housing 31 to change；Highly
Adjustment module is leading screw and nut mechanism, and leading screw and nut mechanism is connected on housing 31, in use, housing 31 can be along screw direction
Move up and down, so that the height of adjustment housings 31.
In order to enable connecting seat 37 to facilitate what is consolidated to be connected on load platform 2, connecting seat 37 includes the first connecting plate
371st, 372 and second connecting plate 373 of linking arm, the first connecting plate 371 are connected to the upper end of position adjustment block 38, linking arm
372 lower end is connected to the upper end of the first connecting plate 371, and the second connecting plate 373 is connected to the upper end of linking arm 372, and second connects
Fishplate bar 373 be equipped with 2 matched connecting hole of load platform, can be connected by the second connecting plate 373 flat to load
On platform 2, so that ejection throwing device 3 is installed on unmanned plane so that unmanned plane has the function of that ejection is jettisoninged, and can realize remote
Distance throws goods and materials, it is preferred that linking arm 372 is copper post, and the quantity of copper post is 4 so that stable connection and can bear compared with
Big power.
To sum up, the unmanned plane provided by the utility model for having the function of ejection and jettisoninging, ejection throwing device pass through connection
Seat is connected to load platform, and the rocket body of the device is equipped with hook, can be arranged on carry goods and materials, spring in housing and be located at rocket body
Rear, pull rod is arranged on spring and the propulsion end of pull rod is equipped with pressure head, and pressure head can compress spring to form strength
Elastic potential energy, one end of trigger is equipped with buckling parts, in spring-compressed, buckling parts can snapping live spring spring stored up
Substantial amounts of elastic potential energy is deposited, the other end of trigger is connected on the pivoted arm of steering engine, and the pivoted arm of steering engine, which rotates, moves trigger so that
Buckling parts departs from spring, and elastic force release pushing drawing rod hits rocket body, the goods and materials that rocket body is carried on hook is flown to destination,
So that unmanned plane has the function of that ejection is jettisoninged, it is possible to achieve launches goods and materials at a distance, operating process convenient quickly is efficient.
The above is only the preferred embodiment of the utility model, it is noted that for the common skill of the art
For art personnel, on the premise of the utility model technical principle is not departed from, some improvement and replacement can also be made, these change
The scope of protection of the utility model is also should be regarded as into replacement.
Claims (8)
1. a kind of have the function of the unmanned plane jettisoninged of ejection, it is characterised in that it includes main body, load platform and ejection and jettisonings dress
Put, the load platform is arranged on the lower end of the main body；
The ejection throwing device includes housing, rocket body, steering engine, trigger, spring, pull rod and connecting seat, and the rocket body is arranged on institute
The front end of housing is stated, and the rocket body is equipped with hook, the spring is arranged in the housing and after the rocket body
Side, the pull rod are arranged on the spring, and the propulsion end of the pull rod is equipped with the pressure head for being used for compressing the spring；Institute
The one end for stating trigger is equipped with buckling parts, and the other end of the trigger is connected on the pivoted arm of the steering engine, during the spring-compressed,
State spring in the buckling parts snapping residence；The connecting seat is connected to the top of the housing, and the upper end of the connecting seat connects
It is connected to the load platform.
2. the unmanned plane as claimed in claim 1 that there is ejection and jettisoning, it is characterised in that the rear end of the rocket body is equipped with
Shock absorber part.
3. the unmanned plane as claimed in claim 2 that there is ejection and jettisoning, it is characterised in that the shock absorber part is rubber cushion.
4. the unmanned plane as claimed in claim 1 that there is ejection and jettisoning, it is characterised in that on the lateral wall of the housing
It is additionally provided with around line piece.
5. the unmanned plane as claimed in claim 1 that there is ejection and jettisoning, it is characterised in that the pull rod is equipped with handle
Hand.
6. the unmanned plane as claimed in claim 1 that there is ejection and jettisoning, it is characterised in that the ejection throwing device is also
Including position adjustment block, the position adjustment block be connected on the housing and positioned at the housing and the connecting seat it
Between.
7. the unmanned plane as claimed in claim 6 that there is ejection and jettisoning, it is characterised in that the connecting seat includes first
Connecting plate, linking arm and the second connecting plate, first connecting plate are connected to the upper end of the position adjustment block, the connection
The lower end of arm is connected to the upper end of first connecting plate, and second connecting plate is connected to the upper end of the linking arm.
8. the unmanned plane as claimed in claim 7 that there is ejection and jettisoning, it is characterised in that the linking arm is copper post,
The quantity of the copper post is 4.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721018522.XU CN207274985U (en) | 2017-08-14 | 2017-08-14 | There is the unmanned plane that ejection is jettisoninged |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721018522.XU CN207274985U (en) | 2017-08-14 | 2017-08-14 | There is the unmanned plane that ejection is jettisoninged |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207274985U true CN207274985U (en) | 2018-04-27 |
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ID=61984069
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721018522.XU Active CN207274985U (en) | 2017-08-14 | 2017-08-14 | There is the unmanned plane that ejection is jettisoninged |
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| CN (1) | CN207274985U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945462A (en) * | 2018-06-11 | 2018-12-07 | 易瓦特科技股份公司 | Power load-bearing emitter for unmanned plane |
| CN109334981A (en) * | 2018-11-22 | 2019-02-15 | 东北大学秦皇岛分校 | A kind of unmanned plane equipped with fire extinguishing bullet launching device |
| CN109649657A (en) * | 2019-01-29 | 2019-04-19 | 华北电力大学（保定） | A kind of fixed point delivery device for launching small goods and materials with unmanned plane cooperation |
| CN110697067A (en) * | 2019-10-21 | 2020-01-17 | 深圳市科比特航空科技有限公司 | Unmanned aerial vehicle transverse projection device |
| CN112810817A (en) * | 2021-02-19 | 2021-05-18 | 广西一号农服航空科技有限公司 | Aerial goods hook formula unmanned aerial vehicle of jettisoninging |
| CN113665815A (en) * | 2021-08-16 | 2021-11-19 | 航天时代飞鹏有限公司 | Unmanned aerial delivery device |
-
2017
- 2017-08-14 CN CN201721018522.XU patent/CN207274985U/en active Active
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945462A (en) * | 2018-06-11 | 2018-12-07 | 易瓦特科技股份公司 | Power load-bearing emitter for unmanned plane |
| CN108945462B (en) * | 2018-06-11 | 2021-05-28 | 易瓦特科技股份公司 | A power bearing emitter for unmanned aerial vehicle |
| CN109334981A (en) * | 2018-11-22 | 2019-02-15 | 东北大学秦皇岛分校 | A kind of unmanned plane equipped with fire extinguishing bullet launching device |
| CN109334981B (en) * | 2018-11-22 | 2023-09-05 | 东北大学秦皇岛分校 | Unmanned aerial vehicle carrying fire extinguishing bomb launching device |
| CN109649657A (en) * | 2019-01-29 | 2019-04-19 | 华北电力大学（保定） | A kind of fixed point delivery device for launching small goods and materials with unmanned plane cooperation |
| CN109649657B (en) * | 2019-01-29 | 2023-12-29 | 华北电力大学（保定） | Fixed point delivery device for delivering small materials in cooperation with unmanned aerial vehicle |
| CN110697067A (en) * | 2019-10-21 | 2020-01-17 | 深圳市科比特航空科技有限公司 | Unmanned aerial vehicle transverse projection device |
| CN110697067B (en) * | 2019-10-21 | 2024-02-20 | 深圳市科比特航空科技有限公司 | Unmanned aerial vehicle transverse projection device |
| CN112810817A (en) * | 2021-02-19 | 2021-05-18 | 广西一号农服航空科技有限公司 | Aerial goods hook formula unmanned aerial vehicle of jettisoninging |
| CN113665815A (en) * | 2021-08-16 | 2021-11-19 | 航天时代飞鹏有限公司 | Unmanned aerial delivery device |
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