CN216332787U - Unmanned aerial vehicle carries thing case and unmanned aerial vehicle thereof - Google Patents

Unmanned aerial vehicle carries thing case and unmanned aerial vehicle thereof Download PDF

Info

Publication number
CN216332787U
CN216332787U CN202123324939.8U CN202123324939U CN216332787U CN 216332787 U CN216332787 U CN 216332787U CN 202123324939 U CN202123324939 U CN 202123324939U CN 216332787 U CN216332787 U CN 216332787U
Authority
CN
China
Prior art keywords
unmanned aerial
aerial vehicle
case
vehicle carrier
carrier case
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202123324939.8U
Other languages
Chinese (zh)
Inventor
李勇
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhongshan Huaao Yihang Technology Co ltd
Original Assignee
Zhongshan Huaao Yihang Technology Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zhongshan Huaao Yihang Technology Co ltd filed Critical Zhongshan Huaao Yihang Technology Co ltd
Priority to CN202123324939.8U priority Critical patent/CN216332787U/en
Application granted granted Critical
Publication of CN216332787U publication Critical patent/CN216332787U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • 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
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries

Landscapes

  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

The utility model provides an unmanned aerial vehicle carrying case which comprises a carrying case shell, wherein a first accommodating space is arranged in the middle of the carrying case shell, battery bins are arranged on two sides of the first accommodating space, a hanging part used for connecting articles to be carried is arranged at the top of the first accommodating space, and a detachable connecting structure connected with an unmanned aerial vehicle main body is arranged at the top of the carrying case shell. The unmanned aerial vehicle carrying box has the advantages of being capable of being rapidly disassembled or assembled, convenient to store and the like.

Description

Unmanned aerial vehicle carries thing case and unmanned aerial vehicle thereof
Technical Field
The utility model relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle carrying box.
Background
Unmanned aerial vehicles, i.e. unmanned aerial vehicles controlled by radio remote control or by their own programs. The method is widely applied to various fields such as agriculture, military, photography and the like. At the present stage, more and more unmanned aerial vehicles have the thing function of carrying. But the unmanned aerial vehicle that has the thing function at present carries thing case and unmanned aerial vehicle main part and can't dismantle, and inconvenient accomodating is carried.
SUMMERY OF THE UTILITY MODEL
The present invention is directed to solving at least one of the problems of the prior art. The utility model provides an unmanned aerial vehicle carrying box and an unmanned aerial vehicle thereof.
According to an embodiment of the utility model, the unmanned aerial vehicle carrying box comprises a carrying box shell, wherein a first accommodating space is arranged in the middle of the carrying box shell, battery bins are arranged on two sides of the first accommodating space, a hanging part used for connecting articles to be carried is arranged at the top of the first accommodating space, and a connecting structure which is connected with an unmanned aerial vehicle main body and can be detached is arranged at the top of the carrying box shell.
According to some embodiments of the present invention, the connecting structure includes a first connecting portion and a second connecting portion, the first connecting portion is provided with a first connecting groove, the second connecting portion is provided with a second connecting groove, and the first connecting portion is further provided with a clamping opening.
According to some embodiments of the utility model, the mounting portion is provided with a round hole or a threaded hole.
According to some embodiments of the utility model, the inside of the front wall of the carrier box housing is provided with a mounting table for mounting a distance measuring sensor, and the front wall of the carrier box housing is provided with a through hole.
According to some embodiments of the present invention, a second receiving space for mounting the circuit board is provided at a rear side of the carrier case housing, and the second receiving space is communicated with the first receiving space.
According to some embodiments of the utility model, the carrier housing is provided with a wiring hole.
According to some embodiments of the utility model, a wire guard is provided behind the connection structure.
According to some embodiments of the utility model, the side wall of the battery compartment is provided with a plurality of hollows.
According to some embodiments of the utility model, the carrier case housing and the battery compartment are made of carbon fiber nylon.
The utility model also provides an unmanned aerial vehicle, which comprises the unmanned aerial vehicle carrying box.
The utility model has at least the following technical effects:
1. according to the unmanned aerial vehicle carrying box disclosed by the embodiment of the utility model, the detachable connecting structure is arranged, so that the unmanned aerial vehicle carrying box and the unmanned aerial vehicle main body can be rapidly detached and assembled, and the unmanned aerial vehicle carrying box is convenient to store and carry.
2. According to the unmanned aerial vehicle carrying box disclosed by the embodiment of the utility model, the side wall of the battery compartment is provided with a plurality of hollows. Be favorable to reducing unmanned aerial vehicle's whole weight, make unmanned aerial vehicle lighter, the flight is faster.
Drawings
FIG. 1 is a schematic overall view from a first perspective of an embodiment of the present invention;
FIG. 2 is a schematic overall second perspective view of an embodiment of the present invention;
FIG. 3 is a schematic overall third perspective view of an embodiment of the present invention.
Reference numerals: the luggage box comprises a luggage box shell 100, a first accommodating space 110, a hanging part 111, a through hole 120, a wiring hole 130, a battery bin 200, a hollow part 210, a connecting structure 300, a first connecting part 310, a first connecting groove 311, a clamping interface 312, a second connecting part 320, a second connecting groove 321, a mounting table 400, a second accommodating space 500 and a wire protection part 600.
Detailed Description
The following description is provided with reference to the accompanying drawings to assist in a comprehensive understanding of various embodiments of the disclosure as defined by the claims and their equivalents. The description includes various specific details to aid understanding, but such details are to be regarded as exemplary only. Accordingly, those of ordinary skill in the art will recognize that various changes and modifications of the various embodiments described herein can be made without departing from the scope and spirit of the present disclosure. Moreover, descriptions of well-known functions and constructions may be omitted for clarity and conciseness.
The terms and words used in the following description and claims are not limited to the literal meanings, but are used by the inventors to enable a clear and consistent understanding of the disclosure. Accordingly, it will be apparent to those skilled in the art that the following descriptions of the various embodiments of the present disclosure are provided for illustration only and not for the purpose of limiting the disclosure as defined by the appended claims and their equivalents.
It is to be understood that the singular forms "a", "an" and "the" include plural referents unless the context clearly dictates otherwise. Thus, for example, reference to "a component surface" includes reference to one or more of such surfaces.
The terms "having," "may have," "including," or "may include" used in various embodiments of the present disclosure indicate the presence of the respective functions, operations, elements, etc., disclosed, but do not limit additional one or more functions, operations, elements, etc.
Furthermore, it is to be understood that the terms "comprises" or "comprising," when used in various embodiments of the present disclosure, are intended to specify the presence of stated features, integers, operations, elements, components, or groups thereof, but do not preclude the presence or addition of one or more other features, integers, operations, elements, components, or groups thereof.
As shown in fig. 1 to 3, the utility model provides an unmanned aerial vehicle carrier case, which comprises a carrier case casing 100, wherein a first accommodating space 110 is arranged in the middle of the carrier case casing 100, battery compartments 200 are arranged on both sides of the first accommodating space 110, a mounting part 111 for connecting articles to be carried is arranged at the top of the first accommodating space 110, and a connecting structure 300 which is connected with and detachable from an unmanned aerial vehicle main body is arranged at the top of the carrier case casing 100. Through setting up detachable connection structure 300, make unmanned aerial vehicle carry thing case and unmanned aerial vehicle main part can dismantle fast and assemble, conveniently accomodate and carry. Waiting to transport article accessible mount 111 and hanging on unmanned aerial vehicle, first accommodation space 110 is used for holding waiting to transport article, and the battery compartment 200 of first accommodation space 110 both sides all loads the battery, makes unmanned aerial vehicle electric power sufficient, and flight time lasts longer, and the flight distance is farther. In addition, the battery compartment 200 of thing case casing 100 both sides can be the symmetry setting, makes unmanned aerial vehicle's fuselage weight more balanced like this, and the flight is more steady.
As shown in fig. 1 and 2, in some embodiments, the connection structure 300 includes a first connection portion 310 and a second connection portion 320, the first connection portion 310 is provided with a first connection groove 311, the second connection portion 320 is provided with a second connection groove 321, and the first connection portion 310 is further provided with a card interface 312. Through first connecting groove 311 and second connecting groove 321 and joint interface 312 and unmanned aerial vehicle main part joint, convenient dismantlement or equipment.
As shown in fig. 3, in some embodiments, mounting portion 111 is provided with a round hole or a threaded hole. When the mounting part 111 is provided with the round hole, the carried article is provided with a column body matched with the round hole, and the carried article can be mounted on the carrying box by inserting the column body into the round hole; when the mounting portion 111 is provided with the threaded hole, the article to be mounted is provided with a screw rod matched with the threaded hole, and the article to be mounted can be mounted on the carrying box by screwing the screw rod into the threaded hole. Just so firmly be connected carried article and year thing case, prevent that carried article from taking place to rock at unmanned aerial vehicle flight in-process, be favorable to keeping unmanned aerial vehicle's stationarity.
As shown in fig. 1 and 3, in some embodiments, an installation stage 400 for installing a distance measuring sensor is provided on the inner side of the front wall of the carrier case housing 100, and the through hole 120 is provided on the front wall of the carrier case housing 100. For example, the distance measuring sensor may be a laser sensor, and after the laser sensor is mounted, the laser probe is located at the through hole 120. The laser sensor can accurately measure the distance from the unmanned aerial vehicle to the target or the obstacle.
As shown in fig. 2, in some embodiments, a second receiving space 500 for mounting a circuit board is provided at the rear side of the carrier case 100, and the second receiving space 500 is communicated with the first receiving space 110. The second accommodating space 500 is used for accommodating a circuit board, and specifically, a plurality of fixing columns are arranged in the second accommodating space 500, and the circuit board is fixedly connected with the fixing columns through screws.
In some embodiments, as shown in fig. 3, the carrier housing 100 is provided with a wiring aperture 130. Walk line hole 130 and conveniently walk the line, specifically, walk line hole 130 and set up directly over second accommodation space 500, make unmanned aerial vehicle structure compacter, make the whole volume of unmanned aerial vehicle littleer.
As shown in fig. 1, in some embodiments, a wire guard 600 is disposed rearward of the connection structure 300. The wire guard 600 is used for covering the naked electric wire in unmanned aerial vehicle surface, is favorable to prolonging unmanned aerial vehicle's life.
As shown in fig. 1, in some embodiments, the battery compartment 200 has a plurality of openings 210 formed in the sidewall thereof. Fretwork 210 can reduce unmanned aerial vehicle's whole weight, makes unmanned aerial vehicle lighter, and flight speed is faster. In addition, the hollow 210 also helps to dissipate heat, preventing the temperature of the battery from being too high. The junction of the front of the battery compartment 200 and the carrier case housing 100 is streamlined. Reduce air resistance, make unmanned aerial vehicle airspeed faster.
As shown in fig. 1, in some embodiments, the carrier housing 100 and the battery compartment 200 are both made of carbon fiber nylon. The casing 100 and the battery compartment 200 quality of carbon fiber nylon material are light, are favorable to improving unmanned aerial vehicle's airspeed.
The utility model also provides an unmanned aerial vehicle which comprises the unmanned aerial vehicle carrying box. This unmanned aerial vehicle has advantages such as convenient dismantlement is accomodate, the quality is light, flying speed is fast.
The foregoing is a more detailed description of the present invention that is presented in conjunction with specific embodiments, and the practice of the utility model is not to be considered limited to those descriptions. It will be apparent to those skilled in the art that a number of simple derivations or substitutions can be made without departing from the inventive concept.

Claims (10)

1. Unmanned aerial vehicle carries thing case, its characterized in that: including carrying case casing (100), be provided with first accommodation space (110) in the middle of carrying case casing (100), the both sides of first accommodation space (110) all are provided with battery compartment (200), the top of first accommodation space (110) is provided with and is used for connecting carry-on portion (111) of waiting to carry on article, the top of carrying case casing (100) is provided with and is connected and detachable connection structure (300) with the unmanned aerial vehicle main part.
2. The unmanned aerial vehicle carrier case of claim 1, wherein: connection structure (300) include first connecting portion (310) and second connecting portion (320), be provided with first connecting groove (311) on first connecting portion (310), be provided with second connecting groove (321) on second connecting portion (320), still be provided with joint interface (312) on first connecting portion (310).
3. The unmanned aerial vehicle carrier case of claim 1, wherein: the mounting part (111) is provided with a round hole or a threaded hole.
4. The unmanned aerial vehicle carrier case of claim 1, wherein: the inboard of the antetheca of thing case casing (100) is provided with mount table (400) that are used for installing range finding sensor, be provided with through-hole (120) on the antetheca of thing case casing (100).
5. The unmanned aerial vehicle carrier case of claim 1, wherein: the rear side of the luggage box shell (100) is provided with a second accommodating space (500) for installing a circuit board, and the second accommodating space (500) is communicated with the first accommodating space (110).
6. An unmanned aerial vehicle carrier case of claim 5, wherein: the luggage carrier shell (100) is provided with a wiring hole (130).
7. The unmanned aerial vehicle carrier case of claim 1, wherein: and a wire protecting part (600) is arranged behind the connecting structure (300).
8. The unmanned aerial vehicle carrier case of claim 1, wherein: the side wall of the battery bin (200) is provided with a plurality of hollows (210).
9. The unmanned aerial vehicle carrier case of claim 1, wherein: the carrier case shell (100) and the battery compartment (200) are made of carbon fiber nylon materials.
10. Unmanned aerial vehicle, its characterized in that: comprising the unmanned aerial vehicle carrier box of any of claims 1-9.
CN202123324939.8U 2021-12-24 2021-12-24 Unmanned aerial vehicle carries thing case and unmanned aerial vehicle thereof Active CN216332787U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202123324939.8U CN216332787U (en) 2021-12-24 2021-12-24 Unmanned aerial vehicle carries thing case and unmanned aerial vehicle thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202123324939.8U CN216332787U (en) 2021-12-24 2021-12-24 Unmanned aerial vehicle carries thing case and unmanned aerial vehicle thereof

Publications (1)

Publication Number Publication Date
CN216332787U true CN216332787U (en) 2022-04-19

Family

ID=81166187

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202123324939.8U Active CN216332787U (en) 2021-12-24 2021-12-24 Unmanned aerial vehicle carries thing case and unmanned aerial vehicle thereof

Country Status (1)

Country Link
CN (1) CN216332787U (en)

Similar Documents

Publication Publication Date Title
US8256715B2 (en) Devices, systems and methods for modular payload integration for unmanned aerial vehicles
US8873238B2 (en) Chassis system and method for holding and protecting electronic modules
US7885056B2 (en) Center instrument pedestal display
US9600028B2 (en) Enclosures for protecting devices and methods of manufacturing enclosures for protecting devices
US20170036748A1 (en) Unmanned aerial vehicle
US9357111B2 (en) Casing
CN216332787U (en) Unmanned aerial vehicle carries thing case and unmanned aerial vehicle thereof
US20190016460A1 (en) Unmanned aerial vehicle
US20020011106A1 (en) Compact inertial measurement unit
US10401136B1 (en) Radio frequency tracking system for projectiles
CN211926880U (en) Inertia measurement module and unmanned aerial vehicle
WO2019100313A1 (en) Unmanned aerial vehicle and avionics system therefor
US20100085695A1 (en) Aircraft Canister Design
US8711557B2 (en) Support tray for server
CN206466169U (en) A kind of rotor wing unmanned aerial vehicle
EP2373950B1 (en) Multi-purpose mounting devices for mounting electrical packages to airborne objects
CN206618857U (en) A kind of unmanned plane prevention and control rifle
CN111731465A (en) Fuselage frame rack construction and unmanned aerial vehicle for unmanned aerial vehicle
US20180354655A1 (en) Test Module Fixture for Aerial Vehicle Module
CN204945804U (en) A kind of unmanned plane robot pilot
CN210822802U (en) Load suspension device for unmanned aerial vehicle to acquire ground coordinates
US20210237869A1 (en) Unmanned aerial vehicle
GB2591212A (en) Methods and assemblies for mounting equipment to an aircraft fuselage
CN202256301U (en) Gas analysis detection probe capable of realizing long-range emission and gas detection device
US11115569B1 (en) Ruggedized camera system for aerospace environments

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant