CN206841724U - A kind of unmanned plane with parachute assembly - Google Patents
A kind of unmanned plane with parachute assembly Download PDFInfo
- Publication number
- CN206841724U CN206841724U CN201720671080.2U CN201720671080U CN206841724U CN 206841724 U CN206841724 U CN 206841724U CN 201720671080 U CN201720671080 U CN 201720671080U CN 206841724 U CN206841724 U CN 206841724U
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- CN
- China
- Prior art keywords
- parachute
- parachute assembly
- support
- umbrella
- unmanned plane
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Abstract
The utility model discloses a kind of unmanned plane with parachute assembly,Including unmanned body,Parachute assembly,Buzzer siren,Main control chip,Parachute,Umbrella frame,Gas generator,Support,Rotating shaft,Fixed spiral cover,Blade,Support frame,Umbrella storehouse,The parachute assembly of the present utility model is arranged at the top center of unmanned body,Buzzer siren is provided with by the parachute assembly,The main control chip is embedded in unmanned internal body,The external structure of the parachute assembly is umbrella storehouse,The San Cang bottom centre is fixedly connected with support,Gas generator is fixedly mounted at the carriage center,Support frame as described above is fixedly mounted on support through gas generator,A rotating device is respectively installed in end at the 4 of support frame as described above,The top colligation of the umbrella frame is in the edge of parachute,The end of the umbrella frame is fixed on support,The utility model prevents unmanned plane is out of control in flight from falling,The situation of fuselage damage occurs.
Description
Technical field
It the utility model is related to UAV technical field, more particularly to a kind of nobody with parachute assembly
Machine.
Background technology
UAV is to utilize radio remote-controlled telemetry equipment and the presetting apparatus provided for oneself referred to as " unmanned plane "
The not manned aircraft manipulated.Without driving cabin on machine, but be provided with navigation and flight control, presetting apparatus and power and
The equipment such as power supply.Ground remote control telemetry station personnel are tracked to it, positioned, being remotely controlled, remote measurement sum by equipment such as Data-Links
Word transmits.Compared with manned aircraft, it has small volume, low cost, spy easy to use, adapting to a variety of flight environment of vehicle requirements
Point, therefore can be widely used in air remote sensing, meteorological research, agriculture plant seeds by airplane and the prevention and control of plant diseases, pest control, particularly in war more
There is special advantage, can be widely used for aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc..
In the modern life, aeromodelling airplane obtains the understanding of more and more people and liked, various aeromodelling airplanes emerge in an endless stream.But
It is due to a variety of causes of technology or unmanned plane in itself, it is out of control awing to still suffer from unmanned plane, can not normal flight landing
Situation, cause a series of troubles, fuselage falls damage, therefore the setting of the parachute assembly of aeromodelling airplane is very necessary.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane with parachute assembly, to solve above-mentioned background technology
The problem of middle proposition.
To realize the utility model purpose, the technical scheme of use is：A kind of unmanned plane with parachute assembly, including
Unmanned body, parachute assembly, buzzer siren, main control chip, parachute, umbrella frame, gas generator, support, dividing plate, electricity
Machine, parachute assembly controller, rotating shaft, fixed spiral cover, blade, support frame, umbrella storehouse, described the utility model fill with parachute
The parachute assembly for the unmanned plane put is arranged at the top center of unmanned body, and buzzing is provided with by the parachute assembly and is alarmed
Device, the main control chip are embedded in unmanned internal body, and the external structure of the parachute assembly is umbrella storehouse, and the umbrella storehouse is
Cylinder, the San Cang bottom centre are fixedly connected with support, and the main body of the support is a circular plate face, bottom by
Three bars are centered on the center of circle of circular slab, radial support, and the frame bottom is fixedly connected with a dividing plate, in the dividing plate
Motor and parachute assembly controller are placed, gas generator is fixedly mounted at the carriage center, support frame as described above is in " ten "
Font, the center of support frame is hollow, and inflated diameter is identical with gas generator body diameter, fixes and pacifies through gas generator
On support, support frame as described above 4 at each one rotating device of installation in end, the rotating device include rotating shaft, fixed spiral cover,
Blade, intercalation two panels blade on the fixed spiral cover, the blade by fixed spiral cover rotational fastener in rotating shaft, the umbrella frame
For folding stand, the top colligation of the umbrella frame is fixed on support in the edge of parachute, the end of the umbrella frame, the drop
The material for falling umbrella is canvas, the hexagon for being shaped as sticking out that the parachute struts.
Preferably, the gas generator is connected with parachute assembly controller input.
Preferably, the gas generator is connected with parachute assembly controller output end.
Preferably, the motor connects with the input of parachute assembly controller.
Preferably, the motor connects with the output end of parachute assembly controller
Preferably, the input of the rotating shaft and motor connects.
Preferably, the output end of the rotating shaft and motor connects.
Compared with prior art, the beneficial effects of the utility model are：
1st, the utility model parachute assembly and unmanned plane body are relatively independent, detachably, are easy to the maintenance of parachute assembly
The progress of maintenance work.
2nd, the utility model solves parachute and quickly goes out umbrella storehouse by the setting of folding umbrella rib, and umbrella rope is easily wound, from
And the problem of making parachute not open, improve parachute assembly can practicality.
3rd, on the utility model unmanned plane buzzer siren setting, buzzer siren will be started when parachute flicks,
Sound is sent, facilitates user to find, design is humanized.
4th, the utility model is made parachute when going out umbrella storehouse, is opened rotating device, passed through by the setting of rotating device
Wind-force plays a part of balance and stability parachute body, unmanned plane is landed more steady, the infringement being subject to is reduced to smaller.
Brief description of the drawings
Fig. 1 is a kind of structural representation of the unmanned plane with parachute assembly of the utility model；
Fig. 2 is a kind of parachute assembly structural representation of the unmanned plane with parachute assembly of the utility model；
Fig. 3 is a kind of parachute assembly top view of the unmanned plane with parachute assembly of the utility model.
In figure：1st, unmanned body；2nd, parachute assembly；3rd, buzzer siren；4th, main control chip；201st, parachute；202、
Umbrella frame；203rd, gas generator；204th, support；205th, dividing plate；206th, motor；207th, parachute assembly controller；208th, rotating shaft；
209th, fixed spiral cover；210th, blade；211st, support frame；212nd, umbrella storehouse.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Refer to shown in Fig. 1-3, the utility model provides a kind of technical scheme：A kind of nobody with parachute assembly
Machine, including unmanned body 1, parachute assembly 2, buzzer siren 3, main control chip 4, parachute 201, umbrella frame 202, gas occur
Device 203, support 204, dividing plate 205, motor 206, parachute assembly controller 207, rotating shaft 208, fixed spiral cover 209, blade
210th, support frame 211, umbrella storehouse 212, the parachute assembly 2 of unmanned plane of the described the utility model with parachute assembly are arranged on
At the top center of unmanned body 1, buzzer siren 3 is provided with by the parachute assembly, the main control chip 4 is embedded in unmanned plane
Inside body 1, the external structure of the parachute assembly is umbrella storehouse 212, and the umbrella storehouse 212 is cylinder, the bottom of umbrella storehouse 212
Center is fixedly connected with support 204, and the main body of the support 204 is a circular plate face, and bottom is by three bars with the center of circle of circular slab
Centered on, radial support, the bottom of support 204 is fixedly connected with a dividing plate 205, and motor 206 is placed in the dividing plate 205
With parachute assembly controller 207, gas generator 203 is fixedly mounted at the center of support 204, support frame as described above 211 is in
" ten " font, the center of support frame 211 is hollow, and inflated diameter is identical with the body diameter of gas generator 203, is sent out through gas
Raw device 203 is fixedly mounted on support, support frame as described above 211 4 at each one rotating device of installation in end, the rotating device bag
Include rotating shaft 208, fix spiral cover 209, blade 210, intercalation two panels blade 210 on the fixed spiral cover 209, the blade 210 leads to
The fixed rotational fastener of spiral cover 209 is crossed in rotating shaft 208, the umbrella frame 202 is folding stand, and the top colligation of the umbrella frame 202 exists
The edge of parachute 201, the end of the umbrella frame 202 are fixed on support, and the material of the parachute 201 is canvas, institute
State the hexagon for being shaped as sticking out that parachute 201 struts.
Operation principle：When unmanned plane not manipulated person's remote control out of control, when will falling, main control chip 4 is opened
Forced landing pattern, umbrella storehouse 212 are opened, and power source of the gas generator 203 as the parachute-opening of parachute 201, are filled by parachute
Put controller 207 to control, produce a large amount of gases, folding umbrella rib 202 deploys, and parachute 201 is gone out umbrella by gases at high pressure
Storehouse 212, while rotating device is rotated by blade 210, is played a part of balance and stability parachute 201, is delayed unmanned plane
It is slow to fall, and buzzer siren 3 will be started when parachute 201 flicks, facilitate manipulator to find unmanned plane.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out with a variety of changes in the case where not departing from principle of the present utility model and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (7)
1. a kind of unmanned plane with parachute assembly, including unmanned body (1), parachute assembly (2), buzzer siren (3),
Main control chip (4), parachute (201), umbrella frame (202), gas generator (203), support (204), dividing plate (205), motor
(206), parachute assembly controller (207), rotating shaft (208), fixed spiral cover (209), blade (210), support frame (211), umbrella
Storehouse (212), the parachute assembly are arranged at the top center of unmanned body (1), and buzzing is provided with by the parachute assembly
Alarm (3), the embedded unmanned body (1) of the main control chip (4) is internal, and the external structure of the parachute assembly is umbrella storehouse
(212), the umbrella storehouse (212) is cylinder, and umbrella storehouse (212) bottom centre is fixedly connected with support (204), the support
(204) main body is a circular plate face, bottom by three bars centered on the center of circle of circular slab, radial support, the branch
Frame (204) bottom is fixedly connected with a dividing plate (205), and motor (206) and parachute assembly controller are placed in the dividing plate (205)
(207) gas generator (203), is fixedly mounted at support (204) center, support frame as described above (211) is in " ten " font, branch
The center of support (211) is hollow, and inflated diameter is identical with gas generator (203) body diameter, through gas generator
(203) be fixedly mounted on support, support frame as described above (211) 4 at end respectively installation one rotating device, the rotating device bag
Include rotating shaft (208), fix spiral cover (209), blade (210), intercalation two panels blade (210) on the fixed spiral cover (209) is described
Blade (210) is by fixed spiral cover (209) rotational fastener in rotating shaft (208), and the umbrella frame (202) is folding stand, the umbrella
The top colligation of bone (202) is fixed on support in the edge of parachute (201), the end of the umbrella frame (202), the drop
The material for falling umbrella (201) is canvas, the hexagon for being shaped as sticking out that the parachute (201) struts.
A kind of 2. unmanned plane with parachute assembly according to claim 1, it is characterised in that the motor (206)
Connected with parachute assembly controller (207) input.
A kind of 3. unmanned plane with parachute assembly according to claim 1, it is characterised in that the motor (206)
Connected with parachute assembly controller (207) output end.
A kind of 4. unmanned plane with parachute assembly according to claim 1, it is characterised in that the gas generator
(203) it is connected with parachute assembly controller (207) input.
A kind of 5. unmanned plane with parachute assembly according to claim 1, it is characterised in that the gas generator
(203) it is connected with parachute assembly controller (207) output end.
A kind of 6. unmanned plane with parachute assembly according to claim 1, it is characterised in that the rotating shaft (208)
It is connected with motor (206) input.
A kind of 7. unmanned plane with parachute assembly according to claim 1, it is characterised in that the rotating shaft (208)
It is connected with motor (206) output end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720671080.2U CN206841724U (en) | 2017-06-12 | 2017-06-12 | A kind of unmanned plane with parachute assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720671080.2U CN206841724U (en) | 2017-06-12 | 2017-06-12 | A kind of unmanned plane with parachute assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206841724U true CN206841724U (en) | 2018-01-05 |
Family
ID=60799562
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720671080.2U Expired - Fee Related CN206841724U (en) | 2017-06-12 | 2017-06-12 | A kind of unmanned plane with parachute assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206841724U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109911224A (en) * | 2019-03-26 | 2019-06-21 | 郭永宣 | A kind of dropout prevents the unmanned plane protection mechanism of crash |
| CN110979655A (en) * | 2019-11-21 | 2020-04-10 | 东莞理工学院 | Mechanical bird with anti-collision buffer structure |
-
2017
- 2017-06-12 CN CN201720671080.2U patent/CN206841724U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109911224A (en) * | 2019-03-26 | 2019-06-21 | 郭永宣 | A kind of dropout prevents the unmanned plane protection mechanism of crash |
| CN109911224B (en) * | 2019-03-26 | 2022-08-26 | 山东经纬润林发展集团有限公司 | Unmanned aerial vehicle protection mechanism for preventing signal loss and crash |
| CN110979655A (en) * | 2019-11-21 | 2020-04-10 | 东莞理工学院 | Mechanical bird with anti-collision buffer structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180105 Termination date: 20190612 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |