CN209321266U - A kind of multi-functional unmanned plane during flying platform - Google Patents

Abstract

The utility model discloses a kind of multi-functional unmanned plane during flying platforms, including UAV flight's platform and the rotor bar being fixedly mounted on UAV flight's platform side, the rotor bar equidistantly distributes on UAV flight's platform, and six roots of sensation rotor bar is the point centered on UAV flight's platform, and radial structure, the rotor bar are fixedly installed with the drive motor for playing driving effect on one end of extraneous radiation outward.The multi-functional unmanned plane during flying platform by the equipment interface of multiple and different types of setting, promotes the mission payload of unmanned plane that plug and play may be implemented in actual use, and replacement load does not need to debug unmanned plane again, improves the multiple functions of unmanned plane；The undercarriage bottom of unmanned plane is provided with supporting mechanism, and includes buffer cell in supporting mechanism, when unmanned plane is in landing, during ground face contact, impact force caused by landing can be allowed to do maximum reduction processing.

Description

A kind of multi-functional unmanned plane during flying platform

Technical field

The utility model relates to air vehicle technique field, specially a kind of multi-functional unmanned plane during flying platform.

Background technique

UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer, compared with manned aircraft, nobody Machine is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Unmanned plane press application field, can be divided into it is military with it is civilian. Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+industrial application are that unmanned plane has really just needed； At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, The application in news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded unmanned plane itself Purposes, developed country also actively extension industrial application and develop unmanned air vehicle technique.

Through retrieving, Chinese patent disclose it is a kind of based on unmanned plane multi-functional flying platform (authorization public number: CN207902742U), which includes propeller, motor, bracket, chassis, cross bar, auxiliary frame, holder, controller, leads Navigate device, and the bracket is the radial structure of point with center, and the body of rod of You Duogen equidistant arrangement is composed, above and below the bracket End face is consistent, after installation with ground be in parallel construction, the carrier openings end position be equipped with motor, using fastening mounting means, The propeller is bilobed structure, is rotated always in carrier openings end position, the bracket is equipped with close to center position Corresponding chassis, the chassis are "u"-shaped, and lower end vertical welding is connected cross bar, and the utility model is equipped with auxiliary frame, has and pacify Dress, fastening, regulatory function, can temporarily increase photographic device, and unmanned plane is helped to realize image collection operation.

To sum up, above-mentioned patented technology content and in the prior art used in unmanned plane in use, due to Its equipment interface for lacking multiple and different types, so that the mission payload of unmanned plane cannot achieve plug and play, replacement load is needed Again unmanned plane is debugged, the multiple functions of unmanned plane are reduced；In addition, unmanned plane during rising and falling, is especially dropping During falling, the undercarriage of unmanned plane will receive great impact power, and then cause to damage to the undercarriage of unmanned plane, promote nothing Generally shorter phenomenon occurs man-machine and undercarriage normal service life；And existing unmanned plane can not executive chairman's distance Task, because of the limited capacity of the power storage electric power of unmanned plane so that unmanned plane can only be confined to execute it is short-range Task reduces the service performance of unmanned plane itself, and we have proposed a kind of multi-functional unmanned plane during flying platforms thus.

Utility model content

The technical problems to be solved in the utility model is to overcome existing defect, and it is flat to provide a kind of multi-functional unmanned plane during flying Platform can effectively solve the problems in background technique.

To achieve the above object, the utility model provides the following technical solutions: a kind of multi-functional unmanned plane during flying platform, packet The rotor bar for including UAV flight's platform and being fixedly mounted on UAV flight's platform side, the rotor bar is in unmanned plane It is equidistantly distributed on carrying platform, and six roots of sensation rotor bar is the point centered on UAV flight's platform, and radial knot outward Structure, the rotor bar are fixedly installed with the drive motor for playing driving effect, the drive motor on one end of extraneous radiation Driving end on be fixedly installed with helical blade in a rectangular parallelepiped shape, the upper surface of UAV flight's platform is fixedly installed with One be in regular polygon shape protection box body, it and is not that insertion, which is equipped with no less than four, on the side of the protection box body Congener data-interface, the upper surface of the protection box body are fixedly installed with the photovoltaic solar electricity that can produce a small amount of electric energy Pond plate, the lower surface of UAV flight's platform, which is bolted, is equipped with undercarriage, and the bottom of the undercarriage is fixed The supporting mechanism that drop impact power can be cut down is installed, the inside of the protection box body is successively fixedly mounted useful from left to right To receive the signal receiving module of wireless signal, play the role of the navigation module in clear unmanned plane target place and to manipulator The data processing module that the instruction issued is handled.

It further include the unmanned plane charging system resting on the ground, institute as a kind of optimal technical scheme of the utility model Stating unmanned plane charging system includes emitting location information for the GPS module in place of charging recently to be presented to unmanned plane, plays The signal emission module acted on to remote control terminal and the signal amplification module to location information progress signal enhancing.

As a kind of optimal technical scheme of the utility model, the supporting mechanism includes fixed plate, buffer cell and holds The upper surface of pressing plate, the fixed plate is connected by bolt with the bottom of undercarriage, the fixed peace in the lower surface of the fixed plate For dress there are three structure snd size buffer cell all the same, and linearly arranging, the bottom of three buffer cells is fixed It is connected with the bearing plate of one piece of rubber material.

As a kind of optimal technical scheme of the utility model, the buffer cell includes telescopic rod, the first mounting plate, Two mounting plates, axle sleeve, limit cutting ferrule, spring, first rotating shaft, the second shaft and connecting rod, the fixing end connection of the telescopic rod There is the first mounting plate, and the telescopic end of telescopic rod is fixedly connected with the second mounting plate, is socketed on the centre portion of the telescopic rod Have the axle sleeve that can move up and down, and on the centre portion of telescopic rod close to axle sleeve lower position be fixedly attached it is limited Position cutting ferrule is socketed with spring, the axle sleeve between the axle sleeve and the first mounting plate and at the outer surface position of telescopic rod Side on be fixedly installed with first rotating shaft, the upper surface of second mounting plate fixed peace at a side position of telescopic rod Equipped with the second shaft, a connecting rod is connected between the first rotating shaft and the second shaft.

As a kind of optimal technical scheme of the utility model, the number of the first rotating shaft, the second shaft and connecting rod There are two amount is respectively provided with, and two groups of first rotating shafts, the second shaft and connecting rod are the settings substantially symmetrical about its central axis with telescopic rod.

As a kind of optimal technical scheme of the utility model, the data-interface includes four kinds of interfaces, respectively PWM altogether Interface, PPM interface, USB data interface and SDIO interface.

Compared with prior art, the utility model has the beneficial effects that

1, the multi-functional unmanned plane during flying platform is connect by the equipment of multiple and different types of setting in actual use Mouthful, promote the mission payload of unmanned plane that plug and play may be implemented, replacement load does not need to debug unmanned plane again, improves nothing Man-machine multiple functions.

2, the multi-functional unmanned plane during flying platform passes through the signal receiving module of setting, navigation module in actual use And data processing module, can with rest on the ground unmanned plane charging base station carry out data connection, unmanned plane can by search, The charging base station nearest apart from unmanned plane is found, by the road model plane of GPS module and unmanned plane itself in charging base station Block can allow unmanned plane to quickly generate flight path, solve the problems, such as that unmanned plane can not carry out executing aerial mission over long distances.

3, the multi-functional unmanned plane during flying platform is provided with support in the undercarriage bottom of unmanned plane in actual use Mechanism, and include buffer cell in supporting mechanism, when unmanned plane is in landing, during ground face contact, Ke Yirang Impact force caused by landing does maximum reduction processing, so that the undercarriage to unmanned plane is protected, extends nothing Man-machine and undercarriage normal service life, it is scientific and reasonable for structure, it is safe and convenient to use.

Detailed description of the invention

Fig. 1 is the structural schematic diagram of the utility model；

Fig. 2 is that the unmanned plane of the utility model finds the functional block diagram of charging base station；

Fig. 3 is the structural schematic diagram of the utility model supporting mechanism；

Fig. 4 is the structural schematic diagram of the utility model buffer cell.

In figure: 1, UAV flight's platform；2, rotor bar；3, drive motor；4, helical blade；5, box body is protected；6, number According to interface；7, photovoltaic solar cell panels；8, undercarriage；9, supporting mechanism；91, fixed plate；92, buffer cell；921, it stretches Bar；922, the first mounting plate；923, the second mounting plate；924, axle sleeve；925, cutting ferrule is limited；926, spring；927, first rotating shaft； 928, the second shaft；929, connecting rod；93, bearing plate；10, signal receiving module；11, navigation module；12, data processing mould Block；13, unmanned plane charging system；14, GPS module；15, signal emission module；16, signal amplification module.

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.

The utility model provides a kind of technical solution referring to FIG. 1-2: a kind of multi-functional unmanned plane during flying platform, including UAV flight's platform 1 and the rotor bar 2 being fixedly mounted on 1 side of UAV flight's platform, rotor bar 2 are taken in unmanned plane It is equidistantly distributed on carrying platform 1, and six roots of sensation rotor bar 2 is the point centered on UAV flight's platform 1, and radial knot outward Structure, rotor bar 2 are fixedly installed with the drive motor 3 for playing driving effect, the driving of drive motor 3 on one end of extraneous radiation Helical blade 4 in a rectangular parallelepiped shape is fixedly installed on end, the upper surface of UAV flight's platform 1 is fixedly installed with one in just The protection box body 5 of multilateral shape protects insertion on the side of box body 5 to be equipped with no less than four, and is different types of number According to interface 6, the upper surface of box body 5 is protected to be fixedly installed with the photovoltaic solar cell panels 7 that can produce a small amount of electric energy, nobody The lower surface of machine carrying platform 1, which is bolted, is equipped with undercarriage 8, and the bottom of undercarriage 8, which is fixedly installed with, to cut down The inside of the supporting mechanism 9 of drop impact power, protection box body 5 is successively fixedly installed with for receiving wireless signal from left to right Signal receiving module 10, the navigation module 11 for playing the role of clear unmanned plane target place and the instruction that manipulator is issued The data processing module 12 handled, the unmanned plane during flying platform further include the unmanned plane charging system 13 resting on the ground, Unmanned plane charging system 13 includes for the GPS module 14 in place of charging recently to be presented to unmanned plane, plays and sends out location information Penetrate to the signal emission module 15 of remote control terminal effect and carry out to location information the signal amplification module of signal enhancing 16。

Referring to Fig. 3, supporting mechanism 9 includes fixed plate 91, buffer cell 92 and bearing plate 93, the upper table of fixed plate 91 Face is connected by bolt with the bottom of undercarriage 8, and there are three structure snd size are homogeneous for the lower surface fixed installation of fixed plate 91 Together, and linearly the buffer cell 92 arranged, the bottom of three buffer cells 92 are fixedly connected to holding for one piece of rubber material Pressing plate 93.

Referring to Fig. 4, buffer cell 92 includes telescopic rod 921, the first mounting plate 922, the second mounting plate 923, axle sleeve 924, cutting ferrule 925, spring 926, first rotating shaft 927, the second shaft 928 and connecting rod 929, the fixing end of telescopic rod 921 are limited The first mounting plate 922 is connected with, and the telescopic end of telescopic rod 921 is fixedly connected with the second mounting plate 923, in telescopic rod 921 Between be socketed with the axle sleeve that can move up and down 924 on section, and close to axle sleeve 924 on the centre portion of telescopic rod 921 Lower position has been fixedly attached limit cutting ferrule 925, between axle sleeve 924 and the first mounting plate 922 and is located at the outer of telescopic rod 921 It is socketed with spring 926 at surface location, first rotating shaft 927 is fixedly installed on the side of axle sleeve 924, the second mounting plate 923 Upper surface is fixedly installed with the second shaft 928, first rotating shaft 927 and the second shaft at a side position of telescopic rod 921 A connecting rod 929 is connected between 928, the quantity of first rotating shaft 927, the second shaft 928 and connecting rod 929 is provided with Two, and two groups of first rotating shafts 927, the second shaft 928 and connecting rod 929 are the settings substantially symmetrical about its central axis with telescopic rod 921.

Data-interface 6 includes four kinds of interfaces altogether, respectively PWM interface, PPM interface, USB data interface and SDIO interface, PWM interface transmits a kind of single-wire signal, and the period sends positive pulse, mode of the variation pulsewidth as transmitting information, and a stitch passes A channel is passed, often arrange in pairs or groups ground wire and the controllable steering engine of power supply line or an electricity tune, PPM interface is each signal period The combination for becoming sending one group of multiple pulsewidth, carrys out while transmitting the change information in multiple channels, and USB interface can be connected by HUB Connect multiple equipment, the mission payload of unmanned plane promoted to may be implemented plug and play, SDIO interface be for connecting SD card or TF card, Carry out flight data recording.

The working principle and process for using of the utility model: when unmanned plane is during executing aerial mission hair, appearance is electric When the situation that energy is insufficient, the openable operation control terminal of operator utilizes the GPS module resting on the ground in unmanned plane charging system 13 14, signal emission module 15 and signal amplification module 16 are determined in conjunction with the locating module that unmanned plane inside inherently has Behind the charging base station nearest apart from unmanned plane, manipulator can change the flight path of unmanned plane using remote control terminal, nobody After signal receiving module 10 on machine receives flight orders, in conjunction with the navigation module 11 of itself, flight path is planned, and pass through Data processing module 12 changes the state of flight of unmanned plane driving mechanism, so as to realize the recharging function of unmanned plane, Solve the problems, such as that unmanned plane can not execute long-distance flight task, when unmanned plane during flying terminates to need to land, landing is produced Raw impact force can act at the first time on the bearing plate 93 of rubber material, and under inner transmitting effect, bearing plate 93 can be incited somebody to action Impact force is transferred to the second mounting plate 923, then is transferred on telescopic rod 921, and telescopic rod 921 on the one hand can directly be promoted to shrink, Another aspect impact force can be transferred to axle sleeve 924 under the action of connecting rod 929, first rotating shaft 927 and the second shaft 928 On, promote axle sleeve 924 to cause to squeeze to spring 926, and then realize the purpose for cutting down impact force, limit cutting ferrule 925 plays limitation Position of the axle sleeve 924 in folding process, in addition, the unmanned plane is promoted by the data-interface 6 of multiple and different types of setting Plug and play may be implemented in the mission payload of unmanned plane, and replacement load does not need to debug unmanned plane again, improves unmanned plane Multiple functions, wherein data-interface 6, signal receiving module 10, navigation module 11, data processing module 12, GPS module 14, letter Number transmitting module 15 and signal amplification module 16 are all made of the prior art, and and will not be described here in detail.

Finally, it should be noted that above embodiments are only to illustrate the technical solution of the utility model, rather than its limitations； Although the utility model is described in detail with reference to the foregoing embodiments, those skilled in the art should understand that: It is still possible to modify the technical solutions described in the foregoing embodiments, or part of technical characteristic is carried out etc. With replacement；And these are modified or replaceed, various embodiments of the utility model technology that it does not separate the essence of the corresponding technical solution The spirit and scope of scheme.

Claims (6)

1. a kind of multi-functional unmanned plane during flying platform, including UAV flight's platform (1) and it is fixedly mounted on UAV flight Rotor bar (2) on platform (1) side, it is characterised in that: the rotor bar (2) is equidistant on UAV flight's platform (1) Distribution, and six roots of sensation rotor bar (2) is the point centered on UAV flight's platform (1), and radial structure outward, the rotor Bar (2) is fixedly installed with the drive motor (3) for playing driving effect on one end of extraneous radiation, the drive motor (3) Helical blade (4) in a rectangular parallelepiped shape, the fixed peace in the upper surface of UAV flight's platform (1) are fixedly installed on driving end It is in the protection box body (5) of regular polygon shape equipped with one, insertion is equipped with no less than four on the side of protection box body (5) It is a, and be different types of data-interface (6), the upper surface of protection box body (5), which is fixedly installed with, can produce on a small quantity The photovoltaic solar cell panels (7) of electric energy, the lower surface of UAV flight's platform (1), which is bolted to be equipped with, rises and falls Frame (8), the bottom of the undercarriage (8) are fixedly installed with the supporting mechanism (9) that can cut down drop impact power, the protection box The inside of body (5) be successively fixedly installed with from left to right for receive wireless signal signal receiving module (10), play it is clear The data processing mould that the navigation module (11) of unmanned plane target place effect and the instruction issued to manipulator are handled Block (12).

2. a kind of multi-functional unmanned plane during flying platform according to claim 1, it is characterised in that: further include resting on the ground Unmanned plane charging system (13), the unmanned plane charging system (13) include for give unmanned plane present recently charging place GPS module (14) plays the role of the signal emission module (15) that location information is transmitted to remote control terminal and to positioning The signal amplification module (16) of information progress signal enhancing.

3. a kind of multi-functional unmanned plane during flying platform according to claim 1, it is characterised in that: the supporting mechanism (9) Including fixed plate (91), buffer cell (92) and bearing plate (93), the upper surface of the fixed plate (91) passes through bolt and rises and falls The bottom of frame (8) is connected, and there are three the lower surface fixed installations of the fixed plate (91), and structure snd size are all the same, and are in line Property arrangement buffer cell (92), the bottom of three buffer cells (92) is fixedly connected to the pressure-bearing of one piece of rubber material Plate (93).

4. a kind of multi-functional unmanned plane during flying platform according to claim 3, it is characterised in that: the buffer cell (92) Including telescopic rod (921), the first mounting plate (922), the second mounting plate (923), axle sleeve (924), limit cutting ferrule (925), spring (926), the fixing end of first rotating shaft (927), the second shaft (928) and connecting rod (929), the telescopic rod (921) is connected with First mounting plate (922), and the telescopic end of telescopic rod (921) is fixedly connected with the second mounting plate (923), the telescopic rod (921) axle sleeve that can move up and down (924) is socketed on centre portion, and on the centre portion of telescopic rod (921) Lower position close to axle sleeve (924) has been fixedly attached limit cutting ferrule (925), the axle sleeve (924) and the first mounting plate (922) it is socketed with spring (926) between and at the outer surface position of telescopic rod (921), on the side of the axle sleeve (924) It is fixedly installed with first rotating shaft (927), the side position of the upper surface of second mounting plate (923) close to telescopic rod (921) Place is fixedly installed with the second shaft (928), is connected with one between the first rotating shaft (927) and the second shaft (928) and is connect Bar (929).

5. a kind of multi-functional unmanned plane during flying platform according to claim 4, it is characterised in that: the first rotating shaft (927), there are two the quantity of the second shaft (928) and connecting rod (929) is respectively provided with, and two groups of first rotating shafts (927), second Shaft (928) and connecting rod (929) are with the setting substantially symmetrical about its central axis of telescopic rod (921).

6. a kind of multi-functional unmanned plane during flying platform according to claim 1, it is characterised in that: the data-interface (6) It altogether include four kinds of interfaces, respectively PWM interface, PPM interface, USB data interface and SDIO interface.