CN213036090U - Follow-on airborne laser radar equipment based on unmanned aerial vehicle - Google Patents
Follow-on airborne laser radar equipment based on unmanned aerial vehicle Download PDFInfo
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- CN213036090U CN213036090U CN202022234212.XU CN202022234212U CN213036090U CN 213036090 U CN213036090 U CN 213036090U CN 202022234212 U CN202022234212 U CN 202022234212U CN 213036090 U CN213036090 U CN 213036090U
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Abstract
The utility model provides a follow-on airborne laser radar equipment based on unmanned aerial vehicle, including unmanned aerial vehicle machine control main part, mounting panel, wireless control module, host computer, charger, battery, unmanned aerial vehicle wing, driving motor, the fan blade, the support frame falls to the ground the seat, the link, adjustable laser radar equipment fixing plate structure, adjustable new forms of energy conversion plate structure and the buffer type adjustable rod structure that falls to the ground, unmanned aerial vehicle machine control main part inside screw connection have the mounting panel, screw connection has wireless control module, host computer, charger and battery from left to right in proper order in the front portion of mounting panel. The utility model discloses machine carries laser radar equipment casing, antenna boom pole, polished rod, slide pipe, the setting of wing adjusting screw and machine carries laser radar equipment mounting panel is favorable to adjusting the position of machine carries laser radar equipment mounting panel according to the installation demand to in install fixed laser radar equipment, convenient operation.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle patrols and examines equipment, especially, relate to an improved generation's airborne laser radar equipment based on unmanned aerial vehicle.
Background
Along with the development of laser radar technology, the operation of unmanned aerial vehicle laser radar system gradually becomes a new means of electric power line patrol.
At present, an airborne laser radar system is widely applied to the acquisition of three-dimensional space information in the fields of surveying and mapping, electric power, forestry, agriculture, homeland planning, geological disasters, mine safety and the like.
However, the existing airborne laser radar equipment still has the problems of incapability of adjusting the installation position, poor landing protection effect and serious resource waste.
Therefore, it is very necessary to invent an improved airborne laser radar device based on an unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model provides a follow-on airborne laser radar equipment based on unmanned aerial vehicle to there is unable mounted position to adjust in solving current airborne laser radar equipment, falls to the ground the poor and serious problem of wasting of resources of protecting effect. An improved airborne laser radar device based on an unmanned aerial vehicle comprises an unmanned aerial vehicle control main body, a mounting plate, a wireless control module, a host, a charger, a storage battery, an unmanned aerial vehicle wing, a driving motor, fan blades, a supporting frame, a landing seat, a connecting frame, an adjustable laser radar device mounting plate structure, an adjustable new energy conversion plate structure and a landing buffer type adjustable rod structure, wherein the mounting plate is connected with the inside of the unmanned aerial vehicle control main body through screws, and the wireless control module, the host, the charger and the storage battery are sequentially connected with the front part of the mounting plate through screws from left to right; the periphery of the outer side of the unmanned aerial vehicle control main body is transversely connected with unmanned aerial vehicle wings through bolts, the outer side of the lower part of the unmanned aerial vehicle wings is connected with a driving motor through bolts, and the upper end of an output shaft of the driving motor is connected with a fan blade through a key; the left end and the right end of the lower front side of the unmanned aerial vehicle control main body and the front end and the rear end of the lower rear side of the unmanned aerial vehicle control main body are respectively provided with a ground seat through a support frame; the four corners of the bottom of the unmanned aerial vehicle main control body are all connected with connecting frames through bolts; the connecting frame is connected with the adjustable laser radar equipment mounting plate structure; the adjustable new energy conversion plate structure is connected with the unmanned aerial vehicle main control body; the floor buffer type adjustable rod structure is connected with the floor seat; the adjustable laser radar equipment mounting plate structure comprises an airborne laser radar equipment shell, an antenna support rod, a polished rod, a sliding pipe, a wing-shaped adjusting screw and an airborne laser radar equipment mounting plate, wherein the antenna support rod is connected to the middle part of the upper part of the airborne laser radar equipment shell through a bolt; the upper side and the lower side of the interior of the airborne laser radar equipment shell are both connected with a polished rod through transverse bolts; the outer wall of the polish rod is sleeved with a slide pipe and is fixedly connected and arranged through a wing-shaped adjusting screw; and an airborne laser radar equipment mounting plate is connected to the inner side screw between the sliding pipes.
Preferably, the adjustable new energy conversion plate structure comprises a new energy photoelectric conversion plate, a movable plate, a dismounting bolt, an adjusting rod, a supporting tube and an adjusting bolt, wherein the new energy photoelectric conversion plate is arranged on the upper surface of the movable plate and is fastened and connected through the dismounting bolt; the adjusting rod is longitudinally inserted in the supporting tube and is fastened and connected with the supporting tube through an adjusting bolt, and the other end of the adjusting rod is connected with the left side and the right side of the lower part of the movable plate through bolts.
Preferably, the floor buffer type adjustable rod structure comprises an adjusting nut, a buffer rod, a fixed sleeve, a buffer spring, a floor buffer seat and an anti-slip pad, wherein the adjusting nut is in threaded connection with the upper part of the outer wall of the buffer rod; the buffer rod is longitudinally inserted into the fixed sleeve; the buffer spring is sleeved on the lower side of the outer wall of the buffer rod; the lower surface of the floor buffer seat is glued with an anti-skid pad.
Preferably, the airborne laser radar equipment shell is connected to the lower end between the connecting frames through bolts.
Preferably, the adjusting rod, the supporting tube and the adjusting bolt are two, and the supporting tubes are respectively connected to the left side and the right side of the upper part of the unmanned aerial vehicle control main body through the longitudinal lower end threads.
Preferably, the lower end of the buffer rod is in threaded connection with the middle part inside the floor buffer seat.
Preferably, the adjusting nut is arranged at the upper part of the fixing sleeve.
Preferably, adjusting nut, buffer rod, fixed sleeving, buffer spring, the buffer seat that falls to the ground and slipmat all adopt a plurality ofly to fixed sleeving vertical bolted connection respectively falls to the seat about both ends.
Preferably, the buffer spring is a cylindrical stainless steel spring and is arranged between the fixed sleeve and the floor buffer seat.
Preferably, the mounting plate of the airborne laser radar equipment adopts an aluminum alloy plate with mounting holes.
Compared with the prior art, the beneficial effects of the utility model are that:
the utility model discloses in, machine carries laser radar equipment casing, antenna boom pole, the polished rod, the slide pipe, the setting of wing adjusting screw and machine carries laser radar equipment mounting panel is favorable to adjusting the position of machine carries laser radar equipment mounting panel according to the installation demand to in install fixed laser radar equipment, convenient operation.
The utility model discloses in, new forms of energy photoelectric conversion board, the fly leaf, dismantle the bolt, adjust the pole, stay tube and adjusting bolt's setting is favorable to photoelectric conversion, practices thrift electric power, avoids the wasting of resources.
The utility model discloses in, the fly leaf, dismantle the bolt, adjust the pole, stay tube and adjusting bolt's setting is favorable to carrying out position control according to the photoelectric conversion demand, guarantees the power supply effect.
The utility model discloses in, adjusting nut, buffer beam, the fixed sleeving, buffer spring, the setting of the cushion socket and slipmat fall to the ground is favorable to falling to cushion to guarantee unmanned aerial vehicle job stabilization nature, avoid the damage of falling.
The utility model discloses in, the support frame with fall to the ground the setting of seat, be favorable to playing good support stability.
The utility model discloses in, the setting of link, be favorable to connecting fixedly, convenient operation.
The utility model discloses in, wireless control module's setting, be favorable to wireless control, convenient operation.
The utility model discloses in, the setting of mounting panel, be favorable to the installation to dismantle, convenient maintenance.
Drawings
Fig. 1 is a schematic structural diagram of the present invention;
fig. 2 is a schematic structural diagram of the adjustable lidar equipment mounting plate structure of the present invention;
fig. 3 is a schematic structural diagram of the adjustable new energy conversion plate structure of the present invention;
fig. 4 is a schematic structural view of the floor buffer type adjustable rod structure of the present invention.
In the figure:
1. a main machine control body of the unmanned aerial vehicle; 2. mounting a plate; 3. a wireless control module; 4. a host; 5. a charger; 6. a storage battery; 7. wings of the unmanned aerial vehicle; 8. a drive motor; 9. a fan blade; 10. a support frame; 11. a floor base; 12. a connecting frame; 13. an adjustable laser radar equipment mounting plate structure; 131. an airborne laser radar equipment housing; 132. an antenna mast; 133. a polish rod; 134. a slide pipe; 135. a thumb adjustment screw; 136. an airborne laser radar equipment mounting plate; 14. an adjustable new energy conversion plate structure; 141. a new energy photoelectric conversion panel; 142. a movable plate; 143. disassembling the bolt; 144. adjusting a rod; 145. supporting a tube; 146. adjusting the bolt; 15. a floor buffer type adjustable rod structure; 151. adjusting the nut; 152. a buffer rod; 153. fixing the sleeve; 154. a buffer spring; 155. a floor buffer seat; 156. a non-slip mat.
Detailed Description
The utility model is described in detail with reference to the accompanying drawings, as shown in fig. 1 and fig. 2, an improved airborne laser radar device based on an unmanned aerial vehicle comprises an unmanned aerial vehicle machine control main body 1, a mounting plate 2, a wireless control module 3, a host computer 4, a charger 5, a storage battery 6, an unmanned aerial vehicle wing 7, a driving motor 8, a fan blade 9, a support frame 10, a landing seat 11, a connecting frame 12, an adjustable laser radar device mounting plate structure 13, an adjustable new energy conversion plate structure 14 and a landing buffer type adjustable rod structure 15, wherein the unmanned aerial vehicle machine control main body 1 is internally screwed with the mounting plate 2, and the wireless control module 3, the host computer 4, the charger 5 and the storage battery 6 are sequentially screwed with the front part of the mounting plate 2 from left to right; the periphery of the outer side of the unmanned aerial vehicle machine control main body 1 is transversely connected with unmanned aerial vehicle wings 7 through bolts, the outer side of the lower parts of the unmanned aerial vehicle wings 7 is connected with a driving motor 8 through bolts, and the upper end of an output shaft of the driving motor 8 is connected with a fan blade 9 through a key; the left end and the right end of the front side of the lower part of the unmanned aerial vehicle machine control main body 1 and the front end and the rear end of the rear side of the lower part are respectively provided with a ground seat 11 through a support frame 10; the four corners of the bottom of the unmanned aerial vehicle machine control main body 1 are all connected with connecting frames 12 through bolts; the connecting frame 12 is connected with an adjustable laser radar equipment mounting plate structure 13; the adjustable new energy conversion plate structure 14 is connected with the unmanned aerial vehicle main control body 1; the floor buffer type adjustable rod structure 15 is connected with the floor seat 11; the adjustable laser radar equipment mounting plate structure 13 comprises an airborne laser radar equipment shell 131, an antenna support rod 132, a polished rod 133, a sliding pipe 134, a wing-shaped adjusting screw 135 and an airborne laser radar equipment mounting plate 136, wherein the antenna support rod 132 is connected to the middle part of the upper part of the airborne laser radar equipment shell 131 through a bolt; the upper side and the lower side of the interior of the airborne laser radar equipment shell 131 are transversely connected with a polished rod 133 through bolts; the outer wall of the polish rod 133 is sleeved with a slide pipe 134 and is fastened and connected through a wing-shaped adjusting screw 135; inboard screwed connection between slide pipe 134 have airborne laser radar equipment mounting panel 136, according to the installation demand of laser radar equipment, loosen wing adjusting screw 135, can adjust the slide pipe 134 position of polished rod 133 outer wall, confirm airborne laser radar equipment mounting panel 136 position after, lock wing adjusting screw 135, can install laser radar equipment, satisfy the installation demand.
In this embodiment, referring to fig. 3, the adjustable new energy conversion plate structure 14 includes a new energy photoelectric conversion plate 141, a movable plate 142, a detaching bolt 143, an adjusting rod 144, a supporting tube 145 and an adjusting bolt 146, wherein the new energy photoelectric conversion plate 141 is disposed on the upper surface of the movable plate 142 and is fastened and connected by the detaching bolt 143; the adjusting rod 144 is longitudinally inserted in the supporting tube 145 and is fastened and connected by the adjusting bolt 146, the other end of the adjusting rod 144 is connected to the left side and the right side of the lower portion of the movable plate 142 by bolts, the adjusting bolt 146 is loosened according to the photoelectric conversion requirement, the adjusting rod 144 can be adjusted in height in the supporting tube 145, the adjusting bolt 146 is locked after the height position is determined, and finally, the photoelectric conversion operation can be performed through the new energy photoelectric conversion plate 141, so that the resource waste is avoided.
In this embodiment, referring to fig. 4, the floor buffer type adjustable rod structure 15 includes an adjusting nut 151, a buffer rod 152, a fixing sleeve 153, a buffer spring 154, a floor buffer seat 155 and a non-slip pad 156, wherein the adjusting nut 151 is screwed on the upper portion of the outer wall of the buffer rod 152; the buffer rod 152 is longitudinally inserted into the fixing sleeve 153; the buffer spring 154 is sleeved on the lower side of the outer wall of the buffer rod 152; ground buffer seat 155 lower surface glue joint have slipmat 156, when unmanned aerial vehicle fell to the ground, the accessible fell to the ground buffer seat 155 and slipmat 156 contact ground to make buffer spring 154 buffering action, and then make buffer rod 152 at the inside buffering action of fixed sleeve 153, with the stationarity that guarantees that unmanned aerial vehicle fell to the ground, avoid the damage of falling, can adjust the shock attenuation range through adjusting nut 151, guarantee to fall to the ground stability.
In this embodiment, specifically, the housing 131 of the airborne laser radar device is bolted to the lower end of the connecting frame 12.
In this embodiment, specifically, two adjusting rods 144, two supporting tubes 145 and two adjusting bolts 146 are adopted, and the supporting tubes 145 are respectively connected to the left and right sides of the upper part of the drone machine control main body 1 through the longitudinal lower ends of the supporting tubes.
In this embodiment, specifically, the lower end of the buffer rod 152 is screwed to the middle inside the floor buffer base 155.
In this embodiment, specifically, the adjusting nut 151 is disposed on the upper portion of the fixing sleeve 153.
In this embodiment, specifically, the adjusting nut 151, the buffer rod 152, the fixing sleeve 153, the buffer spring 154, the floor buffer seat 155 and the anti-slip pad 156 are all provided in plurality, and the fixing sleeve 153 is respectively and longitudinally bolted to the left end and the right end of the floor seat 11.
In this embodiment, specifically, the buffer spring 154 is a cylindrical stainless steel spring and is disposed between the fixing sleeve 153 and the floor buffer base 155.
In this embodiment, specifically, the mounting plate 136 of the airborne laser radar device is an aluminum alloy plate with mounting holes.
In this embodiment, specifically, the new energy photoelectric conversion panel 141 is a single crystal silicon solar panel.
In this embodiment, specifically, the movable plate 142 is a hollow aluminum plate.
In this embodiment, specifically, the buffer rod 152 is a stainless steel screw.
In this embodiment, the anti-slip pad 156 is a rubber pad.
In this embodiment, specifically, the driving motor 8 and the wireless control module 3 are connected to the host 4 through wires, and the new energy photoelectric conversion panel 141, the charger 5 and the storage battery 6 are connected in series through wires.
In this embodiment, the drive motor 8 is a 775 type motor.
In this embodiment, specifically, the wireless control module 3 adopts an HC-08 type bluetooth module and is connected to the smart phone through a wireless signal.
In this embodiment, specifically, the host 4 employs an stm32f103 type single chip microcomputer.
In this embodiment, specifically, the charger 5 is a 12V small photovoltaic charger, and the storage battery 6 is a 12V rechargeable lithium ion storage battery.
Principle of operation
In the utility model, according to the installation requirement of laser radar equipment, the wing-shaped adjusting screw 135 is loosened, the position of the sliding pipe 134 of the outer wall of the polished rod 133 can be adjusted, after the position of the mounting plate 136 of the airborne laser radar equipment is determined, the wing-shaped adjusting screw 135 is locked, the laser radar equipment can be mounted, the mounting requirement is met, according to the photoelectric conversion requirement, the adjusting bolt 146 is loosened, the height adjusting work of the adjusting rod 144 in the supporting pipe 145 can be carried out, after the height position is determined, the adjusting bolt 146 is locked, finally, the photoelectric conversion operation can be carried out through the new energy photoelectric conversion plate 141, the resource waste is avoided, when the unmanned aerial vehicle falls to the ground, the ground can be contacted with the anti-slip pad 156 through the floor buffer seat 155, the buffer spring 154 can buffer the buffer action, the buffer action of the buffer rod 152 in the fixing sleeve 153 can be, the damping amplitude can be adjusted by adjusting the nut 151, and the landing stability is ensured.
Utilize technical scheme, or technical personnel in the field are in the utility model discloses under technical scheme's the inspiration, design similar technical scheme, and reach above-mentioned technological effect, all fall into the utility model discloses a protection scope.
Claims (10)
1. An improved airborne laser radar device based on an unmanned aerial vehicle is characterized by comprising an unmanned aerial vehicle machine control main body (1), a mounting plate (2), a wireless control module (3), a main machine (4), a charger (5), a storage battery (6), unmanned aerial vehicle wings (7), a driving motor (8), fan blades (9), a support frame (10), a landing seat (11) and a connecting frame (12), an adjustable laser radar equipment mounting plate structure (13), an adjustable new energy conversion plate structure (14) and a floor buffer type adjustable rod structure (15), the inner part of the unmanned aerial vehicle machine control main body (1) is connected with a mounting plate (2) through screws, the front part of the mounting plate (2) is sequentially connected with a wireless control module (3), a host (4), a charger (5) and a storage battery (6) by screws from left to right; the periphery of the outer side of the unmanned aerial vehicle machine control main body (1) is transversely connected with unmanned aerial vehicle wings (7) through bolts, the outer side of the lower part of the unmanned aerial vehicle wings (7) is connected with a driving motor (8) through bolts, and the upper end of an output shaft of the driving motor (8) is connected with a fan blade (9) through a key; the left end and the right end of the lower front side of the unmanned aerial vehicle machine control main body (1) and the front end and the rear end of the lower rear side are respectively provided with a ground seat (11) through a support frame (10); the four corners of the bottom of the unmanned aerial vehicle machine control main body (1) are connected with connecting frames (12) through bolts; the connecting frame (12) is connected with the adjustable laser radar equipment mounting plate structure (13); the adjustable new energy conversion plate structure (14) is connected with the unmanned aerial vehicle main control body (1); the floor buffer type adjustable rod structure (15) is connected with the floor seat (11); the adjustable laser radar equipment mounting plate structure (13) comprises an airborne laser radar equipment shell (131), an antenna support rod (132), a polished rod (133), a sliding pipe (134), a wing-shaped adjusting screw (135) and an airborne laser radar equipment mounting plate (136), wherein the antenna support rod (132) is connected to the middle part of the upper part of the airborne laser radar equipment shell (131) through a bolt; the upper side and the lower side of the interior of the airborne laser radar equipment shell (131) are both connected with a polished rod (133) through transverse bolts; the outer wall of the polish rod (133) is sleeved with a slide pipe (134) and is fixedly connected and arranged through a wing-shaped adjusting screw (135); and an airborne laser radar equipment mounting plate (136) is connected between the slide pipes (134) through screws on the inner side.
2. The improved airborne lidar apparatus based on unmanned aerial vehicle of claim 1, wherein the adjustable new energy conversion plate structure (14) comprises a new energy photoelectric conversion plate (141), a movable plate (142), a detaching bolt (143), an adjusting rod (144), a supporting tube (145) and an adjusting bolt (146), the new energy photoelectric conversion plate (141) is disposed on the upper surface of the movable plate (142) and is fastened and connected to the movable plate (142) through the detaching bolt (143); the adjusting rods (144) are longitudinally inserted in the supporting tubes (145) and are fastened and connected through adjusting bolts (146), and the other ends of the adjusting rods are all connected to the left side and the right side of the lower portion of the movable plate (142) through bolts.
3. The improved airborne lidar apparatus based on unmanned aerial vehicle of claim 1, wherein said landing buffer adjustable rod structure (15) comprises an adjusting nut (151), a buffer rod (152), a fixed sleeve (153), a buffer spring (154), a landing buffer seat (155) and a non-slip pad (156), said adjusting nut (151) is screwed on the upper portion of the outer wall of the buffer rod (152); the buffer rod (152) is longitudinally inserted into the fixing sleeve (153); the buffer spring (154) is sleeved on the lower side of the outer wall of the buffer rod (152); the lower surface of the floor buffer seat (155) is glued with an anti-skid pad (156).
4. Improved drone-based airborne lidar equipment according to claim 1, characterized in that said airborne lidar equipment housing (131) is bolted at the lower end between the connection frames (12).
5. The improved airborne lidar apparatus based on unmanned aerial vehicle of claim 2, wherein there are two adjusting rods (144), two supporting tubes (145) and two adjusting bolts (146), and the supporting tubes (145) are respectively screwed at the lower longitudinal ends on the left and right sides of the upper part of the unmanned aerial vehicle control body (1).
6. The improved airborne lidar apparatus of claim 3, wherein said bumper bar (152) is threaded at a central location within said landing bumper base (155) at a lower end thereof.
7. The improved airborne lidar apparatus based on unmanned aerial vehicle of claim 3, wherein said adjusting nut (151) is disposed at an upper portion of the retaining sleeve (153).
8. The improved airborne lidar apparatus based on unmanned aerial vehicle of claim 3, wherein said adjusting nut (151), said bumper bar (152), said fixing sleeve (153), said cushion spring (154), said landing cushion seat (155) and said non-slip mat (156) are plural, and said fixing sleeve (153) is longitudinally bolted to the left and right ends of said landing seat (11).
9. The improved airborne lidar apparatus of claim 3, wherein said bumper spring (154) is a cylindrical stainless steel spring and is disposed between the fixed sleeve (153) and the landing bumper (155).
10. The improved drone-based airborne lidar apparatus of claim 1, wherein the airborne lidar apparatus mounting plate (136) is an aluminum alloy plate with mounting holes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022234212.XU CN213036090U (en) | 2020-10-09 | 2020-10-09 | Follow-on airborne laser radar equipment based on unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022234212.XU CN213036090U (en) | 2020-10-09 | 2020-10-09 | Follow-on airborne laser radar equipment based on unmanned aerial vehicle |
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| CN213036090U true CN213036090U (en) | 2021-04-23 |
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| CN202022234212.XU Active CN213036090U (en) | 2020-10-09 | 2020-10-09 | Follow-on airborne laser radar equipment based on unmanned aerial vehicle |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114183674A (en) * | 2021-12-04 | 2022-03-15 | 深圳市广通测绘有限公司 | Small-size airborne laser radar scanning measuring remove stabilising arrangement for base |
| CN114572400A (en) * | 2022-03-30 | 2022-06-03 | 桂林电子科技大学 | Logistics unmanned aerial vehicle based on laser radar |
-
2020
- 2020-10-09 CN CN202022234212.XU patent/CN213036090U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114183674A (en) * | 2021-12-04 | 2022-03-15 | 深圳市广通测绘有限公司 | Small-size airborne laser radar scanning measuring remove stabilising arrangement for base |
| CN114183674B (en) * | 2021-12-04 | 2024-05-14 | 深圳市广通测绘有限公司 | Small-size airborne laser radar scanning measurement's stabilising arrangement for mobile base |
| CN114572400A (en) * | 2022-03-30 | 2022-06-03 | 桂林电子科技大学 | Logistics unmanned aerial vehicle based on laser radar |
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