CN205525009U - Low -latitude flying ware - Google Patents
Low -latitude flying ware Download PDFInfo
- Publication number
- CN205525009U CN205525009U CN201620107657.2U CN201620107657U CN205525009U CN 205525009 U CN205525009 U CN 205525009U CN 201620107657 U CN201620107657 U CN 201620107657U CN 205525009 U CN205525009 U CN 205525009U
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- Prior art keywords
- main stand
- aircraft
- low flyer
- seat
- axis aircraft
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Abstract
The utility model provides a low -latitude flying ware, it both can regard as unmanned vehicles to use, also can regard as the manned vehicle to use. This aircraft leading features is the large -scale or extra -large -size aircraft that is made up by a plurality of multiaxis aircraft to control by a controller is unified. Every multiaxis aircraft is independent unit, and itself can use by normal flight, assembles them respectively in the main part frame, and each other does not influence. The main part frame still is equipped with the one or more balancing pole for keep the steady of flight, in addition, safety umbrella is equipped with to main part frame top for the safety of keep balance and descending, the foot rest is equipped with to main part frame below for support the organism, and play the cushioning effect that descends and land. The utility model discloses an aircraft, the installation operation is simple and easy, can take off and land safely, and the smooth flight has better application prospect.
Description
Technical field
This utility model relates to aircraft, in particular it relates to low flyer.
Background technology
In recent years, along with graduallying relax control of domestic and international low latitude, the life people applied by increasing low flyer
In work, production.It is in traditional low flyer, excessive due to volume including dirigible, fire balloon, dalta wing etc.,
Affected by environment relatively big, therefore use unsuitable for ordinary circumstance.And existing fixed wing airplane, landing environment is subject to
Multiple condition limits, and airflight operation complexity, manipulation needs through strict training.Additionally, helicopter is main
For performing the low altitude flight of special duty, energy consumption is big, require the highest to flight environment of vehicle.By contrast, four axles or
Multiaxis rotor craft, has feature light and handy, flexible, that be easily manipulated, becomes the Hot spots for development of low flyer
One of.
As far back as 20 beginnings of the century, scientist begins to make the least Rotor Helicopter, but does not make a successful trial flight.
Later, people have made the four-axle aircraft that some are large-scale, unmanned plane or manned machine, and some also makes a successful trial flight,
The most aerial time of staying is the shortest, does not has actual application.Due to sensor, microcontroller etc. at that time development not
Maturation, four axles or Multi-axis aircraft do not grow up.Entering 21 century, microcontroller etc. has been achieved with bigger
Development, miniaturization, four axles of miniaturization or multiaxis unmanned vehicle are flourish, be widely used in taking photo by plane,
The fields such as scouting, the disaster relief, transport.
But due to the little load-carrying of its volume is light, and often there is the message of crash, limit their further application.
Carry more weight, more preferable four axles of security performance or Multi-axis aircraft to this end, develop, there is bigger real value
And application prospect.
Utility model content
For defect of the prior art, the purpose of this utility model is to provide a kind of low flyer.
A kind of low flyer provided according to this utility model, including main stand, multiple Multi-axis aircraft；
The plurality of Multi-axis aircraft is arranged on main stand；
Interval is all there is between any two Multi-axis aircraft.
Preferably, also include following any one or appoint multiple device:
-safe umbrella, described safe umbrella is connected on main stand；
-foot rest, described foot rest is located at the bottom of main stand, described foot rest be an overall structure, foldable structure or
Person's stretching structure；
-seat, described seat is arranged on main stand；
-attitude transducer, described attitude transducer is arranged on main stand；
-acceleration transducer, described acceleration transducer is arranged on main stand；
-electric connection line passage, described electric connection line passage extends in the inside of described main stand.
Preferably, also include following any one or appoint multiple device:
-the gimbal lever, the described gimbal lever is arranged on safe umbrella or on main stand；
-seat belt, described seat belt is connected on safe umbrella, or is connected between safe umbrella and main stand.
Preferably, symmetrical structure centered by described main stand, the plurality of Multi-axis aircraft is separately positioned on described
In the mounting bracket that main stand is unsettled, the plurality of Multi-axis aircraft is uniform or non-along the circumference of described main stand
Uniform setting.
Preferably, described main stand is X-shaped, cross, triangle, square, trapezoidal, circular or polygon
Shape.
Preferably, described Multi-axis aircraft includes power supply, motor, rotor, flight controller, induction apparatus；
Power supply is motor, flight controller, induction apparatus provide power supply；
Motor drives rotor；
Flight controller connects motor, induction apparatus.
Preferably, also include that ground traffic tools, described main stand are arranged on described ground traffic tools.
Preferably, the protective plate being arranged on described seat is also included；
Described protective plate extends to from the bottom of seat between space, surface and the Multi-axis aircraft of described seat；
Preferably, protective plate part between space, surface and the Multi-axis aircraft of described seat is arc,
And the nock of described arc is towards described seat；
Preferably, described arc is provided with hollow mesh structure or transparent material structure.
Preferably, controller is also included；Described controller is for carrying out Collaborative Control to the plurality of Multi-axis aircraft
Or the most individually control.
Preferably, under the control of described controller:
The attitude of the attitude transducer detection main stand being arranged on main stand, described controller is according to described appearance
The gimbal lever that state controls to be arranged on main stand rotates, and makes the attitude of main stand trend towards the balance preset
Attitude；
The acceleration of the acceleration transducer detection main stand being arranged on main stand, if described acceleration is hanging down
Nogata component upwards is more than or equal to acceleration of gravity, and the most described controller controls the safety being arranged on main stand
Umbrella is opened.
Compared with prior art, this utility model has a following beneficial effect:
1, possess installation operation landing simple, safe, the feature of smooth flight, both can make as unmanned vehicle
With, it is also possible to use as manned vehicle；
2, multiple Multi-axis aircrafts can independent assortment, be independent of each other, if one of them damage, other can make as usual
With；
3, equipped with a safe umbrella on main stand, similar umbrella can be opened with automatic or manual, for awing
Keep balance or shield in landing and emergency, special parachute can be used as required；
4, by one or more gimbal levers, it is assembled on main stand, is used for keeping balance；
5, by one or more foot rests, it is assembled on main stand, has been used for supporting and the cushioning effect of landing；
This foot rest can stretch or fold, it is simple to uses；
6, remote controller can be utilized to carry out remote control, this remote controller controls all of miniature small-sized or large-scale flight
Device unit and safe umbrella, the gimbal lever, thus manipulate whole aircraft, remote controller can use 2.4G frequency, also
Can be used for controlling aircraft by installation software on mobile phone；
7, can be with the combination of the ground traffic tools such as bicycle, it is achieved multipurpose is flown.
Accompanying drawing explanation
By the detailed description non-limiting example made with reference to the following drawings of reading, of the present utility model other
Feature, purpose and advantage will become more apparent upon:
The one unmanned low flyer overall structure schematic diagram that Fig. 1 provides for this utility model；
The one manned low flyer overall structure schematic diagram that Fig. 2 provides for this utility model；
A kind of combination type weight carrier low flyer overall structure schematic diagram that Fig. 3 provides for this utility model；
In figure:
1, safe umbrella；
2, the gimbal lever；
3, main stand；
4, controller；
5, Multi-axis aircraft；
6, foot rest；
7, seat；
8, seat belt；
9, the vehicles.
Detailed description of the invention
Below in conjunction with specific embodiment, this utility model is described in detail.Following example will assist in the skill of this area
Art personnel are further appreciated by this utility model, but limit this utility model the most in any form.It should be pointed out that, to this
For the those of ordinary skill in field, without departing from the concept of the premise utility, it is also possible to make some changes and
Improve.These broadly fall into protection domain of the present utility model.
This utility model provides a kind of low flyer, and it both can use as unmanned vehicle, it is also possible to as load
People's aircraft uses.Its large-scale or ultra-large type being mainly characterized by being combined into by multiple multiaxises (such as four axles) aircraft flies
Row device, and by the unified manipulation of a controller.Each Multi-axis aircraft is independent unit, and itself can make with normal flight
With, they are respectively assembled on main stand, are independent of each other.Main stand is also equipped with one or more gimbal levers, uses
In keeping the steady of flight；It addition, above main stand, equipped with safe umbrella, for keeping balance and the safety of landing；
Below main stand, equipped with foot rest, it is used for supporting body, and plays the cushioning effect that decline lands.Of the present utility model
Aircraft, it is simple to install operation, can safe landing, smooth flight, there is preferable application prospect.
In the embodiment of basis of the present utility model, a kind of low flyer provided according to this utility model, including main body
Frame, multiple Multi-axis aircraft (such as 4,6,10 the most more or less)；The plurality of multiaxis flies
Device is arranged on main stand；Interval is all there is between any two Multi-axis aircraft；It is to be appreciated that the flight of multiple multiaxises
Device is owing to being multiple combinations, and each Multi-axis aircraft is not necessarily the same gauge size, uses and flight safety normal
Principle under, can use same size or differ in size Multi-axis aircraft combination, such that it is able to provide the biggest
Lift, can carry the heaviest article or personnel.Multi-axis aircraft can be minute vehicle, small aircraft or
Large Scale Space Vehicle, according to the difference of Multi-axis aircraft size, can obtain large-scale low flyer or ultra-large type low latitude flies
Row device.From the number of axle, Multi-axis aircraft can determine the number of axle as required, such as, select four-axle aircraft.Many
Can be with synergistic combinations control between individual Multi-axis aircraft, it is also possible to individually control as separate unit.According to reality
Border needs, and can multiple Multi-axis aircraft independent assortments be independent of each other, if one of them damages, other can
As usual use.
In the embodiment of basis of the present utility model, symmetrical structure centered by described main stand, the plurality of multiaxis flies
Device is separately positioned in the mounting bracket that described main stand is unsettled, and the plurality of Multi-axis aircraft is along described main stand
Uniform or the non-uniform setting of circumference.Described main stand be X-shaped, cross, triangle, square, trapezoidal, circular or
Person is polygon-shaped.
Described low flyer also includes attitude transducer, acceleration transducer, electric connection line passage.Described attitude senses
Device is arranged on main stand；Described acceleration transducer is arranged on main stand；Described electric connection line passage is described
The inside of main stand extends.
Described low flyer also includes controller；Described controller for carrying out collaborative control to the plurality of Multi-axis aircraft
Make or the most individually control.Under the control of described controller: the attitude transducer inspection being arranged on main stand
Surveying the attitude of main stand, the gimbal lever that described controller is arranged on main stand according to described gesture stability rotates,
The attitude making main stand trends towards the statokinetic preset；The acceleration transducer detection main body being arranged on main stand
The acceleration of frame, if the component that described acceleration is in vertical direction is more than or equal to acceleration of gravity, the most described controller
The safe umbrella controlling to be arranged on main stand is opened.Preferably, controller comprises remote controller part, illustrates, if
Select the four-axle aircraft on market, be commonly provided with the remote controller of 2.4G FREQUENCY CONTROL.Further, it is also possible to make four
Axle aircraft is manipulated on mobile phone by software.
Shown in Fig. 1 above-mentioned basis embodiment a preference in, described low flyer include safe umbrella, foot rest,
The gimbal lever.Described safe umbrella is connected on main stand；Described foot rest is located at the bottom of main stand, and described foot rest is one
Overall structure, foldable structure or stretching structure；Safe umbrella can be fabricated to similar umbrella, can automatic or manual tighten up,
Launch, be used for keeping balance and shielding in landing and emergency.In actual fabrication, foot rest can root
According to factors such as body shape and layouts, the number of foot rest is rationally set, plays and support and the pooling feature of landing.
Shown in Fig. 2 above-mentioned basis embodiment a preference in, described low flyer include seat, the gimbal lever,
Seat belt.Described seat is arranged on main stand；The described gimbal lever is arranged on safe umbrella or on main stand；Institute
State seat belt to be connected on safe umbrella, or be connected between safe umbrella and main stand, by installing seat and seat belt additional,
Can realize carrying people to fly.Low flyer also includes the protective plate being arranged on described seat.Described Multi-axis aircraft bag
Include power supply, motor, rotor, flight controller, induction apparatus；Power supply is motor, flight controller, induction apparatus provide electricity
Source；Motor drives rotor；Flight controller connects motor, induction apparatus.
In a preference of the above-mentioned basis embodiment shown in Fig. 3, low flyer also includes ground traffic tools,
Described main stand is arranged on described ground traffic tools.
Specific description, as it is shown in figure 1, the manipulation of described low flyer is worked by the controller at middle part, it is permissible
Landing, speed and the direction of each miniature/small-sized/large-scale four axles (multiaxis) aircraft of manipulation corner, and safe umbrella
Folding, the attitude of the gimbal lever, thus control whole aircraft；The power of this low flyer mainly miniature by corner
/ small-sized/large-scale four axles (multiaxis) aircraft common combination provides；This aircraft landing and aloft balance, except by
Outside the regulation of multiple miniature/small-sized/large-scale four axles (multiaxis) aircraft, also safe umbrella and the gimbal lever by top works；
The safety of this aircraft, be embodied in the most multiple miniature/small-sized/large-scale four axles (multiaxis) aircraft do not interfere with each other and
Having coordinated flight, be also embodied in decline, particularly in the decline of emergency, safe umbrella and foot rest can play slow
Punching and the effect of protection.
In Fig. 2, the technical scheme of embodiment, principle and Fig. 1 are basically identical, it should be added that, the enforcement of Fig. 1
Example is that unmanned plane load-carrying is less, and in Fig. 2, embodiment is manned vehicle, and this requires that lifting capacity is bigger.In Fig. 2 four
Individual four axles (multiaxis) aircraft is only used as signal, and in actual fabrication, embodiment needs to select small-sized four axles (multiaxis) to fly
Row device, or large-scale four axles (multiaxis) aircraft is as unit, and unit number is abundant, to ensure to provide bigger
Lift, it is achieved manned.Meanwhile, manned vehicle is higher to security requirement, safe umbrella, the gimbal lever, main body machine
Frame and foot rest etc. all can be improved and be adjusted on the basis of embodiment in FIG.Manned can be single, double or many people.
In above-mentioned Fig. 2 embodiment, having installed seat additional, it uses light material to make, and can conveniently pacify installation and dismantling
Unload.Meanwhile, by the seat belt installed additional, the seat belt on aircraft or on automobile can be selected, to ensure the people seizing the opportunity people
Body safety.
In Fig. 3, the technical scheme of embodiment, principle and Fig. 1 and Fig. 2 are basically identical, need explanation, the enforcement of Fig. 3 equally
Example carrying is heavier, can the most manned and loading.As such, it is desirable to the biggest stronger frame, more aircraft unit,
Miscellaneous part is also required to reequip further.Meanwhile, increase some parts to realize existing with bicycle or the combination of other vehicles
Together.So, the range of application of this utility model aircraft has been expanded.
Special instruction, Fig. 1, Fig. 2, Fig. 3 are structural representation of the present utility model, in above-mentioned each figure embodiment, only
Parts in figure are set forth.It is appreciated that aircraft is the electronic component by multiple precisions and machine components group
Conjunction forms.Aircraft of the present utility model not only includes the parts in embodiment, also includes the parts of other indispensabilities.
Above specific embodiment of the utility model is described.It is to be appreciated that this utility model is not
Being confined to above-mentioned particular implementation, those skilled in the art can make a variety of changes within the scope of the claims
Or amendment, this has no effect on flesh and blood of the present utility model.In the case of not conflicting, embodiments herein
Can arbitrarily be mutually combined with the feature in embodiment.
Claims (8)
1. a low flyer, it is characterised in that include main stand, multiple Multi-axis aircraft；
The plurality of Multi-axis aircraft is arranged on main stand；
Interval is all there is between any two Multi-axis aircraft.
Low flyer the most according to claim 1, it is characterised in that also include following any one or appoint multiple
Device:
-safe umbrella, described safe umbrella is connected on main stand；
-foot rest, described foot rest is located at the bottom of main stand, and described foot rest is an overall structure, foldable structure or stretches
Shrinking structure；
-seat, described seat is arranged on main stand；
-attitude transducer, described attitude transducer is arranged on main stand；
-acceleration transducer, described acceleration transducer is arranged on main stand；
-electric connection line passage, described electric connection line passage extends in the inside of described main stand.
Low flyer the most according to claim 2, it is characterised in that also include following any one or appoint multiple
Device:
-the gimbal lever, the described gimbal lever is arranged on safe umbrella or on main stand；
-seat belt, described seat belt is connected on safe umbrella, or is connected between safe umbrella and main stand.
Low flyer the most according to claim 2, it is characterised in that symmetrical junction centered by described main stand
Structure, the plurality of Multi-axis aircraft is separately positioned in the mounting bracket that described main stand is unsettled, and the plurality of multiaxis flies
Row device is along the uniform or non-uniform setting of circumference of described main stand.
Low flyer the most according to claim 1, it is characterised in that described main stand is X-shaped, cross
Shape, triangle, square, trapezoidal, circular or polygon-shaped.
Low flyer the most according to claim 1, it is characterised in that described Multi-axis aircraft include power supply,
Motor, rotor, flight controller, induction apparatus；
Power supply is motor, flight controller, induction apparatus provide power supply；
Motor drives rotor；
Flight controller connects motor, induction apparatus.
Low flyer the most according to claim 1, it is characterised in that also include ground traffic tools, described
Main stand is arranged on described ground traffic tools.
Low flyer the most according to claim 2, it is characterised in that also include being arranged on described seat
Protective plate；
Described protective plate extends to from the bottom of seat between space, surface and the Multi-axis aircraft of described seat.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620107657.2U CN205525009U (en) | 2016-02-02 | 2016-02-02 | Low -latitude flying ware |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620107657.2U CN205525009U (en) | 2016-02-02 | 2016-02-02 | Low -latitude flying ware |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205525009U true CN205525009U (en) | 2016-08-31 |
Family
ID=56775639
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620107657.2U Expired - Fee Related CN205525009U (en) | 2016-02-02 | 2016-02-02 | Low -latitude flying ware |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205525009U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105564647A (en) * | 2016-02-02 | 2016-05-11 | 向东 | Low-altitude aircraft |
| CN111776227A (en) * | 2019-04-04 | 2020-10-16 | 杭州海存信息技术有限公司 | Airplane cabin for carrying out cabin service by using unmanned aerial vehicle and method thereof |
-
2016
- 2016-02-02 CN CN201620107657.2U patent/CN205525009U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105564647A (en) * | 2016-02-02 | 2016-05-11 | 向东 | Low-altitude aircraft |
| CN111776227A (en) * | 2019-04-04 | 2020-10-16 | 杭州海存信息技术有限公司 | Airplane cabin for carrying out cabin service by using unmanned aerial vehicle and method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160831 Termination date: 20210202 |