CN210503187U

CN210503187U - Unmanned aerial vehicle for air monitering

Info

Publication number: CN210503187U
Application number: CN201920869627.9U
Authority: CN
Inventors: 吉丽珠
Original assignee: Hainan Xingmeng Technology Co Ltd
Current assignee: Hainan Xingmeng Technology Co Ltd
Priority date: 2019-06-11
Filing date: 2019-06-11
Publication date: 2020-05-12
Anticipated expiration: 2029-06-11

Abstract

The utility model relates to an unmanned air vehicle technique field just discloses an unmanned aerial vehicle for air monitering, including the unmanned aerial vehicle body, four rotation grooves, four have been seted up in the outside of unmanned aerial vehicle body it has joint support bar, four all to articulate in the rotation groove the one end that the unmanned aerial vehicle body was kept away from to joint support bar all extends to the outside of unmanned aerial vehicle body. The utility model discloses a, thereby hold the frame through the operation and pull down the air monitor body, because the folding wing can rotate, be convenient for accomodate the inside that gets into the groove of accomodating with folding wing and perpendicular screw, it is articulated with this internal rotation groove of seting up of unmanned aerial vehicle through joint support pole, it is convenient with joint support pole folding down, thereby fold the unmanned aerial vehicle body, through accomodating to folding wing and perpendicular screw, make and to protect it when carrying and storing, reduce whole occupation of land volume simultaneously, convenient to use person's carrying and use.

Description

Unmanned aerial vehicle for air monitering

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle for air monitering.

Background

The unmanned plane is called unmanned plane for short, and is called UAV in English for short, and is an unmanned plane operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and the unmanned plane + industry application is really just needed for the unmanned plane in civil aspects; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded.

Along with the development of science and technology, unmanned aerial vehicle also uses in the air monitering field, but when using unmanned aerial vehicle, because the safety restriction of size and part for unmanned aerial vehicle's carrying is a trouble, is unfavorable for user's operation when retrieving storage to unmanned aerial vehicle, influences user's use, so proposed an air monitering and use unmanned aerial vehicle to solve above-mentioned problem.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

Not enough to prior art, the utility model provides an unmanned aerial vehicle for air monitering possesses advantages such as collapsible, has solved when using unmanned aerial vehicle, because the safety restriction of size and part for unmanned aerial vehicle's carrying is a trouble, is unfavorable for user's operation when retrieving storage to unmanned aerial vehicle, influences user's the problem of use.

(II) technical scheme

In order to realize the folding purpose, the utility model provides a following technical scheme: an unmanned aerial vehicle for air monitoring comprises an unmanned aerial vehicle body, wherein four rotating grooves are formed in the outer side of the unmanned aerial vehicle body, connecting support rods are hinged in the four rotating grooves, one ends, away from the unmanned aerial vehicle body, of the four connecting support rods extend to the outer side of the unmanned aerial vehicle body, storage grooves are formed in the four connecting support rods along the horizontal direction, one sides, away from the unmanned aerial vehicle body, of the four storage grooves respectively penetrate through and extend to the outer sides of the four connecting support rods, folding wings are hinged to the inner sides of the four storage grooves, vertical propellers are hinged to the top ends of the four folding wings, the bottom of unmanned aerial vehicle body is provided with and holds the frame, the top that holds the frame articulates there are four telescopic links, four the top of telescopic link is articulated with four joint support poles respectively, the top fixed mounting that holds the frame has the air monitor body.

Preferably, hold the frame and include braced frame, two slide bars, two draw slips and two threaded rods, four the bottom of telescopic link all with braced frame fixed connection, two the slide bar be located braced frame's top and with braced frame fixed connection, two the slide bar respectively with two slide bar sliding connection, two the top of slide all with the bottom fixed connection of air monitor body, two the threaded rod is located one side that two slide bars kept away from mutually respectively and respectively with two slide bar threaded connection, two the threaded rod is close to the one end of slide bar and runs through two slide bars and two slide bars respectively in proper order and extend to the one side that two slide bars are close to mutually.

Preferably, the bottom end of the supporting frame is fixedly connected with fixing blocks which are uniformly distributed, and the bottom end of each fixing block is fixedly connected with a rubber pad.

Preferably, four equal joint in one side of joint support pole has the U-shaped fixture block, four the U-shaped fixture block is located four outsides of accomodating the groove respectively, four one side that the U-shaped fixture block is close to the groove of accomodating runs through the inside of accomodating the groove and contacts with folding wing.

Preferably, four two cotter ways have all been seted up to the one end that joint support pole is close to the unmanned aerial vehicle body, peg graft on the top of unmanned aerial vehicle body has four pins, four the bottom of pin runs through the cotter way on unmanned aerial vehicle body, four rotation grooves and four joint support pole tops in proper order and pegs graft with the cotter way on four joint support pole tops respectively.

Preferably, the bottom fixedly connected with of unmanned aerial vehicle body keeps apart the abrasionproof pad, keep apart the bottom and the air monitor body contact of abrasionproof pad.

(III) advantageous effects

Compared with the prior art, the utility model provides an unmanned aerial vehicle for air monitering possesses following beneficial effect:

1. this unmanned aerial vehicle for air monitering, thereby hold the frame through the operation and pull down the air monitor body, through will lift off with the U-shaped fixture block of joint support pole joint, thereby make folding wing can rotate, be convenient for accomodate folding wing and perpendicular screw and get into the inside of accomodating the groove, then it is articulated to extract the round pin pole and pass through this internal rotation groove of seting up of joint support pole and unmanned aerial vehicle, it is convenient to fold joint support pole down, because the telescopic pole has the elasticity and is convenient for will hold the frame and put into between four joint support poles, thereby fold the unmanned aerial vehicle body, through accomodating of fifty percent discount folding wing and perpendicular screw, make and can protect it when carrying and storing, reduce whole occupation of land volume simultaneously, convenient to use person's carrying and use.

2. This unmanned aerial vehicle for air monitering loosens the threaded rod through rotating, conveniently with the draw runner roll-off in the slide bar to drive the air monitor body and dismantle from braced frame, simple structure, convenient to use person is favorable to user to its maintenance and use to the dismouting of air monitor body, and fixed block and the rubber pad through the braced frame bottom make things convenient for unmanned aerial vehicle's descending, vibrations and wearing and tearing when reducing unmanned aerial vehicle descending.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic view of the connection structure of the U-shaped fixture block and the connecting support rod of the present invention;

fig. 3 is an enlarged schematic view of a portion a in fig. 1 according to the present invention.

In the figure: 1. an unmanned aerial vehicle body; 2. a rotating groove; 3. connecting the supporting rods; 4. a receiving groove; 5. folding the wings; 6. a vertical propeller; 7. a containing rack; 701. a support frame; 702. a chute rod; 703. a slide bar; 704. a threaded rod; 8. a telescopic rod; 9. an air monitor body; 10. a fixed block; 11. a U-shaped clamping block; 12. a pin slot; 13. a pin rod; 14. an isolated wear pad.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-3, an unmanned aerial vehicle for air monitoring comprises an unmanned aerial vehicle body 1, four rotating grooves 2 are formed in the outer side of the unmanned aerial vehicle body 1, connecting support rods 3 are hinged in the four rotating grooves 2, one ends of the four connecting support rods 3, which are far away from the unmanned aerial vehicle body 1, extend to the outer side of the unmanned aerial vehicle body 1, accommodating grooves 4 are formed in the four connecting support rods 3 along the horizontal direction, one sides of the four accommodating grooves 4, which are far away from the unmanned aerial vehicle body 1, respectively penetrate through and extend to the outer sides of the four connecting support rods 3, folding wings 5 are hinged on the inner sides of the four accommodating grooves 4, vertical propellers 6 are hinged on the top ends of the four folding wings 5, a containing frame 7 is arranged at the bottom end of the unmanned aerial vehicle body 1, four telescopic rods 8 are hinged on the top end of the containing frame 7, the top ends of the four telescopic rods, hold frame 7 through the operation thereby pull down air monitor body 9, through will lift off with the U-shaped fixture block 11 of joint support rod 3 joint, thereby make folding wing 5 can rotate, be convenient for accomodate folding wing 5 and perpendicular screw 6 and get into the inside of accomodating groove 4, then extract pin pole 13 and set up rotation groove 2 articulated in connecting support rod 3 and the unmanned aerial vehicle body 1, it is convenient with the folding down of joint support rod 3, because telescopic link 8 has the elasticity and be convenient for will hold frame 7 and put into between four connecting support rod 3, thereby fold unmanned aerial vehicle body 1, through accomodating to folding wing 5 and perpendicular screw 6, make and to protect it when carrying and storing, reduce whole occupation of land volume simultaneously, convenient to use person's carrying and use.

Further, the containing frame 7 includes a supporting frame 701, two sliding rods 702, two sliding bars 703 and two threaded rods 704, the bottom ends of the four telescopic rods 8 are all fixedly connected with the supporting frame 701, the two sliding rods 702 are located at the top end of the supporting frame 701 and fixedly connected with the supporting frame 701, the two sliding bars 703 are respectively slidably connected with the two sliding rods 702, the top ends of the two sliding bars 703 are respectively fixedly connected with the bottom end of the air monitor body 9, the two threaded rods 704 are respectively located at the far side of the two sliding rods 702 and respectively in threaded connection with the two sliding rods 702, one end of the two threaded rods 704 close to the sliding rods 702 sequentially penetrates through the two sliding rods 702 and the two sliding rods 703 and extends to the near side of the two sliding rods 702, the threaded rods 704 are loosened by rotation, the sliding bars 703 in the sliding rods 702 are conveniently slid out, so as to drive the air monitor body 9 to be detached from the supporting frame 701, simple structure, the dismouting of convenient to use person to air monitor body 9 is favorable to the user to its maintenance and use.

Further, braced frame 701's bottom fixedly connected with evenly distributed's fixed block 10, the bottom fixedly connected with rubber pad of fixed block 10, fixed block 10 and the rubber pad through braced frame 701 bottom make things convenient for unmanned aerial vehicle's descending, vibrations and wearing and tearing when reducing unmanned aerial vehicle and descending.

Further, four equal joints in one side of joint support pole 3 have U-shaped fixture block 11, and four U-shaped fixture blocks 11 are located four outsides of accomodating groove 4 respectively, and four U-shaped fixture blocks 11 are close to one side of accomodating groove 4 and run through the inside of accomodating groove 4 and contact with folding wing 5, through the joint of U-shaped fixture block 11 with joint support pole 3 to restriction joint support pole 3's rotation, because U-shaped fixture block 11 and joint support pole 3 contact, further fix it.

Further, two cotter way 12 have all been seted up to four joint support pole 3 one end that is close to unmanned aerial vehicle body 1, it has four pins 13 to peg graft on the top of unmanned aerial vehicle body 1, unmanned aerial vehicle body 1 is run through in proper order to four pins 13's bottom, four rotate the cotter way 12 on groove 2 and four joint support pole 3 tops and peg graft with the cotter way 12 on four joint support pole 3 tops respectively, through four pins 13 and eight cotter way 12's grafting cooperation, restriction joint support pole 3's rotation, thereby fix joint support pole 3.

Further, the bottom fixedly connected with of unmanned aerial vehicle body 1 keeps apart abrasionproof pad 14, keeps apart the bottom and the contact of air monitor body 9 of abrasionproof pad 14, through keeping apart 14 bottoms of abrasionproof pads and the contact of air monitor body 9, prevents that telescopic link 8 from freely stretching out and drawing back, avoids air monitor body 9 and the contact of unmanned aerial vehicle body 1 simultaneously, causes wearing and tearing.

The working principle is as follows: hold frame 7 through the operation thereby pull down air monitor body 9, through will lift off with the U-shaped fixture block 11 of joint support rod 3 joint, thereby make folding wing 5 can rotate, be convenient for accomodate folding wing 5 and perpendicular screw 6 and get into the inside of accomodating groove 4, then extract pin pole 13 and set up rotation groove 2 articulated in connecting support rod 3 and the unmanned aerial vehicle body 1, it is convenient with the folding down of joint support rod 3, because telescopic link 8 has the elasticity and be convenient for will hold frame 7 and put into between four connecting support rod 3, thereby fold unmanned aerial vehicle body 1, through accomodating to folding wing 5 and perpendicular screw 6, make and to protect it when carrying and storing, reduce whole occupation of land volume simultaneously, convenient to use person's carrying and use.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an unmanned aerial vehicle for air monitering, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle is characterized in that four rotating grooves (2) are formed in the outer side of the unmanned aerial vehicle body (1), connecting support rods (3) are hinged in the four rotating grooves (2), one ends, far away from the unmanned aerial vehicle body (1), of the connecting support rods (3) extend to the outer side of the unmanned aerial vehicle body (1), storage grooves (4) are formed in the four connecting support rods (3) in the horizontal direction, one sides, far away from the unmanned aerial vehicle body (1), of the storage grooves (4) penetrate through and extend to the outer sides of the four connecting support rods (3) respectively, folding wings (5) are hinged to the inner sides of the four storage grooves (4), vertical propellers (6) are hinged to the top ends of the four folding wings (5), a storage frame (7) is arranged at the bottom end of the unmanned aerial vehicle body (1), and four telescopic rods (8) are hinged to the top end of the, four the top of telescopic link (8) is articulated with four joint support poles (3) respectively, the top fixed mounting who holds frame (7) has air monitor body (9).

2. The unmanned aerial vehicle for air monitoring of claim 1, wherein: the containing frame (7) comprises a supporting frame (701), two sliding track rods (702), two sliding strips (703) and two threaded rods (704), the bottom ends of the four telescopic rods (8) are fixedly connected with the supporting frame (701), the two sliding track rods (702) are positioned at the top end of the supporting frame (701) and fixedly connected with the supporting frame (701), the two sliding strips (703) are respectively in sliding connection with the two sliding track rods (702), two the top of draw runner (703) all with the bottom fixed connection of air monitor body (9), two threaded rod (704) are located one side that two slide bar (702) kept away from mutually respectively and respectively with two slide bar (702) threaded connection, two one end that threaded rod (704) are close to slide bar (702) runs through two slide bar (702) and two draw runner (703) respectively in proper order and extends to one side that two slide bar (702) are close to mutually.

3. The unmanned aerial vehicle for air monitoring of claim 2, wherein: the bottom fixedly connected with of braced frame (701) evenly distributed fixed block (10), the bottom fixedly connected with rubber pad of fixed block (10).

4. The unmanned aerial vehicle for air monitoring of claim 1, wherein: four equal joint in one side of joint support pole (3) has U-shaped fixture block (11), four U-shaped fixture block (11) are located four outsides of accomodating groove (4) respectively, four one side that U-shaped fixture block (11) are close to accomodating groove (4) runs through the inside of accomodating groove (4) and contacts with folding wing (5).

5. The unmanned aerial vehicle for air monitoring of claim 1, wherein: four two cotter way (12) have all been seted up to the one end that joint support pole (3) are close to unmanned aerial vehicle body (1), peg graft on the top of unmanned aerial vehicle body (1) has four cotter bar (13), four the bottom of cotter bar (13) runs through in proper order unmanned aerial vehicle body (1), four rotates cotter way (12) on groove (2) and four joint support pole (3) tops and pegs graft with cotter way (12) on four joint support pole (3) tops respectively.

6. The unmanned aerial vehicle for air monitoring of claim 1, wherein: the bottom fixedly connected with of unmanned aerial vehicle body (1) keeps apart abrasionproof pad (14), keep apart the bottom and the air monitor body (9) contact of abrasionproof pad (14).