CN207580177U - A kind of unmanned plane with buffer gear - Google Patents
A kind of unmanned plane with buffer gear Download PDFInfo
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- CN207580177U CN207580177U CN201721347376.5U CN201721347376U CN207580177U CN 207580177 U CN207580177 U CN 207580177U CN 201721347376 U CN201721347376 U CN 201721347376U CN 207580177 U CN207580177 U CN 207580177U
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- unmanned plane
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- buffer gear
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- 230000003139 buffering effect Effects 0.000 claims abstract description 12
- 238000003466 welding Methods 0.000 claims description 4
- 239000002775 capsule Substances 0.000 claims 1
- 230000001133 acceleration Effects 0.000 abstract description 4
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 3
- 230000000712 assembly Effects 0.000 description 3
- 238000000429 assembly Methods 0.000 description 3
- 238000012806 monitoring device Methods 0.000 description 3
- 239000002131 composite material Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 229910001095 light aluminium alloy Inorganic materials 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000002860 competitive effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008676 import Effects 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 230000019491 signal transduction Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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Abstract
The utility model discloses a kind of unmanned planes with buffer gear,Its structure includes flight fin,High-speed brushless motor,Supporting rod,Motor rack,Unmanned plane function rack,Accumulator,Unmanned plane covers rack,Functional connector,The assisting in flying wing,Geodesic distance sensor,Transceiving antennas,Braced wing,Airbag buffer,Flight fin is connected with the upper end of high-speed brushless motor,A kind of unmanned plane with buffer gear of the utility model,Structure is equipped with airbag buffer,The lower end of airbag buffer and functional connector is nested,Geodesic distance sensor detects the increase of acceleration over the ground when unmanned plane needs forced landing,Signal is imported to the outer plate of airbag buffer after control board processing,Air bag start expansion until unmanned plane is landed by air bag into row buffering,There is no need to parachutes for unmanned plane buffering in this way,Simultaneously parachute it is possible that the special circumstances that can not be opened just are not present,Unmanned plane buffering would not be damaged in time.
Description
Technical field
The utility model is a kind of unmanned plane with buffer gear, belongs to field.
Background technology
At present, unmanned plane is widely used in civilian, commercial and military field, in civil field, more and more limit fortune
Dynamic fan is shot with video-corder using unmanned plane, in commercial kitchen area, is navigated except picture pick-up device is carried to every competitive sports into line trace
Other than bat, and logistic industry is had been enter into, cargo can be sent to manpower and dispense more difficult, slower remote districts, therefore, unmanned plane
The range that has a wide range of applications and vast market prospect.
Prior art discloses application No. is a kind of 201620034718.7 unmanned plane, be included in throwing to fly to monitor under pattern
The data of the unmanned plane dish out monitoring device and judge the unmanned plane whether dish out and according to judging result control institute
The flight control assemblies of unmanned plane during flying pattern are stated, the monitoring device of dishing out is electrically connected with the flight control assemblies, in institute
It states unmanned plane and opens the state thrown and fly pattern, the data monitored are sent to the flight and controlled by the monitoring device of dishing out
Device, the flight control assemblies control the unmanned plane to enter from steady pattern after judging that the unmanned plane is spilled over, still
When the situation for needing to force-land occurs in unmanned plane during flying in the prior art, often landed into row buffering with parachute
, which there is situation, in umbrella normally to be opened, and cause unmanned plane landing damage.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of unmanned plane with buffer gear, with
When solving existing technology and occurring the situation for needing to force-land in unmanned plane during flying, it is into row buffering with parachute, often occurs
, which there is situation, in parachute normally to be opened, and unmanned plane is caused to land damage problem.
To achieve these goals, the utility model is to realize by the following technical solutions：A kind of band buffer gear
Unmanned plane, structure include flight fin, high-speed brushless motor, supporting rod, motor rack, unmanned plane function rack, accumulator,
Unmanned plane covers rack, functional connector, the assisting in flying wing, geodesic distance sensor, transceiving antennas, braced wing, air bag
Buffer, the flight fin are connected with the upper end of high-speed brushless motor, the upper table of the high-speed brushless motor and motor rack
Face fits, and the mutually welding of the supporting rod and motor rack, the functional connector is connected with the lower end of unmanned plane function rack
It connects, the upper end of the braced wing and functional connector is nested, the assisting in flying wing and the lower end phase of unmanned plane function rack
Connection, the geodesic distance sensor cover rack with unmanned plane and are connected, the braced wing and the lower end of unmanned plane function rack
It mutually welds, the lower end of the airbag buffer and functional connector is nested, and the airbag buffer includes outer plate, pressure release
The upper surface of mouth, air bag, clip plate, air inlet, support plate, connection ring, the outer plate and clip plate fits, the pressure release
Mouth is connected with the upper end of clip plate, and the lower surface of the air bag and clip plate fits, and the clip plate and air inlet are mutually embedding
Set, the air inlet is connected with the upper end of air bag, and the upper end of the air inlet and outer plate is nested, the support plate with into
Gas port mutually welds, and the connection ring is connected with support plate, and the connection ring is connected with the lower end of functional connector.
Further, the lower end of the unmanned plane function rack and unmanned plane covering rack is nested.
Further, the accumulator is connected with the lower end of unmanned plane function rack.
Further, the unmanned plane covers rack and is nested with supporting rod.
Further, the motor rack is trigone important actor engraved structure.
Further, the supporting rod is made of light aluminum alloy.
Further, the unmanned plane covers rack and is made of light composite material.
Advantageous effect
A kind of unmanned plane with buffer gear of the utility model, structure are equipped with airbag buffer, airbag buffer and work(
Can the lower end of connector be nested, geodesic distance sensor detects the increase of acceleration over the ground when unmanned plane needs forced landing, in
The outer plate that signal is imported to airbag buffer after plate is handled is controlled, air bag starts expansion to be carried out until unmanned plane is landed by air bag
Buffering, such unmanned plane buffering there is no need to parachute, while parachute it is possible that the special circumstances that can not be opened just
It is not present, unmanned plane buffering would not be damaged in time.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structure diagram of the unmanned plane with buffer gear of the utility model；
Fig. 2 is the structure diagram of the utility model buffer gear.
In figure：Flight fin -1, supporting rod -3, motor rack -4, unmanned plane function rack -5, stores high-speed brushless motor -2
Battery -6, unmanned plane cover rack -7, functional connector -8, the assisting in flying wing -9, geodesic distance sensor -10, transceiving
Antenna -11, braced wing -12, airbag buffer -13, outer plate -1301, pressure relief opening -1302, air bag -1303, clip plate -
1304th, air inlet -1305, support plate -1306, connection ring -1307.
Specific embodiment
To be easy to understand technical means, creative features, achievable purpose and effectiveness of the utility model, below
With reference to specific embodiment, the utility model is expanded on further.
It please refers to Fig.1, Fig. 2, the utility model provides a kind of technical solution of the unmanned plane with buffer gear：Its structure packet
Flight fin 1, high-speed brushless motor 2, supporting rod 3, motor rack 4, unmanned plane function rack 5, accumulator 6, unmanned plane is included to cover
Rack 7, functional connector 8, the assisting in flying wing 9, geodesic distance sensor 10, transceiving antennas 11, braced wing 12, air bag delay
Device 13 is rushed, the flight fin 1 is connected with the upper end of high-speed brushless motor 2, the high-speed brushless motor 2 and motor rack 4
Upper surface fits, the mutually welding of the supporting rod 3 and motor rack 4, the functional connector 8 and unmanned plane function rack 5
Lower end is connected, and the upper end of the braced wing 12 and functional connector 8 is nested, the assisting in flying wing 9 and unmanned plane function
The lower end of rack 5 is connected, and the geodesic distance sensor 10 covers rack 7 with unmanned plane and is connected, the braced wing 12 and nothing
The lower end of Study on Man-Machine Function rack 5 is mutually welded, and the lower end of the airbag buffer 13 and functional connector 8 is nested, the air bag
Buffer 13 include outer plate 1301, pressure relief opening 1302, air bag 1303, clip plate 1304, air inlet 1305, support plate 1306,
Connection ring 1307, the upper surface of the outer plate 1301 and clip plate 1304 fit, the pressure relief opening 1302 and clip plate
1304 upper end is connected, and the lower surface of the air bag 1303 and clip plate 1304 fits, the clip plate 1304 and air inlet
Mouth 1305 is nested, and the air inlet 1305 is connected with the upper end of air bag 1303, the air inlet 1305 and outer plate 1301
Upper end be nested, the support plate 1306 and 1305 phase of air inlet are welded, and the connection ring 1307 is connected with support plate 1306
It connects, the connection ring 1307 is connected with the lower end of functional connector 8, and the unmanned plane function rack 5 covers machine with unmanned plane
The lower end of frame 7 is nested, and the accumulator 6 is connected with the lower end of unmanned plane function rack 5, and the unmanned plane covers rack 7
It is nested with supporting rod 3, the motor rack 4 is trigone important actor engraved structure, and the supporting rod 3 is made of light aluminum alloy, institute
Unmanned plane covering rack 7 is stated to be made of light composite material.
Flight fin 1 described in this patent is that propeller refers to rotate in air or water by blade, by engine rotation
Power is converted into the device of propulsive force, can there are two or more leaf be connected with hub, leaf backward one side be helicoid or approximation
In a kind of propeller of helicoid, the high-speed brushless motor 2 is that brshless DC motor is made of motor body and driver,
It is a kind of typical electromechanical integrated product, brushless direct current motor is run with autocontrol.
Detect that acceleration is abnormal over the ground by geodesic distance sensor 10 when being used, by signal transduction to control board,
The signal of control board processing simultaneously sends it to connection ring 1307, then signal is passed to outer plate by support plate 1306
1301, outer plate 1301 is connected to signal triggering clip plate 1304, while air inlet 1305 starts air-breathing, and air bag 1303 starts to expand
When the air pressure in air bag 1303 stops suction to air inlet 1305 when limiting threshold values, pressure relief opening 1302 will collide when being collided until contacting to earth
Kinetic energy pressure release go out to make unmanned plane safe falling.
The utility model solve the prior art occur in unmanned plane during flying need force-land situation when, be to use parachute
Into row buffering, the problem of parachute often occur and situation occur normally opening, causing unmanned plane landing damage, this practicality is newly
Type is combined with each other by above-mentioned component, and structure is equipped with airbag buffer, the lower end phase of airbag buffer and functional connector
Nesting, geodesic distance sensor detects the increase of acceleration over the ground when unmanned plane needs forced landing, by signal after control board processing
Import the outer plate of airbag buffer, air bag start expansion until unmanned plane is landed by air bag into row buffering, such unmanned plane
Buffering there is no need to parachute, while parachute it is possible that the special circumstances that can not be opened just are not present, unmanned plane delays
Punching would not damage in time, described in detail below:
The airbag buffer 13 includes outer plate 1301, pressure relief opening 1302, air bag 1303, clip plate 1304, air inlet
1305th, support plate 1306, connection ring 1307, the upper surface of the outer plate 1301 and clip plate 1304 fit, the pressure release
Mouth 1302 is connected with the upper end of clip plate 1304, and the lower surface of the air bag 1303 and clip plate 1304 fits, described interior
Pressing plate 1304 is nested with air inlet 1305, and the air inlet 1305 is connected with the upper end of air bag 1303, the air inlet
1305 are nested with the upper end of outer plate 1301, the support plate 1306 and the mutually welding of air inlet 1305, the connection ring
1307 are connected with support plate 1306, and the connection ring 1307 is connected with the lower end of functional connector 8.
The basic principle of the utility model and main feature and the advantages of the utility model has been shown and described above, for
For those skilled in the art, it is clear that the utility model is not limited to the details of above-mentioned exemplary embodiment, and without departing substantially from this
In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent requirements of the claims
All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in each embodiment can also be properly combined, forms those skilled in the art
The other embodiment being appreciated that.
Claims (5)
1. a kind of unmanned plane with buffer gear, it is characterised in that：Its structure includes flight fin (1), high-speed brushless motor
(2), supporting rod (3), motor rack (4), unmanned plane function rack (5), accumulator (6), unmanned plane cover rack (7), function connects
Connect device (8), the assisting in flying wing (9), geodesic distance sensor (10), transceiving antennas (11), braced wing (12), air bag buffering
Device (13), the flight fin (1) are connected with the upper end of high-speed brushless motor (2), the high-speed brushless motor (2) and motor
The upper surface of frame (4) fits, the supporting rod (3) and the mutually welding of motor rack (4), the functional connector (8) and nobody
The lower end of machine function rack (5) is connected, and the braced wing (12) and the upper end of functional connector (8) are nested, the auxiliary
Flying wing (9) is connected with the lower end of unmanned plane function rack (5), and the geodesic distance sensor (10) covers rack with unmanned plane
(7) be connected, the braced wing (12) and the lower end of unmanned plane function rack (5) are mutually welded, the airbag buffer (13) with
The lower end of functional connector (8) is nested, and the airbag buffer (13) includes outer plate (1301), pressure relief opening (1302), gas
Capsule (1303), clip plate (1304), air inlet (1305), support plate (1306), connection ring (1307), the outer plate (1301)
It fits with the upper surface of clip plate (1304), the pressure relief opening (1302) is connected with the upper end of clip plate (1304), described
Air bag (1303) and the lower surface of clip plate (1304) fit, and the clip plate (1304) is nested with air inlet (1305),
The air inlet (1305) is connected with the upper end of air bag (1303), the air inlet (1305) and the upper end of outer plate (1301)
It is nested, the support plate (1306) is mutually welded with air inlet (1305), the connection ring (1307) and support plate (1306) phase
Connection, the connection ring (1307) are connected with the lower end of functional connector (8).
2. a kind of unmanned plane with buffer gear according to claim 1, it is characterised in that：The unmanned plane function rack
(5) lower end that rack (7) is covered with unmanned plane is nested.
3. a kind of unmanned plane with buffer gear according to claim 1, it is characterised in that：The accumulator (6) and nothing
The lower end of Study on Man-Machine Function rack (5) is connected.
4. a kind of unmanned plane with buffer gear according to claim 1, it is characterised in that：The unmanned plane covers rack
(7) it is nested with supporting rod (3).
5. a kind of unmanned plane with buffer gear according to claim 1, it is characterised in that：The motor rack (4) is three
Terrace with edge column engraved structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721347376.5U CN207580177U (en) | 2017-10-19 | 2017-10-19 | A kind of unmanned plane with buffer gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721347376.5U CN207580177U (en) | 2017-10-19 | 2017-10-19 | A kind of unmanned plane with buffer gear |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207580177U true CN207580177U (en) | 2018-07-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721347376.5U Active CN207580177U (en) | 2017-10-19 | 2017-10-19 | A kind of unmanned plane with buffer gear |
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| Country | Link |
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| CN (1) | CN207580177U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109353493A (en) * | 2018-09-28 | 2019-02-19 | 许剑聪 | A kind of self-rescue device of drowning unmanned plane equipped with gas generation buoyancy |
| CN109573026A (en) * | 2018-11-13 | 2019-04-05 | 浙江云来集科技有限公司 | Unmanned plane is used in a kind of detection of unmanned aerial photography |
| CN110001932A (en) * | 2019-04-06 | 2019-07-12 | 胡永星 | It is a kind of to be prevented from falling the unmanned plane of taking photo by plane of damage based on aerodynamic decelerator |
| CN111056027A (en) * | 2019-12-28 | 2020-04-24 | 河南省科宇信息技术有限公司 | High-endurance anti-collision monitoring inspection unmanned aerial vehicle |
| CN113022865A (en) * | 2021-04-16 | 2021-06-25 | 商丘师范学院 | Unmanned aerial vehicle is used in survey and drawing |
-
2017
- 2017-10-19 CN CN201721347376.5U patent/CN207580177U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109353493A (en) * | 2018-09-28 | 2019-02-19 | 许剑聪 | A kind of self-rescue device of drowning unmanned plane equipped with gas generation buoyancy |
| CN109573026A (en) * | 2018-11-13 | 2019-04-05 | 浙江云来集科技有限公司 | Unmanned plane is used in a kind of detection of unmanned aerial photography |
| CN109573026B (en) * | 2018-11-13 | 2024-04-19 | 浙江云来集科技有限公司 | Unmanned aerial vehicle for unmanned aerial vehicle aerial photography detection |
| CN110001932A (en) * | 2019-04-06 | 2019-07-12 | 胡永星 | It is a kind of to be prevented from falling the unmanned plane of taking photo by plane of damage based on aerodynamic decelerator |
| CN111056027A (en) * | 2019-12-28 | 2020-04-24 | 河南省科宇信息技术有限公司 | High-endurance anti-collision monitoring inspection unmanned aerial vehicle |
| CN113022865A (en) * | 2021-04-16 | 2021-06-25 | 商丘师范学院 | Unmanned aerial vehicle is used in survey and drawing |
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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: 20190529 Address after: 435400 No. 2 Beichuan Road, Wuxue City, Huanggang City, Hubei Province Patentee after: HUBEI YUCHAI ENGINE CO.,LTD. Address before: Room 1501, Ruojingwan, Hengxing, Dongmen Industrial Zone, Fengzhou Town, Nanan City, Quanzhou City, Fujian Province Patentee before: QUANZHOU CAIQI TRADE Co.,Ltd. |
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| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240122 Address after: 435499 No. 2, North Side, West End of Beichuan Road, Wuxue City, Huanggang City, Hubei Province Patentee after: Hubei Yufa Feifang Agricultural Technology Co.,Ltd. Country or region after: China Address before: 435400 No. 2 Beichuan Road, Wuxue City, Huanggang City, Hubei Province Patentee before: HUBEI YUCHAI ENGINE CO.,LTD. Country or region before: China |
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| TR01 | Transfer of patent right |