CN208530845U - Intelligent navigation steward system based on eight-rotary wing aircraft - Google Patents

Intelligent navigation steward system based on eight-rotary wing aircraft Download PDF

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Publication number
CN208530845U
CN208530845U CN201820659166.8U CN201820659166U CN208530845U CN 208530845 U CN208530845 U CN 208530845U CN 201820659166 U CN201820659166 U CN 201820659166U CN 208530845 U CN208530845 U CN 208530845U
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CN
China
Prior art keywords
shell
controller
solar panel
mounting groove
wing aircraft
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Expired - Fee Related
Application number
CN201820659166.8U
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Chinese (zh)
Inventor
侯黎阳
侯彦东
刘畅
孙悦颖
刘素素
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Henan University
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Henan University
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Publication date
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Priority to CN201820659166.8U priority Critical patent/CN208530845U/en
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Publication of CN208530845U publication Critical patent/CN208530845U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/50On board measures aiming to increase energy efficiency

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  • Photovoltaic Devices (AREA)
  • Arrangements For Transmission Of Measured Signals (AREA)

Abstract

The utility model provides a kind of new intelligent navigation steward system based on eight-rotary wing aircraft, comprising: shell is provided with the first mounting groove at the top center of the shell;The inside of the shell is arranged in controller;The inside of the shell is arranged in first wireless sensor;The inside of the shell is arranged in GPS navigation;The bottom of the shell is arranged in wide-angle camera;Ultrasonic sensor, the ultrasonic sensor are uniformly arranged on the side wall of the shell;Four shaft mechanical arms, are arranged in the middle position of the housing bottom;Bracket, the bracket are arranged in the third mounting groove;Client is provided with third wireless sensor corresponding with first wireless sensor in the client.It by the technical solution of the utility model, is capable of providing material object and navigates, so that route guidance easily facilitates operation, may also help in user and carry part objects, functional diversities improve the usage experience of user.

Description

Intelligent navigation steward system based on eight-rotary wing aircraft
Technical field
The utility model relates to the technical fields of unmanned plane, in particular to a kind of intelligence based on eight-rotary wing aircraft Can navigate steward system.
Background technique
With the rapid development of science and technology, a possibility that mankind enter foreign environment in daily life and work is increasingly Height, cell phone map navigation software progresses into the life of ordinary people whereby.When user enters strange region, user passes through Cell phone map software navigation can reach the destination, but often frequent operation, user are difficult to this kind of software without systematic learning It uses, significantly influences the normal use of user, and function is more single.
Utility model content
The utility model is based at least one above-mentioned technical problem, proposes a kind of new based on eight-rotary wing aircraft Intelligent navigation steward system, structure is simple, strong operability, is capable of providing material object and navigates, and it is negative to may also help in user Part objects are carried on a shoulder pole, functional diversities improve the usage experience of user.
In view of this, the utility model proposes a kind of new intelligent navigation steward system based on eight-rotary wing aircraft, Include: shell, the first mounting groove is provided at the top center of the shell, is provided with solar-electricity in first mounting groove Pond plate is evenly arranged with the second mounting groove led in eight inside, each second installation around first mounting groove It is provided with helical mount in slot, propeller is provided on each helical mount, each propeller is all connected to The solar panel, there are four third mounting grooves for the bottom setting of the shell;Controller is arranged in the shell Portion is connected to the solar panel and the propeller;The inside of the shell is arranged in first wireless sensor, even It is connected to the controller and the solar panel;The inside of the shell is arranged in GPS navigation, is connected to described first Wireless sensor, the controller and the solar panel;The bottom of the shell is arranged in wide-angle camera, connection In first wireless sensor, the controller and the solar panel, for acquiring the eight-rotary wing aircraft week The video information in collarette border;Ultrasonic sensor, the ultrasonic sensor is uniformly arranged on the side wall of the shell, described Ultrasonic sensor is connected to the controller and the solar panel, for acquiring ring locating for the eight-rotary wing aircraft The peripheral obstacle information in border;Four shaft mechanical arms, are arranged in the middle position of the housing bottom, are connected to the controller With the solar panel;Bracket, the bracket are arranged in the third mounting groove;Client is set in the client It is equipped with third wireless sensor corresponding with first wireless sensor.
In the technical scheme, the case top of the intelligent navigation steward system based on eight-rotary wing aircraft is provided with the sun Energy solar panel increases cruising ability convenient for charging;Wide-angle camera setting is in housing bottom, convenient for clearly eight rotation of acquisition Environmental information around rotor aircraft, and by collected information with video information transmission to the controller of connection, controller energy It is enough that propeller rotational is controlled according to ultrasonic sensor, so that effective avoiding barrier, realizes normal flight;It is arranged in shell Four shaft mechanical arms of bottom are connected to controller and solar panel, allow users to weight being suspended on mechanical arm On, burden is alleviated for user, imparts eight-rotary wing aircraft multiple functions;The first wireless sensor being arranged on shell connects The third wireless sensor being connected in client, controller are connected to the first wireless sensor, transmit convenient for information, wherein client End is arranged on the mobile terminal of user, facilitates user and carries out practical operation by client in real time, effectively increases user Usage experience, the bracket in third mounting groove is set, it is therefore prevented that eight-rotary wing aircraft land when be damaged, effectively extend The service life of eight-rotary wing aircraft.
In the above-mentioned technical solutions, it is preferable that further include: LED major light is arranged on the side wall of the shell, connection In the controller and the solar panel, for providing illumination for user;The bottom of the shell is arranged in loudspeaker Portion is connected to the controller and the solar panel;The bottom of the shell is arranged in microphone, is connected to described Controller and the solar panel;Headphone is arranged in the top of the shell, is arranged on the headphone There is the second wireless sensor.
In the technical scheme, LED major light is arranged on the side wall of shell, can provide in a dark environment for user Lighting service improves the usage experience of user;Loudspeaker, microphone and the headphone being installed on shell facilitate to Family carries out voice prompting, provides voice interactive function for user, convenient for users to use.
In the above-mentioned technical solutions, it is preferable that further include: shield, the shield include the first shield and second The top of each second mounting groove is arranged in shield, first shield, and second shield is arranged each The bottom of second mounting groove.
In the technical scheme, shield is located at the top and bottom of the second mounting groove, effectively prevent dust into Enter in the second mounting groove, maintain the normal use of propeller, improves the safety and reliability that eight-rotary wing aircraft uses.
In the above-mentioned technical solutions, it is preferable that the surface of the wide-angle camera is provided with dustproof cover.
In the technical scheme, the dustproof cover that wide-angle imaging head surface is arranged in effectively maintains the use of wide-angle camera Service life.
By above technical scheme, so that route guidance easily facilitates operation, it is capable of providing material object and navigates, it can be with Burden for users part objects are helped, functional diversities improve the usage experience of user.
Detailed description of the invention
Fig. 1 shows the intelligent navigation steward system based on eight-rotary wing aircraft of embodiment according to the present utility model Overall structure diagram;
Fig. 2 shows the bottoms of the intelligent navigation steward system in eight-rotary wing aircraft of embodiment according to the present utility model Portion's structural schematic diagram;
Fig. 3 shows the side of the intelligent navigation steward system in eight-rotary wing aircraft of embodiment according to the present utility model Face structural schematic diagram;
Fig. 4 shows the top of the intelligent navigation steward system in eight-rotary wing aircraft of embodiment according to the present utility model Portion's structural schematic diagram.
Specific embodiment
In order to be more clearly understood that the above objects, features, and advantages of the utility model, with reference to the accompanying drawing and have The utility model is further described in detail in body embodiment.It should be noted that in the absence of conflict, this Shen The feature in embodiment and embodiment please can be combined with each other.
Many details are explained in the following description in order to fully understand the utility model, still, this is practical Novel to be implemented using other than the one described here other way, therefore, the protection scope of the utility model is simultaneously It is not limited by the specific embodiments disclosed below.
Explanation is further explained to the utility model below in conjunction with Fig. 1, Fig. 2, Fig. 3 and Fig. 4.
As shown in Figures 1 to 4, a kind of intelligent navigation steward system based on eight-rotary wing aircraft, comprising: shell 101, institute It states and is provided with the first mounting groove 102 at the top center of shell 101, be provided with solar battery in first mounting groove 102 Plate 103, is evenly arranged with the second mounting groove 104 led in eight inside around first mounting groove 102, and each described the It is provided with helical mount 113105 in two mounting grooves 104, is provided with propeller on each helical mount 113105 106, each propeller 106 is all connected to the solar panel 103, and there are four the bottom settings of the shell 101 Third mounting groove (not shown);Controller 107 is arranged in the inside of the shell 101, is connected to the solar battery Plate 103 and the propeller 106;First wireless sensor 108 is arranged in the inside of the shell 101, is connected to the control Device 107 and the solar panel 103;GPS navigation 109 is arranged in the inside of the shell 101, is connected to described first Wireless sensor 108, the controller 107 and the solar panel 103;Wide-angle camera 110 is arranged in the shell 101 bottom is connected to first wireless sensor 108, the controller 107 and the solar panel 103, is used for Acquire the video information of the eight-rotary wing aircraft ambient enviroment;Ultrasonic sensor 111, the ultrasonic sensor 111 is On the even side wall that the shell 101 is arranged in, the ultrasonic sensor 111 is connected to the controller 107 and the sun Energy solar panel 103, for acquiring the peripheral obstacle information of the eight-rotary wing aircraft local environment;Four shaft mechanical arms 112, The middle position of 101 bottom of shell is set, the controller 107 and the solar panel 103 are connected to;Bracket 113, the bracket 113 is arranged in the third mounting groove;Client (not shown), be provided in the client with The corresponding third wireless sensor of first wireless sensor 108.
In the technical scheme, it is provided at the top of the shell 101 of the intelligent navigation steward system based on eight-rotary wing aircraft Solar panel 103 increases cruising ability convenient for charging;The setting of wide-angle camera 110 is in 101 bottom of shell, convenient for clear Environmental information around clear acquisition eight-rotary wing aircraft, and by collected information with video information transmission to the control of connection Device 107, controller 107 can control propeller 106 according to ultrasonic sensor 111 and rotate, thus effective avoiding barrier, Realize normal flight;The four shaft mechanical arms 112 that 101 bottom of shell is arranged in are connected to controller 107 and solar panel 103, it allows users to for weight being suspended on mechanical arm, alleviates burden for user, it is more to impart eight-rotary wing aircraft Kind function;The first wireless sensor 108 being arranged on shell 101 is connected to the third wireless sensor in client, control Device 107 is connected to the first wireless sensor 108, transmits convenient for information, and wherein client is arranged on the mobile terminal of user, side User practical operation is carried out by client in real time, effectively increase the usage experience of user, be arranged in third mounting groove Interior bracket 113, it is therefore prevented that eight-rotary wing aircraft is damaged when landing, and effectively extend eight-rotary wing aircraft uses the longevity Life.
In the above-mentioned technical solutions, it is preferable that further include: the side wall of the shell 101 is arranged in LED major light 114 On, it is connected to the controller 107 and the solar panel 103, for providing illumination for user;Loudspeaker 115, setting In the bottom of the shell 101, it is connected to the controller 107 and the solar panel 103;Microphone 116, setting exist The bottom of the shell 101 is connected to the controller 107 and the solar panel 103;Headphone 117, setting The second wireless sensor is provided on the top of the shell 101, the headphone 117.
In the technical scheme, LED major light 114 is arranged on the side wall of shell 101, can use in a dark environment Family provides lighting service, improves the usage experience of user;It the loudspeaker 115 that is installed on shell 101, microphone 116 and wears Formula earphone 117, which is facilitated, carries out voice prompting to user, provides voice interactive function for user, convenient for users to use.
In the above-mentioned technical solutions, it is preferable that further include: shield, the shield include the first shield 118 and the The top of each second mounting groove 104, second shield is arranged in two shields 119, first shield 118 119 are arranged in the bottom of each second mounting groove 104.
In the technical scheme, shield is located at the top and bottom of the second mounting groove 104, effectively prevents dust Into in the second mounting groove 104, the normal use of propeller 106 is maintained, improves the safety that eight-rotary wing aircraft uses And reliability.
In the above-mentioned technical solutions, it is preferable that the surface of the wide-angle camera 110 is provided with dustproof cover and (does not show in figure Out).
In the technical scheme, the dustproof cover that 110 surface of wide-angle camera is arranged in effectively maintains wide-angle camera 110 Service life.
In actual application process, destination can be arranged by client in user, then pass through the first wireless sensing Device and third wireless sensor carry out information transmission, are handled by controller, realize instruction issuing, then eight-rotary wing aircraft base Route planning is carried out in GPS navigation, best route is selected to advance, is being advanced on the way, the current road of ultrasonic sensor real-time monitoring The advance property on road, remove barriers object, carries out guidance in kind to user and four shaft mechanicals of housing bottom are arranged at the same time Arm can help user to carry thing, to reduce the burden of user;In night running, it can open and be arranged in housing sidewall LED major light, for user illuminate.
The technical solution of the utility model is had been described in detail above with reference to the accompanying drawings, the technical solution of the utility model proposes A kind of new intelligent navigation steward system based on eight-rotary wing aircraft, is capable of providing material object and navigates, so that route guidance Operation is easily facilitated, may also help in burden for users part objects, functional diversities improve the usage experience of user.
The above descriptions are merely preferred embodiments of the present invention, is not intended to limit the utility model, for this For the technical staff in field, various modifications and changes may be made to the present invention.It is all in the spirit and principles of the utility model Within, any modification, equivalent replacement, improvement and so on should be included within the scope of protection of this utility model.

Claims (4)

1. a kind of intelligent navigation steward system based on eight-rotary wing aircraft characterized by comprising
Shell is provided with the first mounting groove at the top center of the shell, is provided with solar-electricity in first mounting groove Pond plate is evenly arranged with the second mounting groove led in eight inside, each second installation around first mounting groove It is provided with helical mount in slot, propeller is provided on each helical mount, each propeller is all connected to The solar panel, there are four third mounting grooves for the bottom setting of the shell;
The inside of the shell is arranged in controller, is connected to the solar panel and the propeller;
The inside of the shell is arranged in first wireless sensor, is connected to the controller and the solar panel;
The inside of the shell is arranged in GPS navigation, be connected to first wireless sensor, the controller and it is described too Positive energy solar panel;
The bottom of the shell is arranged in wide-angle camera, is connected to first wireless sensor, the controller and described Solar panel, for acquiring the video information of the eight-rotary wing aircraft ambient enviroment;
Ultrasonic sensor, the ultrasonic sensor are uniformly arranged on the side wall of the shell, the ultrasonic sensor It is connected to the controller and the solar panel, for acquiring the surrounding obstacles of the eight-rotary wing aircraft local environment Object information;
Four shaft mechanical arms, are arranged in the middle position of the housing bottom, are connected to the controller and the solar-electricity Pond plate;
Bracket, the bracket are arranged in the third mounting groove;
Client is provided with third wireless sensor corresponding with first wireless sensor in the client.
2. the intelligent navigation steward system according to claim 1 based on eight-rotary wing aircraft, which is characterized in that also wrap It includes:
LED major light is arranged on the side wall of the shell, is connected to the controller and the solar panel, is used for Illumination is provided for user;
The bottom of the shell is arranged in loudspeaker, is connected to the controller and the solar panel;
The bottom of the shell is arranged in microphone, is connected to the controller and the solar panel;
Headphone is arranged in the top of the shell, the second wireless sensor is provided on the headphone.
3. the intelligent navigation steward system according to claim 1 based on eight-rotary wing aircraft, which is characterized in that also wrap It includes:
Shield, the shield include the first shield and the second shield, and first shield is arranged each described The bottom of each second mounting groove is arranged in the top of second mounting groove, second shield.
4. the intelligent navigation steward system according to claim 1 based on eight-rotary wing aircraft, which is characterized in that described wide The surface of angle camera is provided with dustproof cover.
CN201820659166.8U 2018-05-04 2018-05-04 Intelligent navigation steward system based on eight-rotary wing aircraft Expired - Fee Related CN208530845U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820659166.8U CN208530845U (en) 2018-05-04 2018-05-04 Intelligent navigation steward system based on eight-rotary wing aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820659166.8U CN208530845U (en) 2018-05-04 2018-05-04 Intelligent navigation steward system based on eight-rotary wing aircraft

Publications (1)

Publication Number Publication Date
CN208530845U true CN208530845U (en) 2019-02-22

Family

ID=65393206

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201820659166.8U Expired - Fee Related CN208530845U (en) 2018-05-04 2018-05-04 Intelligent navigation steward system based on eight-rotary wing aircraft

Country Status (1)

Country Link
CN (1) CN208530845U (en)

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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: 20190222

Termination date: 20200504