CN208828111U - A kind of unmanned plane air attack bullet throwing device - Google Patents
A kind of unmanned plane air attack bullet throwing device Download PDFInfo
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- CN208828111U CN208828111U CN201821524097.6U CN201821524097U CN208828111U CN 208828111 U CN208828111 U CN 208828111U CN 201821524097 U CN201821524097 U CN 201821524097U CN 208828111 U CN208828111 U CN 208828111U
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- control mechanism
- unmanned plane
- throwing device
- connecting rod
- hanger
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Abstract
The utility model discloses a kind of unmanned plane air attack bullet throwing devices, comprising: carry plate, for carrying entire throwing device and being connect by carry plate with unmanned body；Attachment lug is connected on carry plate；Hanger is connected on attachment lug, and two hangers, which are oppositely arranged, constitutes the space that can be placed for spherical dry chemical projectile；Lock link, one end are connected on hanger, and the other end is connected on control mechanism；Control mechanism is connected on carry plate, and control mechanism includes swing connecting bar, series connection connecting rod support and the series connection connecting rod being connected on series connection connecting rod support；Servo-controller is connected on control mechanism, and the swing connecting bar, series connection connecting rod on Servo-controller control control mechanism move horizontally, and that realizes control mechanism opens or closes state.Can simultaneously carry three most common dry spherical powder fire extinguisher bombs；Can individually be jettisoninged fire extinguisher bomb in three times；By wireless signal far distance control saving casting device steering engine mechanism, carries out fire extinguisher bomb and automatic toss.
Description
Technical field
The utility model relates to air vehicle technique fields, and in particular to a kind of unmanned plane air attack bullet throwing device.
Background technique
Attention of the forest fire prevention and control emergency increasingly by country, when fire either discovery potential risk fire source occurs
It waits, most of fireman carries out fire extinguisher bomb in such a way that hand is thrown and jettisonings.Such fire extinguisher bomb is jettisoninged, low precision, fireman people
Body does not ensure safely.With the development of unmanned air vehicle technique, the mating dedicated load equipment of unmanned plane is widely used in forest and disappears
Anti- field, fireman can jettisoning by unmanned plane carry fire extinguisher bomb from the air.
Currently, domestic unmanned plane fire extinguisher bomb is jettisoninged, equipment and technology is also immature, is also unable to reach following requirement at present: 1,
Dry spherical powder fire extinguisher bomb is accurately jettisoninged to fire source；2, it individually jettisonings in batches；3, it automatics toss in the air；4, it precisely throws
It throws；5, light-weight, carry can be carried out by small-sized multi-rotor unmanned aerial vehicle；6, there are enough intensity, rigidity, be mounted on unmanned plane
The problems such as will not vibrating, do not influence aircraft security.
Utility model content
The utility model scheme combination forest fire prevention and control application demand, for the deficiency of current air attack bullet casting technique,
Unmanned plane air attack bullet throwing device is provided, is solved: 1, the most common dry spherical powder fire extinguisher bomb of jettisonable；It 2, can be in batches
It is secondary individually to jettisoning；3, it is automaticed toss by wireless signal far distance control；4, by unmanned plane GPS positioning system, can accomplish li
Meter level is not jettisoninged precisely；5, light-weight, it can be mounted in most of back yard industry grade multi-rotor unmanned aerial vehicles and use extensively；6, structure
Intensity, rigidity are big, and vibration problem will not be occurred by being mounted on unmanned plane in flight course, will not influence the flight peace of unmanned plane
Entirely.
In order to achieve the above purposes, the technical solution adopted by the utility model is:
A kind of unmanned plane air attack bullet throwing device, the throwing device include:
Carry plate, the carry plate are used to carry entire throwing device and are connect by carry plate with unmanned body；
Attachment lug, the attachment lug are connected on carry plate；
Hanger, the hanger are connected on attachment lug, and two hangers are oppositely arranged composition one can be for spherical dry powder
The space that fire extinguisher bomb is placed；
Lock link, described lock link one end are connected on hanger, and the lock link other end is connected on control mechanism；
Control mechanism, the control mechanism are connected on carry plate, and the control mechanism includes swing connecting bar, series connection connecting rod
Support and the series connection connecting rod being connected on series connection connecting rod support, described series connection connecting rod one end, which is sequentially connected, extends to control mechanism
The lock link connected in connecting rod support, the other end are connect with swing connecting bar；
Servo-controller, the Servo-controller are connected on control mechanism, the pendulum on the Servo-controller control control mechanism
Dynamic connecting rod, series connection connecting rod move horizontally, and that realizes control mechanism opens or closes state.
It is further improved as the utility model, the attachment lug is in T-shaped structure comprising integral structure setting
Weft element and vertical body, wherein vertical body in the middle part of offer notch.
It is further improved as the utility model, the hanger is in "U" shaped structure comprising the cross of integral structure setting
To section and vertical section, the vertical section on the hanger is extended in the vertical body notch on the attachment lug, and passes through an axis
Shape part is connected integrally；Traversing section and vertical section on the hanger offer the arc-shaped limit portion inwardly concaved, and two
The corresponding setting of a hanger and constitute one by the arc-shaped limit portion on traversing section and vertical section can be for spherical dry-chemical fire extinguishing
The space that bullet is placed.
It is further improved as the utility model, the arc-shaped connecting rod of lock link, lock link one end connection
Vertical section on hanger, the lock link other end are connected to the series connection connecting rod on control mechanism.
It is further improved as the utility model, the unmanned plane air attack bullet throwing device includes three groups of control machines
Structure, each group of control mechanism connect one group of Servo-controller, and each group of control mechanism controls two lock link operating statuses.
It is further improved as the utility model, the unmanned plane air attack bullet throwing device includes six groups of U-shaped hangers.
It is further improved as the utility model, there are two attachment lugs for connection on each hanger.
It is further improved as the utility model, the control mechanism, hanger, lock link are by aluminum alloy materials system
At.
It is further improved as the utility model, the carry plate is made of carbon fibre material.
The utility model unmanned plane air attack bullet throwing device, concrete operations principle are
Servo-controller receives by flying the pwm signal that control is given and controls the on and off of control mechanism；Control mechanism
After receiving the control command transmitted by Servo-controller, swing connecting bar is driven to operate；Connect connecting rod swing connecting bar drive under also with
With being operated；The lock link being connected on series connection connecting rod, also follows under the drive also by series connection connecting rod and is operated；Lock
Determine connecting rod to be in an open state from lock state transformation, and then hanger is also to open state, effect of the dry chemical projectile in gravity
It vertically jettisonings down.
The utility model the utility model has the advantages that
1, can simultaneously carry three most common dry spherical powder fire extinguisher bombs；
2, can individually jettisoning fire extinguisher bomb in three times；
3, it by wireless signal far distance control saving casting device steering engine mechanism, carries out fire extinguisher bomb and automatics toss；
4, by unmanned plane GPS positioning system, it can accomplish that a centimetre rank is precisely jettisoninged；
5, light-weight, it can be mounted in most of back yard industry grade multi-rotor unmanned aerial vehicles and use extensively；
6, structural strength, rigidity are big, and vibration problem will not be occurred by being mounted on unmanned plane in flight course, ensure unmanned plane
Flight safety.
For the structure feature and effect for more clearly illustrating the utility model, come with reference to the accompanying drawing with specific embodiment pair
It is described in detail.
Detailed description of the invention
Fig. 1 show one of the utility model unmanned plane air attack bullet throwing device structural schematic diagram；
Fig. 2 show the utility model unmanned plane air attack bullet throwing device second structural representation.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Refering to attached drawing 1 to 2.The present embodiment provides a kind of unmanned plane air attack bullet throwing device, which includes:
Carry plate 1, the carry plate 1 are used to carry entire throwing device and are connect by carry plate 1 with unmanned body；
Attachment lug 2, the attachment lug 2 are connected on carry plate 1；Attachment lug 2 is in T-shaped structure comprising
The weft element 2.1 and vertical body 2.2 of integral structure setting, wherein offering notch 2.3 in the middle part of vertical body 2.2；
Hanger 5, the hanger 5 are connected on attachment lug 2, and two hangers 5 are oppositely arranged composition one can be for spherical
The space that dry chemical projectile 6 is placed；The hanger 5 is in "U" shaped structure comprising 5.1 He of traversing section of integral structure setting
Vertical section 5.2, the vertical section 5.2 on the hanger 5 extend in 2.2 notch 2.3 of vertical body on the attachment lug 2, and
It is connected integrally by an axis shape part；Traversing section 5.1 and vertical section 5.2 on the hanger 5 are offered and are inwardly concaved
Arc-shaped limit portion 5.3, the corresponding setting of two hangers 5 and pass through the arc-shaped limit portion on traversing section 5.1 and vertical section 5.2
5.3 constitute the space that can be placed for spherical dry chemical projectile 6；
Lock link 7, described 7 one end of lock link are connected on hanger 5, and 7 other end of lock link is connected to control machine
On structure 3；The arc-shaped connecting rod of lock link 7, described 7 one end of lock link are connected to the vertical section 5.2 on hanger 5, the locking
7 other end of connecting rod is connected to the series connection connecting rod 3.3 on control mechanism 3；
Control mechanism 3, the control mechanism 3 are connected on carry plate 1, the control mechanism 3 include swing connecting bar 3.1,
Series connection connecting rod support 3.2 and be connected to series connection connecting rod support 3.2 on series connection connecting rod 3.3, described 3.3 one end of series connection connecting rod according to
Secondary connection extends to the lock link 7 that control mechanism 3 is connected in connecting rod support 3.2, and the other end is connect with swing connecting bar 3.1；
Servo-controller 4, the Servo-controller 4 are connected on control mechanism 3, and Servo-controller 4 controls the pendulum on control mechanism 3
Dynamic connecting rod 3.1, series connection connecting rod 3.3 move horizontally, and that realizes control mechanism 3 opens or closes state.
The present embodiment unmanned plane air attack bullet throwing device includes three groups of control mechanisms 3, and each group of control mechanism 3 connects
One group of Servo-controller 4, each group of control mechanism 3 control two 7 operating statuses of lock link.
The present embodiment unmanned plane air attack bullet throwing device includes six groups of U-shaped hangers 5, is connected with two on each hanger 5
A attachment lug 2.
Control mechanism, hanger, lock link on the present embodiment unmanned plane air attack bullet throwing device is by aluminium alloy
Material is made.Carry plate 1 is made of carbon fibre material.
The present embodiment unmanned plane air attack bullet throwing device, concrete operations principle are
Servo-controller 4 receives by flying the pwm signal that control is given and controls the on and off of control mechanism 3；Control machine
After structure receives the control command transmitted by Servo-controller 4, swing connecting bar 3.1 is driven to operate；Connecting rod 3.3 connect in swing connecting bar
It also follows and is operated under 3.1 drives；The lock link 7 being connected on series connection connecting rod 3.3, also by the band of series connection connecting rod 3.3
It also follows and is operated under dynamic；Lock link 7 is in an open state from lock state transformation, and then hanger 5 is also to open state,
Dry chemical projectile 6 is vertically jettisoninged under gravity.
This unmanned plane air attack bullet throwing device the utility model has the advantages that
1, can simultaneously carry three most common dry spherical powder fire extinguisher bombs；
2, can individually jettisoning fire extinguisher bomb in three times；
3, it by wireless signal far distance control saving casting device steering engine mechanism, carries out fire extinguisher bomb and automatics toss；
4, by unmanned plane GPS positioning system, it can accomplish that a centimetre rank is precisely jettisoninged；
5, light-weight, it can be mounted in most of back yard industry grade multi-rotor unmanned aerial vehicles and use extensively；
6, structural strength, rigidity are big, and vibration problem will not be occurred by being mounted on unmanned plane in flight course, ensure unmanned plane
Flight safety.
The above descriptions are merely preferred embodiments of the present invention, not makees in any form to the utility model
Limitation.Anyone skilled in the art, it is all available in the case where not departing from technical solutions of the utility model ambit
The methods and technical content of the disclosure above makes many possible changes and modifications to technical solutions of the utility model, or is revised as
The equivalent embodiment of equivalent variations.Therefore all contents without departing from technical solutions of the utility model, the shape according to the utility model
Equivalence changes made by shape, construction and principle should all be covered by the protection scope of the utility model.
Claims (9)
1. a kind of unmanned plane air attack bullet throwing device, which is characterized in that the throwing device includes:
Carry plate, the carry plate are used to carry entire throwing device and are connect by carry plate with unmanned body；
Attachment lug, the attachment lug are connected on carry plate；
Hanger, the hanger are connected on attachment lug, and two hangers are oppositely arranged composition one can be for spherical dry-chemical fire extinguishing
The space that bullet is placed；
Lock link, described lock link one end are connected on hanger, and the lock link other end is connected on control mechanism；
Control mechanism, the control mechanism are connected on carry plate, and the control mechanism includes swing connecting bar, series connection connecting rod support
And it is connected to the series connection connecting rod on series connection connecting rod support, described series connection connecting rod one end, which is sequentially connected, extends to control mechanism series connection
Lock link in connecting rod support, the other end are connect with swing connecting bar；
Servo-controller, the Servo-controller are connected on control mechanism, and the swing on the Servo-controller control control mechanism connects
Bar, series connection connecting rod move horizontally, and that realizes control mechanism opens or closes state.
2. unmanned plane air attack bullet throwing device according to claim 1, which is characterized in that the attachment lug is in
T-shaped structure comprising the weft element and vertical body of integral structure setting, wherein offering notch in the middle part of vertical body.
3. unmanned plane air attack bullet throwing device according to claim 2, which is characterized in that the hanger is in " U " word
Shape structure comprising the traversing section and vertical section of integral structure setting, the vertical section on the hanger extend to the engaging lug
In the vertical body notch of on piece, and connected integrally by an axis shape part；Traversing section and vertical section on the hanger is equal
The arc-shaped limit portion inwardly concaved is offered, two hangers are corresponding to be arranged and by the arc limit on traversing section and vertical section
Position portion constitutes the space that can be placed for spherical dry chemical projectile.
4. unmanned plane air attack bullet throwing device according to claim 3, which is characterized in that the lock link is in arc
Shape connecting rod, described lock link one end are connected to the vertical section on hanger, and the lock link other end is connected to control mechanism
On series connection connecting rod.
5. unmanned plane air attack bullet throwing device according to claim 1, which is characterized in that the unmanned plane goes out in the air
It includes three groups of control mechanisms that fire, which plays throwing device, and each group of control mechanism connects one group of Servo-controller, each group of control mechanism control
Make two lock link operating statuses.
6. unmanned plane air attack bullet throwing device according to claim 1, which is characterized in that the unmanned plane goes out in the air
It includes six groups of U-shaped hangers that fire, which plays throwing device,.
7. unmanned plane air attack bullet throwing device according to claim 1, which is characterized in that connected on each hanger
There are two attachment lugs.
8. unmanned plane air attack bullet throwing device according to claim 1, which is characterized in that the control mechanism, extension
Frame, lock link are made of aluminum alloy materials.
9. unmanned plane air attack bullet throwing device according to claim 1, which is characterized in that the carry plate is by carbon fiber
Dimension material is made.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821524097.6U CN208828111U (en) | 2018-09-18 | 2018-09-18 | A kind of unmanned plane air attack bullet throwing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821524097.6U CN208828111U (en) | 2018-09-18 | 2018-09-18 | A kind of unmanned plane air attack bullet throwing device |
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| Publication Number | Publication Date |
|---|---|
| CN208828111U true CN208828111U (en) | 2019-05-07 |
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ID=66313658
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821524097.6U Active CN208828111U (en) | 2018-09-18 | 2018-09-18 | A kind of unmanned plane air attack bullet throwing device |
Country Status (1)
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| CN (1) | CN208828111U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945466A (en) * | 2018-09-18 | 2018-12-07 | 翼航东升东莞航空实业集团有限公司 | Unmanned aerial vehicle aerial fire extinguishing bomb throwing device and method |
| CN110239715A (en) * | 2019-06-11 | 2019-09-17 | 深圳市科比特航空科技有限公司 | A kind of throwing device and unmanned plane |
-
2018
- 2018-09-18 CN CN201821524097.6U patent/CN208828111U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945466A (en) * | 2018-09-18 | 2018-12-07 | 翼航东升东莞航空实业集团有限公司 | Unmanned aerial vehicle aerial fire extinguishing bomb throwing device and method |
| CN110239715A (en) * | 2019-06-11 | 2019-09-17 | 深圳市科比特航空科技有限公司 | A kind of throwing device and unmanned plane |
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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: 20220525 Address after: 510700 room 810, room 406, No. 1, Yichuang street, Huangpu District, Guangzhou City, Guangdong Province (Zhongxin Guangzhou Knowledge City) Patentee after: Yihang Ruiying Aviation Technology (Guangdong) Co.,Ltd. Address before: 523000 4th Floor, 65 Wanghong Road, Xia Cao Village, Wangniudun Town, Dongguan City, Guangdong Province Patentee before: YIHANG DONGSHENG DONGGUAN AVIATION INDUSTRY GROUP CO.,LTD. |
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| TR01 | Transfer of patent right |