CN117184471B - Unmanned aerial vehicle survey and drawing measuring device - Google Patents
Unmanned aerial vehicle survey and drawing measuring device Download PDFInfo
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- CN117184471B CN117184471B CN202311464508.2A CN202311464508A CN117184471B CN 117184471 B CN117184471 B CN 117184471B CN 202311464508 A CN202311464508 A CN 202311464508A CN 117184471 B CN117184471 B CN 117184471B
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- 238000001514 detection method Methods 0.000 claims abstract description 41
- 230000002633 protecting effect Effects 0.000 claims abstract description 22
- 238000013507 mapping Methods 0.000 claims abstract description 16
- 238000005259 measurement Methods 0.000 claims abstract description 9
- 230000000087 stabilizing effect Effects 0.000 claims description 35
- 238000009434 installation Methods 0.000 claims description 8
- 230000003014 reinforcing effect Effects 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 4
- 230000000694 effects Effects 0.000 description 20
- 230000001681 protective effect Effects 0.000 description 13
- 238000010586 diagram Methods 0.000 description 4
- 230000003139 buffering effect Effects 0.000 description 3
- 239000000428 dust Substances 0.000 description 3
- 230000002787 reinforcement Effects 0.000 description 3
- 238000012876 topography Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000010687 lubricating oil Substances 0.000 description 2
- 241000238631 Hexapoda Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000009435 building construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
- 210000003462 vein Anatomy 0.000 description 1
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Abstract
The invention provides an unmanned aerial vehicle mapping measurement device, which relates to the field of mapping measurement and comprises an unmanned aerial vehicle, wherein a wing is arranged on a fuselage frame of the unmanned aerial vehicle, a clamping assembly is arranged at the middle position of the unmanned aerial vehicle, an expanding assembly can be directly arranged at the bottom of the clamping assembly, a detection assembly is arranged at the inner position of the expanding assembly, the detection assembly can detect mapping on the ground, a protection assembly is arranged at the position of the bottom of the expanding assembly close to the detection assembly, the protection assembly is used for protecting the detection assembly, the problem that the detection assembly is damaged when the unmanned aerial vehicle falls is avoided, a warning assembly is always in a vertical state, the warning assembly is used for conveniently enabling the whole device to be searched when the unmanned aerial vehicle is irradiated with laser, and the problem that the existing unmanned aerial vehicle cannot collide with some flying birds, so that damage is caused to the detection equipment when the unmanned aerial vehicle falls off, and meanwhile, more outdoor plants can cause difficulty in searching the unmanned aerial vehicle is solved.
Description
Technical Field
The invention relates to the technical field of surveying and mapping, in particular to an unmanned aerial vehicle surveying and mapping device.
Background
With the continuous development and progress of social science and technology, the building construction of cities is increased, and some cities are expanded in the planning, so that suburbs near the cities need to be mapped, which is an indispensable step in urban construction; the urban topography is accurately mapped, better calculation is carried out, cities can be planned better, and accurate mapping measurement can better detect some geological veins and the like, so that the urban topography map has better detection effects on some geology, mines and the like.
However, the existing outdoor surveying and mapping measurement is mostly simple through manual erection equipment to detect and measure topography and distance, but can use some unmanned aerial vehicle along with the development of science and technology, can survey and measure more dangerous region, unmanned aerial vehicle can directly hover at a certain height when using, detects the detection of accomplishing the back in the next place, and the eminence unmanned aerial vehicle can not collide with some flying birds when using, causes unmanned aerial vehicle's dropping, and unmanned aerial vehicle department that drops receives the damage and also can let the detection equipment damage, and some outdoor can have more plants simultaneously, can cause the unmanned aerial vehicle that drops to seek the difficult problem.
Disclosure of Invention
In view of the above, the invention provides an unmanned aerial vehicle surveying and mapping device to solve the problem that when the existing unmanned aerial vehicle is used, the existing unmanned aerial vehicle is inevitably collided with some flying birds, so that the unmanned aerial vehicle is damaged when falling, and meanwhile, more outdoor plants can cause difficulty in searching for the falling unmanned aerial vehicle.
The invention provides an unmanned aerial vehicle surveying and mapping device, which specifically comprises an unmanned aerial vehicle, wherein a wing is arranged on a fuselage frame of the unmanned aerial vehicle, a connecting component is arranged at the bottom position of the wing of the fuselage frame, a protection component is arranged at the bottom position of the connecting component, a warning component is arranged at the top position of the protection component, a stabilizing component is additionally arranged at the lower end position of the protection component, a clamping component is arranged at the middle position of the fuselage frame, an expanding component is fixed at the bottom position of the clamping component, a detection component is arranged at the inner position of the expanding component, and a protection component is arranged at the bottom of the expanding component.
Further, the protection frame of the protection assembly is of a frame structure, the protection frame is installed at the outer end position of the unmanned aerial vehicle, reinforcing bars are arranged on the rod bodies of the protection frame, and the rod bodies of the protection frame are located at the outer end position of each group of wings.
Further, the connecting ring of the connecting component is connected to the lower end position of the wing through the connector, the lower end position of the connecting ring is connected with the protection component, the connecting ring is arranged to be of an elliptic structure, and the connecting ring is arranged to be of an upper group and a lower group.
Further, the firm circle of firm subassembly sets up to annular structure, and firm circle sets up in the bottom position of protection subassembly, is provided with protruding strip on the firm circle, and the setting of firm circle is bilayer structure from top to bottom, and the position department between two sets of firm circles is equipped with the firm post additional, and the firm post between the firm circle cup joints the installation each other from top to bottom, is provided with the arch on the bottom surface of bottom firm circle, and the arch of firm circle adopts the rubber material.
Further, the connecting plate of joint subassembly sets up to the joint and installs the intermediate position at the fuselage frame, and the lower extreme position department of connecting plate is provided with the joint frame, is provided with four vertical clamping bars of group on the joint frame, and the joint frame passes through the clamping bar joint to be installed on the connecting plate, and the outer end of connecting plate is exposed to the clamping bar of joint frame, and the clamping bar exposure part joint of joint frame has the fixed plate.
Further, the expansion frame of the expansion assembly is fixed at the bottom of the clamping assembly, the expansion frame is of a conical structure, the annular frame is rotatably installed on the inner wall of the expansion frame, and the outer wall of the expansion frame is provided with an outer opening.
Further, the detection equipment of the detection assembly is arranged to be hinged on the inner wall of the annular frame, the tail end position of the detection equipment is arranged to be a detection head, the contact position of the detection equipment and the annular frame is provided with a clamping strip, and the detection equipment and the clamping strip are mutually clamped and fixed.
Further, the protection cover of the protection assembly is arranged at the bottom of the protection cover in a rotating mode, the middle position of the protection cover is connected with the power assembly, the outer end of the protection cover is provided with a fixed underframe, and the fixed underframe and the expansion frame are mutually fixed.
Further, the balance ring of warning subassembly sets up to annular structure, and the balance ring sets up in the top position of protection subassembly, and the balance ring sets up to inside and outside bilayer structure, and the intermediate position department of balance ring is provided with the warning light, and the bottom of warning light is provided with the balancing weight.
The invention provides an unmanned aerial vehicle surveying and mapping measuring device, which has the beneficial effects that:
1. according to the unmanned aerial vehicle, the clamping assembly is arranged at the middle position of the unmanned aerial vehicle, the expanding assembly can be directly arranged at the bottom of the clamping assembly, the detecting assembly is arranged at the inner position of the expanding assembly, the detecting assembly can detect and map the ground, the protecting assembly is arranged at the bottom of the expanding assembly and close to the position of the detecting assembly, the protecting assembly is protected by the detecting assembly, the problem of damage of the detecting assembly when the unmanned aerial vehicle falls is avoided, the protecting assembly is arranged at the edge position of the unmanned aerial vehicle through the connecting assembly, the protecting assembly is integrally provided with an external protecting effect on the unmanned aerial vehicle, the connecting assembly connected with the unmanned aerial vehicle is provided with a stabilizing assembly which is used for realizing the buffer protection of the unmanned aerial vehicle and the protecting assembly, the unmanned aerial vehicle is provided with a better buffer effect through the stabilizing assembly when the unmanned aerial vehicle falls normally, the warning assembly is arranged at the middle position of the top of the protecting assembly, and when the unmanned aerial vehicle falls into a luxuriant plant position, no matter the device is in any skew state, the warning assembly is always in a vertical state, and the whole device is conveniently found when the device is irradiated with laser.
2. The middle position of the fuselage frame is clamped and provided with the connecting plate, the clamping frame at the bottom of the connecting plate is clamped on the connecting plate through the vertical strips, and the bottom of the clamping frame is connected with the expansion assembly, so that the expansion assembly can be connected to the fuselage frame by the clamping assembly, the vertical clamping strips of the clamping frame, and the fixing plate at the top of the connecting plate can be clamped on the vertical clamping strips of the clamping frame, thereby realizing better stable fixing effect of the fixing plate on the whole clamping assembly.
3. According to the unmanned aerial vehicle protection device, the connecting rings are additionally arranged at the bottom of the wing positions of the fuselage frame, the connecting rings are of an oval structure, after the connecting rings are connected between the unmanned aerial vehicle and the protection assembly, the oval connecting rings have a stable buffer function, so that the protection assembly has a protection function on the unmanned aerial vehicle, the protection frame connected to the connection assembly is additionally provided with the reinforcing strips, the protection frame has a more stable function through the reinforcing strips, the protection frame is positioned at the outer end position of the unmanned aerial vehicle, the protection frame has a more stable function, and when the unmanned aerial vehicle falls down due to collision, the protection frame at the outer end of the unmanned aerial vehicle can be used for buffer protection, so that the protection effect of the protection assembly on the unmanned aerial vehicle is achieved.
4. The bottom of the stabilizing ring is provided with the stabilizing ring, the stabilizing ring is of an upper-lower double-layer structure, the bottom surface of the stabilizing ring at the lower end is provided with the rubber bulge, the stabilizing ring at the bottom has a more stable effect when contacting with the ground, the stabilizing column is arranged between the upper-lower double-layer stabilizing rings, the stabilizing column has a certain anti-vibration effect between the upper-lower stabilizing rings, and the protection effect of the stabilizing component on the unmanned aerial vehicle is improved.
5. The expansion frame is fixed at the bottom of the clamping assembly, the expansion frame is of a cone device structure, the annular frame is rotatably arranged at the inner wall of the expansion frame, the annular frame is arranged for being provided with the detection assembly, so that the annular frame can rotate to control the detection of the detection assembly, the detection assembly can carry out multidirectional detection, the wall of the expansion frame is provided with the outer opening, the annular frame is conveniently controlled from the outside, lubricating oil is conveniently added to the annular frame from the position of the outer opening, and the annular frame can carry out better rotation.
6. The detection equipment is arranged at the inner wall of the annular frame in a hinged mode, the bottom position of the detection equipment is provided with the detection head used on the detection side, the detection equipment which is arranged in a hinged mode has the function of being convenient to replace, and the bottom position of the expansion frame is provided with the protection cover, so that the protection cover protects the detection assembly, and the damage problem of the detection assembly when the whole device falls down is avoided.
Drawings
In order to more clearly illustrate the technical solution of the embodiments of the present invention, the drawings of the embodiments will be briefly described below.
The drawings described below are only for illustration of some embodiments of the invention and are not intended to limit the invention.
In the drawings:
FIG. 1 is a schematic view of the overall structure of an apparatus according to an embodiment of the present invention;
FIG. 2 is a schematic view of the bottom surface structure of the device according to the embodiment of the present invention;
fig. 3 is a schematic view of a fuselage airframe structure of an embodiment of the present invention;
FIG. 4 is a schematic view of a guard assembly according to an embodiment of the present invention;
FIG. 5 is a schematic diagram of a protective component structure according to an embodiment of the present invention;
FIG. 6 is a schematic illustration of an expansion assembly of an embodiment of the present invention;
FIG. 7 is a schematic diagram of a detection assembly according to an embodiment of the present invention;
FIG. 8 is a schematic diagram of a connection assembly according to an embodiment of the present invention;
fig. 9 is a schematic structural diagram of an alarm assembly according to an embodiment of the invention.
List of reference numerals
1. Unmanned plane; 101. a fuselage frame; 102. a wing; 2. a protective assembly; 201. a protective frame; 202. reinforcing strips; 3. a connection assembly; 301. a connecting ring; 302. a connector; 4. a stabilizing assembly; 401. a stabilizing ring; 402. stabilizing the column; 5. a clamping assembly; 501. a clamping frame; 502. a connecting plate; 503. a fixing plate; 6. expanding the assembly; 601. expanding the frame; 602. an outer opening; 603. an annular frame; 7. a detection assembly; 701. a detection device; 702. a probe; 703. a clamping strip; 8. a protection component; 801. a protective cover; 802. fixing the underframe; 9. a warning component; 901. a balance ring; 902. a warning light.
Detailed Description
In order to make the objects, aspects and advantages of the technical solution of the present invention more clear, the technical solution of the embodiment of the present invention will be clearly and completely described below with reference to the accompanying drawings of the specific embodiment of the present invention.
Please refer to fig. 1 to 9:
embodiment one: the invention provides an unmanned aerial vehicle mapping measurement device, which comprises an unmanned aerial vehicle 1, wherein a wing 102 is arranged on a fuselage frame 101 of the unmanned aerial vehicle 1, a connecting component 3 is arranged at the bottom position of the wing 102 of the fuselage frame 101, a protection component 2 is arranged at the bottom position of the connecting component 3, a warning component 9 is arranged at the top position of the protection component 2, a stabilizing component 4 is additionally arranged at the lower end position of the protection component 2, a clamping component 5 is arranged at the middle position of the fuselage frame 101, an expanding component 6 is fixed at the bottom position of the clamping component 5, a detection component 7 is arranged at the inner position of the expanding component 6, and a protection component 8 is arranged at the bottom of the expanding component 6.
Wherein, the protection frame 201 of protection subassembly 2 is established to frame construction, the protection frame 201 is installed in the outer end position department of unmanned aerial vehicle 1, be provided with reinforcement strip 202 on the body of rod of protection frame 201, set up reinforcement strip 202 on the body of rod with protection frame 201, help letting reinforcement strip 202 have and strengthen protection frame 201, let protection frame 201 can not let protection frame 201 appear the problem of deformation when receiving the collision, the body of rod of protection frame 201 is in, the outer end position of every group wing 102, set up protection frame 201 as the position department that is in every group wing 102 of fuselage frame 101, thereby the realization is let protection frame 201 have the protection to wing 102, thereby avoid unmanned aerial vehicle 1 when unexpected falling, let protection frame 201 carry out the effect of protection to wing 102.
Wherein, the go-between 301 of coupling assembling 3 passes through connector 302 to be connected in the lower extreme position of wing 102, the lower extreme position and the protection component 2 interconnect of go-between 301, the go-between 301 of connecting in the wing 102 bottom sets up to connect the main assembly of protection component 2, thereby let go-between 301 play the certain buffering between unmanned aerial vehicle 1 and protection component 2, thereby keep stable interval throughout between protection component 2 and unmanned aerial vehicle 1, the guard action to unmanned aerial vehicle 1 when reaching unmanned aerial vehicle 1 and wholly drop, go-between 301 sets up to oval-shaped structure, go-between 301 sets up to two sets of structures from top to bottom, set up go-between 301 to oval-shaped structure, let go-between 301 can realize keeping the stable interval of protection component 2 and unmanned aerial vehicle 1, the effect, and set up go-between 301 to two sets of structures from top to bottom, let go-between 301 have more stable effect.
Wherein, the firm circle 401 of firm subassembly 4 sets up to annular structure, firm circle 401 sets up the bottom position at protection subassembly 2, be provided with protruding strip on the firm circle 401, set up protruding strip on the firm circle 401, let the firm circle 401 have better increase intensity's effect, the setting of firm circle 401 is bilayer structure from top to bottom, the position department between two sets of firm circles 401 adds and has firm post 402, firm post 402 cup joint each other between the firm circle 401 is installed, set up the mode of cup joint each other installation between the firm circle 401 of upper and lower to firm post 402, the state that lets firm post 402 can form the buffering each other has been realized, make the device when falling with ground contact through firm subassembly 4, it is to the holistic guard action of unmanned aerial vehicle 1 to reach, be provided with the arch on the bottom surface of bottom firm circle 401, the arch of firm circle 401 adopts the rubber material, set up the arch with the bottom firm circle 401, let the arch that adopts the rubber material can realize letting the protruding friction force that can increase with ground between the firm circle 401, the firm post 402 has realized letting the whole stable device that lets through firm circle 401 more land.
Embodiment two: wherein, the connecting plate 502 of joint subassembly 5 sets up to the joint and installs in the intermediate position of fuselage frame 101, the lower extreme position department of connecting plate 502 is provided with joint frame 501, be provided with four vertical joint bars of group on the joint frame 501, joint frame 501 passes through joint bar joint and installs on connecting plate 502, set up the connecting plate 502 as the joint in unmanned aerial vehicle 1 intermediate position, and joint frame 501 then installs on connecting plate 502 through joint bar joint, the mutual stable connection effect between connecting plate 502 and the joint frame 501 has been realized, thereby make the whole convenience of joint subassembly 5 follow unmanned aerial vehicle 1, realize the effect of swift dismouting, the joint bar of joint frame 501 exposes the outer end of connecting plate 502, the joint bar exposure part joint of joint frame 501 has fixed plate 503, in order to make the joint installation of joint frame 501 more stable, directly joint fixed plate 503 is fixed to the joint bar of joint frame 501 in order to the joint bar top position department of joint frame 501, the whole fixed action of joint frame 501 has been increased to the joint bar of joint subassembly 501.
The expansion frame 601 of the expansion assembly 6 is fixed at the bottom of the clamping assembly 5, the expansion frame 601 is in a conical structure, the expansion frame 601 is fixed at the bottom of the clamping assembly 5, the expansion frame 601 is in a conical shape, the problem that rainwater or sundries cannot remain at the expansion frame 601 is solved, the annular frame 603 is rotatably installed on the inner wall of the expansion frame 601, the outer wall of the expansion frame 601 is provided with the outer opening 602, the fact that the outer opening 602 can be contacted with the annular frame 603 from the outside, namely lubricating oil can be added at the outer opening 602, the annular frame 603 is driven by the power assembly installed at the outer opening 602, and the outer opening 602 of the expansion frame 601 can be covered and blocked, so that dust is prevented from falling into the outer opening 602 of the expansion frame 601.
The detecting device 701 of the detecting assembly 7 is arranged to be hinged on the inner wall of the annular frame 603, the tail end position of the detecting device 701 is arranged to be a detecting head 702, the contact position of the detecting device 701 and the annular frame 603 is provided with a clamping strip 703, the detecting device 701 and the clamping strip 703 are clamped and fixed with each other, the detecting device 701 is firstly arranged to be in a hinged installation mode, the clamping strip 703 is arranged at the contact position of the detecting device 701 and the annular frame 603, the clamping strip 703 can be directly clamped at the detecting device 701, and the detecting device 701 is convenient to replace and detach.
Wherein, the safety cover 801 of protection subassembly 8 sets up to rotate the bottom position of installing safety cover 801, the intermediate position and the power component of safety cover 801 are connected, the outer end position of safety cover 801 is provided with fixed chassis 802, fixed chassis 802 and expansion frame 601 are fixed each other, at first, safety cover 801 sets up to rotate the installation, let safety cover 801 have the guard action to detecting assembly 7, avoid unmanned aerial vehicle 1 wholly when falling, the damage problem to detecting assembly 7, and the safety cover 801 outer end then can be unavoidably glue some dust, thereby set up safety cover 801 as pivoted installation, be in the fixed chassis 802 of safety cover 801 outer end can direct contact, thereby when safety cover 801 rotates, can let fixed chassis 802 carry out the effect of dust clearance to pivoted safety cover 801.
Embodiment III: wherein, the balancing ring 901 of warning subassembly 9 sets up to annular structure, balancing ring 901 sets up in the top position of protection subassembly 2, balancing ring 901 sets up to inside and outside bilayer structure, the intermediate position department of balancing ring 901 is provided with warning light 902, the bottom of warning light 902 is provided with the balancing weight, install warning light 902 on balancing ring 901, and the balancing weight that the bottom position department of warning light 902 set up can let warning light 902 be in vertical structure all the time, thereby make the whole of device be difficult to seek when dropping, through the warning light 902 that is vertical structure all the time, can shine light orientation upper end, the convenience is to the holistic effect of seeking of device.
Specific use and action of the embodiment: when the invention is used, the four groups of wings 102 of the fuselage frame 101 are provided with the connecting rings 301 at opposite positions, the connecting rings 301 at the lower end positions of the wings 102 are respectively provided with two groups, the connecting rings 302 are additionally arranged at the positions connected with the connecting rings 301 of the two groups, the effect of stably connecting the connecting rings 301 at the bottom of the wings 102 is realized, the whole of the protecting frame 201 is arranged at the connecting rings 301, the whole of the protecting frame 201 is positioned at the outer end position of the unmanned aerial vehicle 1, the protecting frame 201 plays a role in protecting the whole of the unmanned aerial vehicle 1 when the unmanned aerial vehicle 1 collides, meanwhile, the connecting rings 301 provided with the protecting frame 201 are connected, the protecting function for protecting the whole of the protecting component 2 is increased, the protecting frame 201 is further reinforced by the reinforcing strips 202, the whole of the protecting frame 201 is more stable, the better shape keeping effect of the protecting frame 201 is realized, the lower end of the protective frame 201 is provided with a stabilizing ring 401, the stabilizing ring 401 is arranged into an upper-lower double-layer structure, stabilizing columns 402 which are sleeved and installed with each other are arranged at the positions between the stabilizing rings 401, buffering can be formed between the upper-lower stabilizing rings 401, the effect of better stability increasing is achieved when the device is integrally parked, a balance ring 901 is arranged at the intersection position of the top of the protective frame 201, the balance ring 901 is arranged into an inner-outer double-layer structure, a warning lamp 902 is installed on the inner-layer balance ring 901, the warning lamp 902 can pass through the inner-outer double-layer balance ring 901, a state which is always vertical is achieved, the warning lamp 902 can irradiate laser, when the device falls to a position which is difficult to find, the laser passing through the warning lamp 902 is convenient to find, a clamping component 5 is installed at the position in the middle of the body frame 101, and the whole clamping component 5 is arranged into a rapid installation structure, the quick assembly disassembly effect between the clamping assembly 5 and the unmanned aerial vehicle 1 is convenient, the bottom of the clamping frame 501 is directly fixed with the expansion frame 601, the expansion frame 601 is of a cylindrical structure, the annular frame 603 can be rotatably installed on the inner wall, the position of the outer opening 602 of the expansion frame 601 can be used for realizing contact control of the annular frame 603, the position of the outer opening 602 can lubricate the annular frame 603, the outside of the expansion frame 601 has the effect of preventing entry of some sundries after covering and shielding, the position of the bottom of the expansion frame 601 is rotatably installed with the protective cover 801, the protective cover 801 is provided with the detection assembly 7 for protecting the annular frame 603, the fixed underframe 802 at the outer end position of the protective cover 801 is set to be in a fixed state, the protective cover 801 can be rotated through an internal power part, and after the rotation of the protective cover 801 is realized, the outer wall of the protective cover 801 is cleared through the fixed underframe 802, and the problem that sundries remain at the outer end of the protective cover 801 or insects block the detection assembly 7 is avoided.
Claims (5)
1. The unmanned aerial vehicle surveying and mapping device is characterized by comprising an unmanned aerial vehicle (1), wherein a wing (102) is installed on a fuselage frame (101) of the unmanned aerial vehicle (1), a connecting component (3) is arranged at the bottom position of the wing (102) of the fuselage frame (101), a protection component (2) is arranged at the bottom position of the connecting component (3), a warning component (9) is arranged at the top position of the protection component (2), a stabilizing component (4) is additionally arranged at the lower end position of the protection component (2), a clamping component (5) is arranged at the middle position of the fuselage frame (101), an expanding component (6) is fixed at the bottom position of the clamping component (5), a detection component (7) is installed at the inner position of the expanding component (6), and a protection component (8) is installed at the bottom of the expanding component (6); the protection frame (201) of the protection assembly (2) is of a frame structure, the protection frame (201) is arranged at the outer end position of the unmanned aerial vehicle (1), reinforcing strips (202) are arranged on the rod bodies of the protection frame (201), and the rod bodies of the protection frame (201) are positioned at the outer end position of each group of wings (102); the connecting ring (301) of the connecting assembly (3) is connected to the lower end position of the wing (102) through a connector (302), the lower end position of the connecting ring (301) is connected with the protecting assembly (2), the connecting ring (301) is of an elliptic structure, and the connecting ring (301) is of an upper-lower two-group structure; the stabilizing ring (401) of the stabilizing component (4) is of an annular structure, the stabilizing ring (401) is arranged at the bottom of the protecting component (2), protruding strips are arranged on the stabilizing ring (401), the stabilizing ring (401) is of an upper-lower double-layer structure, stabilizing columns (402) are additionally arranged at positions between the two groups of stabilizing rings (401), the stabilizing columns (402) between the upper stabilizing ring (401) and the lower stabilizing ring (401) are mutually sleeved and installed, protrusions are arranged on the bottom surface of the bottom stabilizing ring (401), and the protrusions of the stabilizing ring (401) are made of rubber materials; the balance ring (901) of warning subassembly (9) sets up to annular structure, and balance ring (901) sets up the top position at protection subassembly (2), and balance ring (901) set up to inside and outside bilayer structure, and the intermediate position department of balance ring (901) is provided with warning light (902), and the bottom of warning light (902) is provided with the balancing weight.
2. The unmanned aerial vehicle mapping measurement apparatus of claim 1, wherein: the connecting plate (502) of joint subassembly (5) set up to the intermediate position of joint installation at fuselage frame (101), and the lower extreme position department of connecting plate (502) is provided with joint frame (501), is provided with four vertical clamping bars of group on joint frame (501), and joint frame (501) are installed on connecting plate (502) through the clamping bar joint, and the outer end of connecting plate (502) is exposed to the clamping bar of joint frame (501), and the clamping bar exposure part joint of joint frame (501) has fixed plate (503).
3. The unmanned aerial vehicle mapping measurement apparatus of claim 1, wherein: expansion frame (601) of expansion subassembly (6) set up to fix in the bottom position of joint subassembly (5), expand frame (601) and set up to conical structure, rotate on expansion frame (601) inner wall and install annular frame (603), be provided with outer trompil (602) on the outer wall of expansion frame (601).
4. The unmanned aerial vehicle mapping measurement apparatus of claim 1, wherein: the detection device (701) of the detection assembly (7) is arranged to be hinged on the inner wall of the annular frame (603), the tail end position of the detection device (701) is provided with a detection head (702), the contact position of the detection device (701) and the annular frame (603) is provided with a clamping strip (703), and the detection device (701) and the clamping strip (703) are mutually clamped and fixed.
5. The unmanned aerial vehicle mapping measurement apparatus of claim 1, wherein: the protection cover (801) of the protection assembly (8) is arranged at the bottom of the protection cover (801) in a rotating mode, the middle position of the protection cover (801) is connected with the power assembly, the outer end of the protection cover (801) is provided with a fixed underframe (802), and the fixed underframe (802) and the expansion frame (601) are mutually fixed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311464508.2A CN117184471B (en) | 2023-11-07 | 2023-11-07 | Unmanned aerial vehicle survey and drawing measuring device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311464508.2A CN117184471B (en) | 2023-11-07 | 2023-11-07 | Unmanned aerial vehicle survey and drawing measuring device |
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| CN117184471A CN117184471A (en) | 2023-12-08 |
| CN117184471B true CN117184471B (en) | 2024-02-06 |
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