CN215245527U

CN215245527U - Unmanned aerial vehicle for surveying and mapping

Info

Publication number: CN215245527U
Application number: CN202121643408.2U
Authority: CN
Inventors: 马嘉骏; 马英权; 郭昊滢
Original assignee: Shandong Binhai Technology Co ltd
Current assignee: Shandong Binhai Technology Co ltd
Priority date: 2021-07-20
Filing date: 2021-07-20
Publication date: 2021-12-21
Anticipated expiration: 2031-07-20

Abstract

The utility model discloses a survey and drawing unmanned aerial vehicle, which comprises a mounting bas, the top fixedly connected with unmanned aerial vehicle body of mount pad, the equal fixedly connected with telescopic support frame in bottom four corners of mount pad, the bottom fixedly connected with installed part of mount pad, the bottom fixedly connected with of support frame plays the piece, the outside swing joint that plays the piece has the supporting shoe, the inside of installed part is provided with fixing device, the bottom of mount pad is provided with the mapping lens, the top of mapping lens is provided with the rotating turret. The utility model discloses a cooperation setting between supporting shoe, play dropping block, damping spring and the shock pad can make the huge impact force of the in-process production of unmanned aerial vehicle body descending, cushions the reduction through damping spring and shock pad, when the impact force that the internal element that has significantly reduced received, also is showing the protective capacities who has improved the unmanned aerial vehicle body.

Description

Unmanned aerial vehicle for surveying and mapping

Technical Field

The utility model relates to a survey and drawing unmanned aerial vehicle technical field specifically is a survey and drawing unmanned aerial vehicle.

Background

The aerial survey of the unmanned aerial vehicle is powerful supplement of the traditional aerial photogrammetry means, has the characteristics of flexibility, high efficiency, rapidness, fineness, accuracy, low operation cost, wide application range, short production period and the like, has obvious advantages in the aspect of rapidly acquiring high-resolution images in small areas and areas with difficult flight, can be widely applied to the aspects of national major engineering construction, disaster emergency and treatment, territorial supervision, resource development, construction of new rural areas and small towns and the like, and particularly has wide prospects in the aspects of basic surveying and mapping, land resource investigation and monitoring, dynamic monitoring of land utilization, digital city construction, emergency disaster relief surveying and mapping data acquisition and the like.

However, current survey and drawing unmanned aerial vehicle collides with ground easily when descending, makes the internal member receive very big impact force, leads to unmanned aerial vehicle to break down, and the camera lens that unmanned aerial vehicle survey and drawing was used exposes externally when not using, receives the damage easily, increases the survey and drawing degree of difficulty, consequently needs a survey and drawing unmanned aerial vehicle to solve current problem now urgently.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a survey and drawing unmanned aerial vehicle is in order to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a survey and drawing unmanned aerial vehicle, includes the mount pad, the top fixedly connected with unmanned aerial vehicle body of mount pad, the equal fixedly connected with telescopic support frame in bottom four corners of mount pad, the bottom fixedly connected with installed part of mount pad, the bottom fixedly connected with of support frame plays the piece, the outside swing joint that plays the piece has the supporting shoe, the inside of installed part is provided with fixing device, the bottom of mount pad is provided with mapping lens, mapping lens's top is provided with the rotating turret.

Preferably, the bottom of mount pad is provided with the translucent cover, the equal fixedly connected with triangle fixture block in both sides of translucent cover.

Preferably, fixing device includes pressure spring, triangle fastener and limiting plate, the inside fixedly connected with pressure spring of installed part, one side fixedly connected with triangle fastener of pressure spring, the equal fixedly connected with limiting plate in both sides of triangle fastener, the joint between triangle fastener and the triangle fixture block.

Preferably, the outer part of the lifting block is fixedly connected with a fixing plate, and a damping spring is fixedly connected between the fixing plate and the supporting block.

Preferably, the inner bottom wall of the supporting block is fixedly connected with a shock pad, and the bottom of the supporting block is fixedly connected with an anti-abrasion pad.

Preferably, the inside swing joint of mount pad has the axis of rotation, fixedly connected with rubber packing ring between axis of rotation and the mount pad.

Compared with the prior art, the beneficial effects of the utility model are that:

1. the utility model discloses a cooperation setting between supporting shoe, play dropping block, damping spring and the shock pad can make the huge impact force of the in-process production of unmanned aerial vehicle body descending, cushions the reduction through damping spring and shock pad, when the impact force that the internal element that has significantly reduced received, also is showing the protective capacities who has improved the unmanned aerial vehicle body.

2. The utility model discloses a cooperation setting between fixing device, triangle fixture block and the translucent cover can protect internally mounted's mapping lens through the use of translucent cover, has both guaranteed mapping lens's safety, makes mapping lens when using again, keeps totally, is favorable to going on of plotting work.

Drawings

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

fig. 2 is a schematic front sectional view of the mounting base of the present invention;

FIG. 3 is a schematic view of a front cross-sectional structure of the middle support block of the present invention;

fig. 4 is an enlarged schematic structural diagram of a point a in fig. 2 according to the present invention.

In the figure: 1. a mounting seat; 2. an unmanned aerial vehicle body; 3. a support frame; 4. a mounting member; 5. lifting and dropping blocks; 6. a support block; 7. a fixing device; 701. a compression spring; 702. a triangular clamping piece; 703. a limiting plate; 8. a mapping lens; 9. a rotating frame; 10. a transparent cover; 11. a triangular clamping block; 12. a fixing plate; 13. a damping spring; 14. a shock pad; 15. an anti-wear pad; 16. a rotating shaft; 17. a rubber gasket.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Referring to fig. 1-4, the present invention provides an embodiment: the utility model provides a survey and drawing unmanned aerial vehicle, includes mount pad 1, the top fixedly connected with unmanned aerial vehicle body 2 of mount pad 1, the equal fixedly connected with telescopic support frame 3 in bottom four corners of mount pad 1, the bottom fixedly connected with installed part 4 of mount pad 1, the bottom fixedly connected with of support frame 3 plays the piece 5, and the outside swing joint of the piece 5 that rises and falls has supporting shoe 6, and the inside of installed part 4 is provided with fixing device 7, and the bottom of mount pad 1 is provided with mapping lens 8, mapping lens 8's top is provided with rotating turret 9, through fixing device 7's setting, can install translucent cover 10 on mount pad 1.

Further, the bottom of mount pad 1 is provided with translucent cover 10, and the equal fixedly connected with triangle fixture block 11 in both sides of translucent cover 10 sets up through the cooperation between translucent cover 10 and the triangle fixture block 11, can avoid mapping lens 8 to receive the damage, leads to follow-up mapping work to go on unable.

Further, fixing device 7 includes pressure spring 701, triangle fastener 702 and limiting plate 703, and the inside fixedly connected with pressure spring 701 of installed part 4, one side fixedly connected with triangle fastener 702 of pressure spring 701, the equal fixedly connected with limiting plate 703 in both sides of triangle fastener 702, joint between triangle fastener 702 and the triangle fixture block 11, through the cooperation setting between pressure spring 701, triangle fastener 702, the limiting plate 703, can make translucent cover 10 be convenient for installation and dismantlement.

Further, the outside fixedly connected with fixed plate 12 of landing gear piece 5, fixedly connected with damping spring 13 between fixed plate 12 and the supporting shoe 6, through damping spring 13's setting, can be to the impact force that unmanned aerial vehicle body 2 produced at the descending in-process, the dissipation of contact avoids the internal element to receive the impact and damage.

Further, the inner bottom wall fixedly connected with shock pad 14 of supporting shoe 6, the bottom fixedly connected with abrasionproof pad 15 of supporting shoe 6, through the setting of abrasionproof pad 15, can protect supporting shoe 6.

Further, the inside swing joint of mount pad 1 has axis of rotation 16, and fixedly connected with rubber packing ring 17 between axis of rotation 16 and the mount pad 1 through rubber packing ring 17's setting, can protect mapping lens 8, avoids it to receive the impact force that the descending produced and damages.

The working principle is as follows: when unmanned aerial vehicle body 2 descends, supporting shoe 6 of 3 bottom installations of support frame contacts ground earlier, the impact force of 2 descending productions of unmanned aerial vehicle body, by damping spring 13 and the 14 contact dissipation of shock pad of supporting shoe 6 inside, make the steady descending of unmanned aerial vehicle body 2, do not cause the impact to internal element, when needing to change translucent cover 10, remove limiting plate 703, make triangle fixture block 11 and triangle fastener 702 separately, can take off it and change, protect the safety of the inside mapping lens 8 of translucent cover 10.

It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Claims

1. A survey and drawing unmanned aerial vehicle, includes mount pad (1), its characterized in that: the utility model discloses an unmanned aerial vehicle, including mount pad (1), the top fixedly connected with unmanned aerial vehicle body (2) of mount pad (1), the equal fixedly connected with telescopic support frame (3) in bottom four corners of mount pad (1), the bottom fixedly connected with installed part (4) of mount pad (1), the bottom fixedly connected with of support frame (3) plays piece (5), the outside swing joint that plays piece (5) has supporting shoe (6), the inside of installed part (4) is provided with fixing device (7), the bottom of mount pad (1) is provided with mapping lens (8), the top of mapping lens (8) is provided with rotating turret (9).

2. A mapping drone according to claim 1, characterised in that: the bottom of mount pad (1) is provided with translucent cover (10), equal fixedly connected with triangle fixture block (11) in both sides of translucent cover (10).

3. A mapping drone according to claim 1, characterised in that: fixing device (7) are including pressure spring (701), triangle fastener (702) and limiting plate (703), the inside fixedly connected with pressure spring (701) of installed part (4), one side fixedly connected with triangle fastener (702) of pressure spring (701), the equal fixedly connected with limiting plate (703) in both sides of triangle fastener (702), joint between triangle fastener (702) and triangle fixture block (11).

4. A mapping drone according to claim 1, characterised in that: the outer part of the lifting block (5) is fixedly connected with a fixing plate (12), and a damping spring (13) is fixedly connected between the fixing plate (12) and the supporting block (6).

5. A mapping drone according to claim 1, characterised in that: the inner bottom wall of the supporting block (6) is fixedly connected with a shock pad (14), and the bottom of the supporting block (6) is fixedly connected with an anti-abrasion pad (15).

6. A mapping drone according to claim 1, characterised in that: the inner part of the mounting seat (1) is movably connected with a rotating shaft (16), and a rubber gasket (17) is fixedly connected between the rotating shaft (16) and the mounting seat (1).