CN117682119A - Unmanned aerial vehicle remote sensing mapping device - Google Patents
Unmanned aerial vehicle remote sensing mapping device Download PDFInfo
- Publication number
- CN117682119A CN117682119A CN202311815908.3A CN202311815908A CN117682119A CN 117682119 A CN117682119 A CN 117682119A CN 202311815908 A CN202311815908 A CN 202311815908A CN 117682119 A CN117682119 A CN 117682119A
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- fixedly connected
- driving motor
- remote sensing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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- 238000013507 mapping Methods 0.000 title claims abstract description 16
- 238000004140 cleaning Methods 0.000 claims abstract description 27
- 241000883990 Flabellum Species 0.000 claims description 4
- 230000005540 biological transmission Effects 0.000 claims description 4
- 230000000712 assembly Effects 0.000 abstract description 6
- 238000000429 assembly Methods 0.000 abstract description 6
- 230000009286 beneficial effect Effects 0.000 abstract description 4
- 230000003139 buffering effect Effects 0.000 description 5
- 230000002349 favourable effect Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000002035 prolonged effect Effects 0.000 description 2
- 239000000428 dust Substances 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/385—Variable incidence wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U60/00—Undercarriages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Remote Sensing (AREA)
- Electric Suction Cleaners (AREA)
Abstract
The invention discloses an unmanned aerial vehicle remote sensing mapping device, which belongs to the technical field of unmanned aerial vehicle remote sensing and comprises an unmanned aerial vehicle body, a plurality of mounting plates arranged on the outer ring of the unmanned aerial vehicle body, and a second driving motor arranged on the mounting plates, wherein the output shaft of the second driving motor is fixedly connected with fan blades, a support frame is arranged at the bottom of the unmanned aerial vehicle body, a first driving motor is sleeved inside the unmanned aerial vehicle body and the support frame, the output shaft of the first driving motor is fixedly connected with a remote sensor, cleaning assemblies connected with the bottom of the unmanned aerial vehicle body are arranged on two sides of the remote sensor and are used for cleaning the surfaces of the remote sensor, and adjustable wing assemblies are arranged on two sides of the unmanned aerial vehicle body. The invention is convenient and stable to fall, avoids rigid collision, can automatically clean the remote sensor, ensures that the remote sensor does not need to fall down to be cleaned manually, is beneficial to high-efficiency continuous work, can adjust the angle of the fixed wing, and is beneficial to prolonging the dead time.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicle remote sensing, and particularly relates to an unmanned aerial vehicle remote sensing mapping device.
Background
The remote sensor is an instrument for remotely detecting electromagnetic waves radiated or reflected by ground objects and environments, and is usually combined with an unmanned person to realize high-altitude remote sensing mapping. The unmanned plane is a unmanned plane which is controlled by using radio remote control equipment and a self-provided program control device, is not provided with a cabin, is provided with an autopilot, a program control device and other equipment, is tracked, positioned, remotely controlled, remotely measured and digitally transmitted by personnel on the ground, a naval vessel or a master remote control station through radar and other equipment, and is carried on the unmanned plane so that the remote sensing plotter can better finish the work of drawing the ground topography or other figures.
When current unmanned aerial vehicle remote sensing survey and drawing, utilize the remote sensor on the unmanned aerial vehicle to survey and drawing work, and the remote sensor is at the high altitude during operation, and its surface can adhere to the dust, and long-time unmanned aerial vehicle cleaning can influence the precision of shooting, traditional unmanned aerial vehicle lacks the buffer measure moreover when taking off and land to and when parallel flight, the lift provides by the flabellum completely, leads to the output of flabellum great, increases the consumption of electric energy, for this we have proposed an unmanned aerial vehicle remote sensing survey and drawing device.
Disclosure of Invention
In order to solve the problems, the invention aims to provide an unmanned aerial vehicle remote sensing mapping device.
In order to achieve the above purpose, the invention provides an unmanned aerial vehicle remote sensing mapping device, which comprises an unmanned aerial vehicle body, a plurality of mounting plates arranged on the outer ring of the unmanned aerial vehicle body, and a second driving motor arranged on the mounting plates, wherein the output shaft of the second driving motor is fixedly connected with fan blades, a support frame is arranged at the bottom of the unmanned aerial vehicle body, a first driving motor is sleeved inside the unmanned aerial vehicle body and the support frame, a remote sensor is fixedly connected with the output shaft of the first driving motor, cleaning components connected with the bottom of the unmanned aerial vehicle body are arranged on two sides of the remote sensor and used for cleaning the surface of the remote sensor, adjustable wing components are arranged on two sides of the unmanned aerial vehicle body and used for adjusting the angle of wings to improve the flying lifting force, and a buffer component is arranged at the bottom of the unmanned aerial vehicle body and used for providing buffering when the unmanned aerial vehicle body falls.
Preferably, the adjustable wing subassembly includes the fixing base of fixed connection in unmanned aerial vehicle organism one side, fixedly connected with push rod motor on the fixing base, the output shaft fixedly connected with double-sided rack of push rod motor, the both sides of double-sided rack are equipped with the pivot of being connected with the mounting panel rotation, the outside fixed cover of pivot is equipped with a plurality of fixed wings, one side fixed cover of pivot is equipped with the gear, and gear and double-sided rack meshing transmission.
Preferably, the buffer assembly comprises an air pump fixedly sleeved at the bottom of the unmanned aerial vehicle body, an air inlet pipe is fixedly connected with an air outlet of the air pump, two air bags communicated with the air inlet pipe are fixedly connected with the bottom end of the air inlet pipe, a fixed cover is arranged at the top of each air bag, a bottom plate is fixedly connected with the bottom of the fixed cover, and the bottom plate is fixedly connected with the support frame.
Preferably, the cleaning assembly comprises a fixed plate fixedly connected to the bottom of the unmanned aerial vehicle body, a screw is sleeved on the internal thread of the fixed plate, one end of the screw is fixedly connected with a cleaning sponge, the other end of the screw is fixedly connected with a gear column, a servo motor fixedly connected with the fixed plate is arranged below the gear column, an output shaft of the servo motor is fixedly connected with a driving gear, and the driving gear is meshed with the gear column for transmission.
Preferably, the bottom of support frame is equipped with two auxiliary stay components, auxiliary stay components includes the rotor plate of being connected with the support frame rotation, two be equipped with the horizontal pole between the rotor plate, fixedly connected with third driving motor on the support frame, and third driving motor drive rotor plate rotates.
Preferably, the bottom plate is provided with a mounting hole, the air bag is sleeved in the mounting hole, and the air bag is of a cylindrical structure.
Preferably, the bottom of organism has seted up the fixed slot, and first driving motor is fixed to be set up in the mounting groove.
The unmanned aerial vehicle remote sensing mapping device provided by the invention has the following beneficial effects:
1. the angle of the fixed wing is adjusted through the adjustable wing assembly, the fixed wing is adjusted to be vertical when the fixed wing is lifted, the resistance when lifted is reduced, and the fixed wing is adjusted to be horizontal when the fixed wing is horizontally flown, so that the lift force when the fixed wing is flown is improved, and the dead time is prolonged;
2. the buffer assembly is used for conveniently buffering the unmanned aerial vehicle in landing, so that collision damage of the unmanned aerial vehicle caused by rigid landing is avoided, and meanwhile, the stability in landing is ensured through the auxiliary supporting assembly, and dumping is avoided;
3. the surface of the remote sensor can be cleaned through the cleaning component, so that the remote sensor is convenient to automatically clean in high-altitude operation, does not need to be manually cleaned by falling, and is beneficial to high-efficiency continuous work;
to sum up, this scheme simple structure, novel in design not only makes things convenient for stable the descending, avoids the rigidity collision, can also carry out self-cleaning to the remote sensor moreover, guarantees not to need to drop down and get down manual cleaning, is favorable to high-efficient continuous operation, can also adjust the angle of fixed wing moreover, is favorable to prolonging the dead time.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention and do not constitute a limitation on the invention.
In the drawings:
fig. 1 is a schematic elevational view of the present invention.
Fig. 2 is a schematic side view of the present invention.
Fig. 3 is a schematic top perspective view of the present invention.
Fig. 4 is a schematic bottom perspective view of the present invention.
FIG. 5 is a schematic perspective view of an adjustable wing assembly of the present invention.
Fig. 6 is a schematic perspective view of a buffering assembly according to the present invention.
Fig. 7 is a schematic perspective view of a cleaning assembly according to the present invention.
In the figure: 1 unmanned aerial vehicle organism, 2 support frames, 3 first driving motor, 4 remote sensor, 5 mounting panels, 6 second driving motor, 7 flabellum, 8 adjustable wing subassembly, 801 pivot, 802 fixed wing, 803 gear, 804 fixing base, 805 push rod motor, 806 double-sided rack, 9 buffer assembly, 901 air pump, 902 intake pipe, 903 gasbag, 904 fixed cover, 10 clean subassembly, 1001 fixed plate, 1002 screw rod, 1003 clean sponge, 1004 gear post, 1005 servo motor, 1006 drive gear, 11 rotor plate, 12 horizontal pole, 13 third driving motor, 14 bottom plate.
Detailed Description
In order to more clearly illustrate the general inventive concept, a detailed description is given below by way of example with reference to the accompanying drawings.
In the description of the present invention, it should be understood that the terms "center," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "axial," "radial," "circumferential," and the like indicate orientations or positional relationships based on the orientation or positional relationships shown in the drawings, merely to facilitate describing the present invention and simplify the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present invention.
Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the present invention, the meaning of "a plurality" is two or more, unless explicitly defined otherwise.
In the present invention, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; the device can be mechanically connected, electrically connected and communicated; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art according to the specific circumstances.
In the present invention, unless expressly stated or limited otherwise, a first feature "up" or "down" a second feature may be the first and second features in direct contact, or the first and second features in indirect contact via an intervening medium. In the description of the present specification, the description with reference to the terms "one aspect," "some aspects," "examples," "specific examples," or "some examples," etc., means that a particular feature, structure, material, or characteristic described in connection with the aspect or example is included in at least one aspect or example of the present invention. In this specification, the schematic representations of the above terms are not necessarily for the same scheme or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more aspects or examples.
As shown in fig. 1 to 7, the embodiment of the invention provides an unmanned aerial vehicle remote sensing mapping device, which comprises an unmanned aerial vehicle body 1, a plurality of mounting plates 5 arranged on the outer ring of the unmanned aerial vehicle body 1, and a second driving motor 6 arranged on the mounting plates 5, wherein the output shaft of the second driving motor 6 is fixedly connected with fan blades 7, the bottom of the unmanned aerial vehicle body 1 is provided with a supporting frame 2, the inner sleeves of the unmanned aerial vehicle body 1 and the supporting frame 2 are provided with a first driving motor 3, the output shaft of the first driving motor 3 is fixedly connected with a remote sensor 4, two sides of the remote sensor 4 are provided with cleaning assemblies 10 connected with the bottom of the unmanned aerial vehicle body 1, the cleaning assemblies 10 are used for cleaning the surfaces of the remote sensor 4, two sides of the unmanned aerial vehicle body 1 are provided with adjustable wing assemblies 8, the adjustable wing assemblies 8 are used for adjusting the angles of wings to improve the flying lift force, the bottom of the unmanned aerial vehicle body 1 is provided with a buffer assembly 9, and the buffer assembly 9 is used for providing buffering when the unmanned aerial vehicle body 1 falls.
As shown in fig. 5, the adjustable wing assembly 8 includes a fixed seat 804 fixedly connected to one side of the unmanned aerial vehicle body 1, a push rod motor 805 is fixedly connected to the fixed seat 804, a double-sided rack 806 is fixedly connected to an output shaft of the push rod motor 805, rotating shafts 801 rotationally connected to the mounting plate 5 are arranged on two sides of the double-sided rack 806, a plurality of fixed wings 802 are fixedly sleeved on the outer portion of the rotating shafts 801, a gear 803 is fixedly sleeved on one side of the rotating shafts 801, the gear 803 is meshed with the double-sided rack 806 to drive the double-sided rack 806 to lift, the double-sided rack 806 drives the gear 803 to rotate, and the gear 803 drives the rotating shafts 801 to rotate so as to adjust the angle of the fixed wings 802.
As shown in fig. 6, the buffer assembly 9 includes an air pump 901 fixedly sleeved at the bottom of the unmanned aerial vehicle body 1, an air outlet of the air pump 901 is fixedly connected with an air inlet pipe 902, two air bags 903 communicated with the air inlet pipe 902 are fixedly connected at the bottom end of the air inlet pipe 902, a fixed cover 904 is arranged at the top of the air bags 903, a bottom plate 14 is fixedly connected at the bottom of the fixed cover 904, the bottom plate 14 is fixedly connected with the support frame 2, and the air pump 901 can be used for inflating the air bags 903 through the air inlet pipe 902, so that buffering is performed through the air bags 903.
As shown in fig. 7, the cleaning assembly 10 includes a fixing plate 1001 fixedly connected to the bottom of the unmanned aerial vehicle body 1, a screw 1002 is sleeved on the internal thread of the fixing plate 1001, one end of the screw 1002 is fixedly connected with a cleaning sponge 1003, the other end of the screw 1002 is fixedly connected with a gear column 1004, a servo motor 1005 fixedly connected to the fixing plate 1001 is arranged below the gear column 1004, an output shaft of the servo motor 1005 is fixedly connected with a driving gear 1006, the driving gear 1006 is meshed with the gear column 1004, the servo motor 1005 drives the driving gear 1006 to rotate by 90 degrees, the driving gear 1006 drives the gear column 1004 to rotate by 90 degrees, the screw 1002 is driven to rotate, the screw 1002 can drive the cleaning sponge 1003 to rotate from a horizontal state to a vertical state, at the moment, the cleaning sponge 1003 can be close to the remote sensor 4, thus the first driving motor 3 drives the remote sensor 4 to rotate to automatically complete cleaning, and the rotation level of the cleaning sponge 1003 can avoid interference to the remote sensor 4 when cleaning is not needed.
As shown in fig. 3, two auxiliary support components are arranged at the bottom of the support frame 2, each auxiliary support component comprises a rotating plate 11 rotationally connected with the support frame 2, a cross rod 12 is arranged between the two rotating plates 11, a third driving motor 13 is fixedly connected to the support frame 2, the third driving motor 13 drives the rotating plates 11 to rotate, so that the rotating plates 11 can horizontally assist the unmanned aerial vehicle to stably fall, and wind resistance can be reduced when the rotating plates 11 rotate vertically.
As shown in fig. 3, the bottom plate 14 is provided with a mounting hole, the air bag 903 is sleeved in the mounting hole, and the air bag 903 has a cylindrical structure.
As shown in fig. 1, a fixing groove is formed in the bottom of the machine body 1, and the first driving motor 3 is fixedly arranged in the mounting groove.
Working principle: the double-sided rack 806 is driven to lift through the push rod motor 805, the double-sided rack 806 drives the gear 803 to rotate, the gear 803 drives the rotating shaft 801 to rotate, the angle of the fixed wing 802 is adjusted, when the double-sided rack 806 moves downwards, the fixed wing 802 which is horizontally arranged is driven to rotate to be in a vertical state, the unmanned aerial vehicle can lift, wind resistance is reduced, when the unmanned aerial vehicle horizontally flies, the double-sided rack 806 drives the fixed wing 802 to rotate horizontally, lifting force is improved by the fixed wing 802, thereby the output power of the fan blade 7 is reduced, the dead time of the unmanned aerial vehicle is prolonged, the second driving motor 6 drives the fan blade 7 to rotate to fly, when the remote sensing operation is carried out at high altitude, remote sensing device 4 carries out remote sensing mapping, when the surface of the remote sensor 4 needs cleaning, the servo motor 1005 drives the driving gear to rotate 90 degrees, the driving gear 1006 drives the gear column 1004 to rotate 90 degrees, and then the screw 1002 drives the screw 1003 to rotate, the cleaning sponge 1003 rotates to be in a vertical state, the screw 1003 drives the cleaning sponge 1003 to rotate and simultaneously horizontally to be close to the remote sensor 4, the first driving motor 3 drives the remote sensor 4 to rotate to automatically, thereby the fan blade 7 rotates, the fan plate 903 does not need to rotate, the air inlet pipe 903 can be driven to rotate, and the air inlet pipe 903 can be prevented from rotating to rotate to the air pump 11 through the air pump 11.
In this specification, each embodiment is described in a progressive manner, and identical and similar parts of each embodiment are all referred to each other, and each embodiment mainly describes differences from other embodiments. In particular, for system embodiments, since they are substantially similar to method embodiments, the description is relatively simple, as relevant to see a section of the description of method embodiments.
The foregoing is merely exemplary of the present invention and is not intended to limit the present invention. Various modifications and variations of the present invention will be apparent to those skilled in the art. Any modification, equivalent replacement, improvement, etc. which come within the spirit and principles of the invention are to be included in the scope of the claims of the present invention.
Claims (7)
1. The utility model provides an unmanned aerial vehicle remote sensing survey and drawing device, includes unmanned aerial vehicle organism (1), sets up a plurality of mounting panels (5) at unmanned aerial vehicle organism (1) outer lane to and set up second driving motor (6) on mounting panel (5), the output shaft fixedly connected with flabellum (7) of second driving motor (6), a serial communication port, the bottom of unmanned aerial vehicle organism (1) is equipped with support frame (2), the inside cover of unmanned aerial vehicle organism (1) and support frame (2) is equipped with first driving motor (3), the output shaft fixedly connected with remote sensor (4) of first driving motor (3), the both sides of remote sensor (4) are equipped with clean subassembly (10) of being connected with the bottom of unmanned aerial vehicle organism (1), and this clean subassembly (10) are used for cleaning the surface of remote sensor (4), the both sides of unmanned aerial vehicle organism (1) are equipped with adjustable wing subassembly (8), and the angle that this adjustable wing subassembly (8) is used for adjusting improves the lift of flight, the bottom of unmanned aerial vehicle organism (1) is equipped with buffer assembly (9), and this buffer assembly (9) are used for providing when unmanned aerial vehicle organism (1) falls.
2. The unmanned aerial vehicle remote sensing mapping device according to claim 1, wherein the adjustable wing assembly (8) comprises a fixed seat (804) fixedly connected to one side of the unmanned aerial vehicle body (1), a push rod motor (805) is fixedly connected to the fixed seat (804), a double-sided rack (806) is fixedly connected to an output shaft of the push rod motor (805), rotating shafts (801) rotationally connected with the mounting plate (5) are arranged on two sides of the double-sided rack (806), a plurality of fixed wings (802) are fixedly sleeved on the outer portion of the rotating shafts (801), a gear (803) is fixedly sleeved on one side of the rotating shafts (801), and the gear (803) is in meshed transmission with the double-sided rack (806).
3. The unmanned aerial vehicle remote sensing mapping device according to claim 1, wherein the buffer assembly (9) comprises an air pump (901) fixedly sleeved at the bottom of the unmanned aerial vehicle body (1), an air outlet of the air pump (901) is fixedly connected with an air inlet pipe (902), the bottom end of the air inlet pipe (902) is fixedly connected with two air bags (903) communicated with the air inlet pipe, the top of each air bag (903) is provided with a fixed cover (904), the bottom of each fixed cover (904) is fixedly connected with a bottom plate (14), and the bottom plate (14) is fixedly connected with the supporting frame (2).
4. The unmanned aerial vehicle remote sensing mapping device according to claim 1, wherein the cleaning assembly (10) comprises a fixed plate (1001) fixedly connected to the bottom of the unmanned aerial vehicle body (1), a screw (1002) is sleeved on the internal thread of the fixed plate (1001), one end of the screw (1002) is fixedly connected with a cleaning sponge (1003), the other end of the screw (1002) is fixedly connected with a gear column (1004), a servo motor (1005) fixedly connected with the fixed plate (1001) is arranged below the gear column (1004), a driving gear (1006) is fixedly connected to an output shaft of the servo motor (1005), and the driving gear (1006) is in meshed transmission with the gear column (1004).
5. The unmanned aerial vehicle remote sensing mapping device according to claim 1, wherein two auxiliary support components are arranged at the bottom of the support frame (2), each auxiliary support component comprises a rotating plate (11) rotationally connected with the support frame (2), a cross rod (12) is arranged between the two rotating plates (11), a third driving motor (13) is fixedly connected to the support frame (2), and the third driving motor (13) drives the rotating plates (11) to rotate.
6. An unmanned aerial vehicle remote sensing mapping device according to claim 3, wherein the base plate (14) is provided with a mounting hole, the air bag (903) is sleeved in the mounting hole, and the air bag (903) has a cylindrical structure.
7. The unmanned aerial vehicle remote sensing mapping device according to claim 1, wherein a fixing groove is formed in the bottom of the machine body (1), and the first driving motor (3) is fixedly arranged in the mounting groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311815908.3A CN117682119A (en) | 2023-12-27 | 2023-12-27 | Unmanned aerial vehicle remote sensing mapping device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311815908.3A CN117682119A (en) | 2023-12-27 | 2023-12-27 | Unmanned aerial vehicle remote sensing mapping device |
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| Publication Number | Publication Date |
|---|---|
| CN117682119A true CN117682119A (en) | 2024-03-12 |
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ID=90138834
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202311815908.3A Pending CN117682119A (en) | 2023-12-27 | 2023-12-27 | Unmanned aerial vehicle remote sensing mapping device |
Country Status (1)
| Country | Link |
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| CN (1) | CN117682119A (en) |
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| US20140103158A1 (en) * | 2012-10-12 | 2014-04-17 | Benjamin Lawrence Berry | AirShip Endurance VTOL UAV and Solar Turbine Clean Tech Propulsion |
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