CN217348242U - Modeling scanning device for unmanned aerial vehicle for territorial space planning - Google Patents

Modeling scanning device for unmanned aerial vehicle for territorial space planning Download PDF

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Publication number
CN217348242U
CN217348242U CN202220072355.1U CN202220072355U CN217348242U CN 217348242 U CN217348242 U CN 217348242U CN 202220072355 U CN202220072355 U CN 202220072355U CN 217348242 U CN217348242 U CN 217348242U
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aerial vehicle
unmanned aerial
scanning device
main part
supporting
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CN202220072355.1U
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Chinese (zh)
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谢伟杰
江琳英
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Fujian Fangyuan Survey And Planning Co ltd
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Fujian Fangyuan Survey And Planning Co ltd
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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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Abstract

The utility model discloses a state soil space planning unmanned aerial vehicle scanning device that models, comprising a main body, branch and supporting shoe, the wing is all installed to four corners on main part top, the battery is installed to the one end of main part, the top of main part is provided with energy-conserving structure, the supporting shoe is installed to the bottom of main part, the bottom of supporting shoe is provided with the connecting block, and the bottom of connecting block installs the camera, the both sides of supporting shoe all are provided with the dismouting structure, branch is all installed to four corners of main part bottom, the bottom of branch all is provided with buffer structure, buffer structure is including expanding spring, the supporting legs, the gag lever post, stopper and spacing groove. The utility model discloses an at the rotatory handle of supporting shoe both sides installation, rotate and revolve the handle, the screw rod drives splint and removes the fixed restriction of splint to the connecting block along the direction of preformed hole, alright take off the camera from the bottom of supporting shoe, realize the purpose of changing the camera.

Description

Modeling scanning device for unmanned aerial vehicle for territorial space planning
Technical Field
The utility model relates to an unmanned aerial vehicle model building scanning technical field, in particular to national soil space planning unmanned aerial vehicle scanning device that models.
Background
Along with the continuous improvement of economic level, the continuous development of science and technology, the planning of homeland space also becomes especially important, at the in-process of homeland space planning, need carry out a large amount of information acquisition to the homeland position through the collection camera of remote information transmission to unmanned aerial vehicle modeling scanning device's remote control through the staff.
The prior art scheme has the weak point, and unmanned aerial vehicle scanning device that models is not convenient for the dismouting, is not convenient for dismantle the camera get off and change, influences the use of camera to a certain extent, has reduced unmanned aerial vehicle scanning device that models's work efficiency.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
The utility model aims at providing a homeland space planning unmanned aerial vehicle scanning device that models for solve the defect of the dismouting of being not convenient for of current unmanned aerial vehicle scanning device that models.
(II) contents of utility model
In order to solve the technical problem, the utility model provides a following technical scheme: the utility model provides a homeland space planning unmanned aerial vehicle scanning device that models, includes main part, branch and supporting shoe, the wing is all installed to four corners on main part top, the battery is installed to the one end of main part, the top of main part is provided with energy-conserving structure, the supporting shoe is installed to the bottom of main part, the bottom of supporting shoe is provided with the connecting block, and the bottom of connecting block installs the camera, the both sides of supporting shoe all are provided with the dismouting structure, branch is all installed to four corners of main part bottom, the bottom of branch all is provided with buffer structure.
Preferably, buffer structure is including expanding spring, supporting legs, gag lever post, stopper and spacing groove, the stopper is all installed in the inside bottom of branch, the spacing groove is all installed to the inside of stopper, the gag lever post is all installed to the bottom of stopper, and the supporting legs is all installed to the bottom of gag lever post, expanding spring is all installed to the both sides on supporting legs top. The buffer structure that sets up can reduce the impact force of main part when descending, plays certain guard action to the main part.
Preferably, the extension springs are symmetrically arranged, and the extension springs and the supporting legs form an extension structure. The elastic force of the extension spring is utilized to realize the buffering capacity.
Preferably, the diameter of the supporting foot is smaller than that of the supporting rod, and the diameter of the limiting rod is smaller than that of the limiting groove. The limiting rod can move towards the inside of the limiting groove.
Preferably, energy-conserving structure is including solar panel, support column and fastening bolt, solar panel installs the top in the main part, the support column is all installed to four corners of solar panel bottom, and the fastening bolt is all installed to the bottom of support column both sides. The energy-saving structure can realize the purpose of saving resources.
Preferably, the dismouting structure is including rubber pad, splint, revolve handle, screw rod and preformed hole, revolve the both sides of all installing at the supporting shoe to the handle, the screw rod is all installed to the one end of revolving the handle, and the one end of screw rod all installs splint, the rubber pad is all installed to the one end of splint, the outside of screw rod all is provided with the preformed hole. The camera can be taken off from the bottom of supporting shoe to the dismouting structure that sets up and change.
Preferably, the inner wall of the preformed hole is provided with threads, and the preformed hole is meshed with the screw rod through the threads. The fixing limit of the clamping plate to the connecting block can be released by rotating the knob.
(III) advantageous effects
The utility model provides a homeland space planning unmanned aerial vehicle scanning device that models, its advantage lies in:
(1) the camera can be taken down from the bottom end of the supporting block by rotating the rotary handles arranged on the two sides of the supporting block and driving the clamping plate to move along the direction of the reserved hole through the screw rod, so that the fixing limit of the clamping plate on the connecting block is removed, and the aim of replacing the camera is fulfilled;
(2) the solar panel is arranged at the top end of the main body, under the action of the solar panel, the photovoltaic controller is utilized to convert light energy into electric energy, and the electric energy is stored in the storage battery and used by the device, so that the aim of saving resources is fulfilled;
(3) through the expanding spring of installation in the inside bottom both sides of branch, utilize expanding spring's elastic force for the gag lever post can remove, and thus can reduce the impact force of main part when descending, realizes the performance of buffering, plays certain guard action to the main part.
Drawings
In order to clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below, and it is obvious that the drawings in the description below are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a schematic front view of the present invention;
fig. 2 is a schematic top view of the present invention;
FIG. 3 is a partial structural view of the detachable structure of the present invention;
fig. 4 is a schematic view of a partial structure of the buffer structure of the present invention;
fig. 5 is a schematic diagram of the energy-saving structure of the present invention.
The reference numerals in the figures illustrate: 1. a main body; 2. a strut; 3. a buffer structure; 301. a tension spring; 302. supporting legs; 303. a limiting rod; 304. a limiting block; 305. a limiting groove; 4. a camera; 5. a supporting block; 6. connecting blocks; 7. an airfoil; 8. an energy-saving structure; 801. a solar panel; 802. a support column; 803. fastening a bolt; 9. a disassembly and assembly structure; 901. a rubber pad; 902. a splint; 903. rotating a handle; 904. a screw; 905. reserving a hole; 10. and (4) a storage battery.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, 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.
Example one
Referring to fig. 1-5, the present invention provides an embodiment: the utility model provides a national soil space planning unmanned aerial vehicle scanning device that models, including main part 1, branch 2 and supporting shoe 5, wing 7 is all installed to four corners on 1 top of main part, battery 10 is installed to the one end of main part 1, the top of main part 1 is provided with energy-conserving structure 8, energy-conserving structure 8 is including solar panel 801, support column 802 and fastening bolt 803, solar panel 801 installs the top in main part 1, support column 802 is all installed to four corners of solar panel 801 bottom, and fastening bolt 803 is all installed to the bottom of support column 802 both sides, fix solar panel 801 on the top of main part 1 through fastening bolt 803, under solar panel 801's effect, utilize photovoltaic controller to convert light energy into electric energy, with electric energy storage in battery 10's inside, supply this device to use.
The bottom end of the main body 1 is provided with a supporting block 5, the bottom end of the supporting block 5 is provided with a connecting block 6, the bottom end of the connecting block 6 is provided with a camera 4, four corners of the bottom end of the main body 1 are provided with supporting rods 2, the bottom end of each supporting rod 2 is provided with a buffer structure 3, each buffer structure 3 comprises a telescopic spring 301, supporting legs 302, a limiting rod 303, a limiting block 304 and a limiting groove 305, the limiting blocks 304 are all arranged at the bottom end inside the supporting rods 2, the limiting grooves 305 are all arranged inside the limiting blocks 304, the limiting rods 303 are all arranged at the bottom end of the limiting blocks 304, the supporting legs 302 are all arranged at the bottom end of the limiting rods 303, the telescopic springs 301 are arranged at two sides of the top ends of the supporting legs 302 symmetrically, the telescopic springs 301 and the supporting legs 302 form a telescopic structure, the diameter of the supporting legs 302 is smaller than that of the supporting rods 2, the diameter of the limiting rods 303 is smaller than that of the limiting grooves 305, through camera 4, can scan the homeland position, when main part 1 descends perpendicularly, utilize expanding spring 301's elastic force for gag lever post 303 can remove to the inside of spacing groove 305, thereby can reduce the impact force of main part 1 when descending, realizes the performance of buffering, plays certain guard action to main part 1.
Example two
The both sides of supporting shoe 5 all are provided with dismouting structure 9, dismouting structure 9 is including rubber pad 901, splint 902, revolve 903, screw rod 904 and preformed hole 905, revolve 903 all install the both sides at supporting shoe 5, revolve the one end of 903 and all install screw rod 904, and splint 902 is all installed to the one end of screw rod 904, rubber pad 901 is all installed to the one end of splint 902, the outside of screw rod 904 all is provided with preformed hole 905, set up screw thread on the inner wall of preformed hole 905, preformed hole 905 meshes with screw rod 904 through the screw thread mutually, when camera 4 needs to be changed, rotate and revolve 903, screw rod 904 drives the direction removal that splint 902 follow preformed hole 905, remove the fixed restriction of splint 902 to connecting block 6, alright take off camera 4 from the bottom of supporting shoe 5 and change.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, 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.
The above-described embodiments of the apparatus are merely illustrative, and the units described as separate parts may or may not be physically separate, and parts displayed as units may or may not be physical units, may be located in one place, or may be distributed on a plurality of network units. Some or all of the modules may be selected according to actual needs to achieve the purpose of the solution of the present embodiment. One of ordinary skill in the art can understand and implement it without inventive effort.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it should be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention in its corresponding aspects.

Claims (7)

1. The utility model provides a homeland space planning unmanned aerial vehicle scanning device that models, includes main part (1), branch (2) and supporting shoe (5), its characterized in that: wings (7) are mounted at four corners of the top end of the main body (1), a storage battery (10) is mounted at one end of the main body (1), an energy-saving structure (8) is arranged at the top end of the main body (1), and a supporting block (5) is mounted at the bottom end of the main body (1);
the bottom end of the supporting block (5) is provided with a connecting block (6), the bottom end of the connecting block (6) is provided with a camera (4), and both sides of the supporting block (5) are provided with dismounting structures (9);
branch (2) are all installed to four corners of main part (1) bottom, the bottom of branch (2) all is provided with buffer structure (3).
2. The unmanned aerial vehicle modeling and scanning device for territorial space planning of claim 1, wherein: buffer structure (3) are including expanding spring (301), supporting legs (302), gag lever post (303), stopper (304) and spacing groove (305), stopper (304) are all installed in branch (2) inside bottom, spacing groove (305) are all installed to the inside of stopper (304), gag lever post (303) are all installed to the bottom of stopper (304), and supporting legs (302) are all installed to the bottom of gag lever post (303), expanding spring (301) are all installed to the both sides on supporting legs (302) top.
3. The modeling and scanning device for unmanned aerial vehicle for territorial space planning according to claim 2, wherein: the telescopic springs (301) are symmetrically arranged, and the telescopic springs (301) and the supporting legs (302) form a telescopic structure.
4. The modeling and scanning device for unmanned aerial vehicle for territorial space planning of claim 2, wherein: the diameter of the supporting leg (302) is smaller than that of the supporting rod (2), and the diameter of the limiting rod (303) is smaller than that of the limiting groove (305).
5. The modeling and scanning device for unmanned aerial vehicle for territorial space planning according to claim 1, wherein: energy-conserving structure (8) are including solar panel (801), support column (802) and fastening bolt (803), the top in main part (1) is installed to solar panel (801), support column (802) are all installed to four corners of solar panel (801) bottom, and fastening bolt (803) are all installed to the bottom of support column (802) both sides.
6. The modeling and scanning device for unmanned aerial vehicle for territorial space planning according to claim 1, wherein: dismouting structure (9) are including rubber pad (901), splint (902), revolve handle (903), screw rod (904) and preformed hole (905), revolve the both sides at supporting shoe (5) all installed in handle (903), revolve the one end of handle (903) and all install screw rod (904), and the one end of screw rod (904) all installs splint (902), rubber pad (901) are all installed to the one end of splint (902), the outside of screw rod (904) all is provided with preformed hole (905).
7. The modeling and scanning device for unmanned aerial vehicle for territorial space planning according to claim 6, wherein: the inner wall of the preformed hole (905) is provided with threads, and the preformed hole (905) is meshed with the screw rod (904) through the threads.
CN202220072355.1U 2022-01-12 2022-01-12 Modeling scanning device for unmanned aerial vehicle for territorial space planning Active CN217348242U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202220072355.1U CN217348242U (en) 2022-01-12 2022-01-12 Modeling scanning device for unmanned aerial vehicle for territorial space planning

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202220072355.1U CN217348242U (en) 2022-01-12 2022-01-12 Modeling scanning device for unmanned aerial vehicle for territorial space planning

Publications (1)

Publication Number Publication Date
CN217348242U true CN217348242U (en) 2022-09-02

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Family Applications (1)

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CN202220072355.1U Active CN217348242U (en) 2022-01-12 2022-01-12 Modeling scanning device for unmanned aerial vehicle for territorial space planning

Country Status (1)

Country Link
CN (1) CN217348242U (en)

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