CN214986135U - Unmanned aerial vehicle descending back position and posture correction mechanism - Google Patents
Unmanned aerial vehicle descending back position and posture correction mechanism Download PDFInfo
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- CN214986135U CN214986135U CN202120099831.4U CN202120099831U CN214986135U CN 214986135 U CN214986135 U CN 214986135U CN 202120099831 U CN202120099831 U CN 202120099831U CN 214986135 U CN214986135 U CN 214986135U
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Abstract
The utility model discloses an unmanned aerial vehicle descending back position and gesture correction mechanism, including rail block one and unmanned aerial vehicle skid clamping mechanism, rail block one's quantity is two, and distributes around being, rail block one's both sides all overlap and are equipped with the connecting plate, the vertical corresponding one side fixedly connected with push rod of two connecting plates, the positive fixed surface of front side rail block one is connected with the rack. The utility model discloses can satisfy unmanned aerial vehicle under the specific environment after falling, the quick correction of posture and position, be convenient for platform or ground fixed establishment carry out effective fixed, can satisfy polytypic unmanned aerial vehicle simultaneously, many sizes descending regional requirement, and unmanned aerial vehicle's automatic quick clamp down under the specific environment is fixed and the pine takes off, adjust the interval and the frame size of fixed hook simultaneously, satisfy polytypic unmanned aerial vehicle's the tight fixed requirement of clamp, unmanned aerial vehicle can't press from both sides the problem of tight fixing according to specific gesture and position after descending under the specific environment has been solved.
Description
Technical Field
The utility model relates to an engineering equipment technical field specifically is an unmanned aerial vehicle falls after position and gesture correction mechanism.
Background
In the actual application process, under the influence of various environments, after the unmanned aerial vehicle falls, the attitude position of the unmanned aerial vehicle has certain deviation, and when the automatic receiver is put in storage, the state after the unmanned aerial vehicle falls is inconvenient for attitude adjustment; so need utilize a mechanism, can correct position and gesture with unmanned aerial vehicle in specific region, be convenient for fix it according to particular position and gesture, the device provides a new position and removes and gesture correction mechanism.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle falls behind position and gesture correction mechanism, it falls behind to possess the unmanned aerial vehicle that can satisfy under the specific environment, the quick correction of posture and position, be convenient for platform or ground fixed establishment carry out effective fixation, can satisfy polytypic unmanned aerial vehicle simultaneously, the regional requirement of many sizes descending, and unmanned aerial vehicle's automatic quick clamp down is fixed and is taken off and take off under the specific environment, adjust fixed hook's interval and frame size simultaneously, satisfy the advantage that polytypic unmanned aerial vehicle presss from both sides the fastening and decides the requirement, unmanned aerial vehicle can't press from both sides the problem of tight fixing according to specific posture and position after descending under the specific environment has been solved.
In order to achieve the above object, the utility model provides a following technical scheme: the mechanism for correcting the position and the posture of the unmanned aerial vehicle after landing comprises a first guide rail slider and a first unmanned aerial vehicle skid clamping mechanism, wherein the first guide rail slider is two and is distributed front and back, connecting plates are sleeved on two sides of the first guide rail slider, push rods are fixedly connected to one sides of the two connecting plates which correspond to each other in the longitudinal direction, racks are fixedly connected to the front surfaces of the first front guide rail slider, a first servo motor reducer is fixedly connected to the front surfaces of the two front connecting plates, a gear meshed with the racks is sleeved on the rear side of the output end of the first servo motor reducer, and a first line following belt is arranged at the bottom of the first servo motor reducer;
unmanned aerial vehicle skid clamping mechanism is located between two guide rail slider one and two push rods, unmanned aerial vehicle skid clamping mechanism includes two frames, and two frames are about distribution, the equal vertical fixedly connected with guide rail slider two in both sides of frame inner chamber, the front side and the rear side of two inner chambers of guide rail slider just are located the front side and the equal fixedly connected with belt pulley in rear side of frame inner chamber, and the cover is equipped with the conveyer belt around two belt pulleys between corresponding one side, the front side on conveyer belt left side surface and the rear side on right side surface all are through bolt fixedly connected with fixed hook, the left rear side fixedly connected with stopper in frame top surface, the top fixedly connected with servo motor speed reducer two of rear side belt pulley.
Preferably, the gear is located at the top of the rack, the inner ring of the connecting plate is in sliding contact with the surface of the first guide rail slider, and two sides of the back surface of the rack are fixedly connected with two sides of the front surface of the first front guide rail slider.
Preferably, the bottom of the second servo motor speed reducer is fixedly connected with the rear side of the top surface of the rack, and the bottom of the output end of the second servo motor speed reducer is fixedly connected with the belt pulley.
Preferably, the bottom of the front side of one side corresponding to the two racks is transversely and fixedly connected with a connecting bottom plate, the bottom of the rear side of one side corresponding to the two racks is transversely provided with a movable plate, the top of the movable plate is fixedly connected with a wire-following belt II, and the right side of the movable plate penetrates through the right side rack and is fixedly connected with a positioning plate.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a set up servo motor speed reducer one, the rack, rail block one, the gear, follow the line area one, the push rod, unmanned aerial vehicle skid clamping mechanism, servo motor speed reducer two, a machine support, rail block two, the fixed hook, the belt pulley, the conveyer belt, the cooperation of stopper and connecting plate is used, can satisfy the unmanned aerial vehicle under the specific environment after falling, the quick correction of posture and position, be convenient for platform or ground fixed establishment carry out effective fixed, can satisfy polytypic unmanned aerial vehicle simultaneously, the regional requirement of multisize descending, and unmanned aerial vehicle's automation under the specific environment presss from both sides tight fixed and pine takes off fast, adjust the interval and the frame size of fixed hook simultaneously, satisfy polytypic unmanned aerial vehicle's the tight fixed requirement of clamp, unmanned aerial vehicle can's the unable fixed problem of clamp according to specific gesture and position after descending under the specific environment has been solved.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is the utility model discloses unmanned aerial vehicle skid clamping mechanism schematic structure.
In the figure: 1 servo motor speed reducer I, 2 racks, 3 guide rail slide block I, 4 gears, 5 following line belt I, 6 push rods, 7 unmanned aerial vehicle skid clamping mechanisms, 71 servo motor speed reducer II, 72 racks, 73 guide rail slide block II, 74 fixing hooks, 75 belt pulleys, 76 connecting bottom plates, 77 conveyor belts, 78 limiters, 79 following line belt II, 710 movable plates, 711 positioning plates and 8 connecting plates.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-2, an unmanned aerial vehicle post-landing position and posture correction mechanism comprises a first guide rail slider 3 and an unmanned aerial vehicle skid clamping mechanism 7, wherein the first guide rail slider 3 is provided with two guide rail sliders which are distributed in the front and back directions, two sides of the first guide rail slider 3 are respectively sleeved with a connecting plate 8, one side of each of the two connecting plates 8 which corresponds to the longitudinal direction is fixedly connected with a push rod 6, a rack 2 is fixedly connected to the front surface of the first front guide rail slider 3, a servo motor reducer 1 is fixedly connected to the front surfaces of the two connecting plates 8 at the front side, a gear 4 meshed with the rack 2 is sleeved on the rear side of the output end of the servo motor reducer 1, and a line following belt 5 is arranged at the bottom of the servo motor reducer 1;
the unmanned aerial vehicle skid clamping mechanism 7 is positioned between the two guide rail sliding blocks I3 and the two push rods 6, the unmanned aerial vehicle skid clamping mechanism 7 comprises two racks 72, the two racks 72 are distributed leftwards and rightwards, two sides of an inner cavity of the rack 72 are longitudinally and fixedly connected with two guide rail sliding blocks 73, the front side and the rear side of the inner cavity of the two guide rail sliding blocks 73 are respectively and fixedly connected with belt pulleys 75, a conveying belt 77 is sleeved between the front and rear corresponding sides of the two belt pulleys 75, the front side of the left side surface and the rear side of the right side surface of the conveying belt 77 are respectively and fixedly connected with a fixed hook 74 through bolts, the rear side of the left side of the top surface of the rack 72 is fixedly connected with a stopper 78, the top of the rear side belt pulley 75 is fixedly connected with a servo motor reducer II 71, the unmanned aerial vehicle skid clamping mechanism 7 is placed at a preset and fixed position of an unmanned aerial vehicle in a landing area, and the length and size of the unmanned aerial vehicle skid clamping mechanism 7 can be changed according to the width of the landing area, through the matching use of a servo motor reducer I1, a rack 2, a guide rail sliding block I3, a gear 4, a line following belt I5, a push rod 6, an unmanned aerial vehicle skid clamping mechanism 7, a servo motor reducer II 71, a rack 72, a guide rail sliding block II 73, a fixed hook 74, a belt pulley 75, a conveyor belt 77, a limiter 78 and a connecting plate 8, can meet the requirements of rapid correction of the posture and the position of the unmanned aerial vehicle after the unmanned aerial vehicle falls under specific environment, is convenient for the effective fixation of a platform or a ground fixing mechanism, meanwhile, the requirements of various types of unmanned aerial vehicles and various sizes of landing areas can be met, and the unmanned aerial vehicles can be automatically and rapidly clamped, fixed and loosened in specific environments, meanwhile, the distance between the fixing hooks 74 and the size of the rack 72 are adjusted, the clamping and fixing requirements of various types of unmanned aerial vehicles are met, and the problem that the unmanned aerial vehicles cannot be clamped and fixed according to specific postures and positions after landing in a specific environment is solved;
the gear 4 is positioned at the top of the rack 2, the inner ring of the connecting plate 8 is in sliding contact with the surface of the guide rail slide block I3, and two sides of the back surface of the rack 2 are fixedly connected with two sides of the front surface of the front guide rail slide block I3;
the bottom of the second servo motor speed reducer 71 is fixedly connected with the rear side of the top surface of the rack 72, and the bottom of the output end of the second servo motor speed reducer 71 is fixedly connected with the belt pulley 75;
the bottom of the front side of the corresponding side of the two frames 72 is transversely and fixedly connected with a connecting bottom plate 76, the bottom of the rear side of the corresponding side of the two frames 72 is transversely provided with a movable plate 710, the top of the movable plate 710 is fixedly connected with a two wire-following belt 79, and the right side of the movable plate 710 penetrates through the right frame 72 and is fixedly connected with a positioning plate 711.
All kinds of parts used in this application file are standard parts, can purchase from the market, and the concrete connected mode of each part all adopts conventional means such as ripe bolt, rivet and welding among the prior art, and machinery, part and electrical equipment all adopt conventional model among the prior art, and circuit connection adopts conventional connected mode among the prior art, and electrical equipment all communicates with external safe power supply, does not make specific statement here again.
In summary, the following steps: the mechanism for correcting the position and the posture of the unmanned aerial vehicle after landing is characterized in that a servo motor speed reducer I1, a rack 2, a guide rail sliding block I3, a gear 4, a line following belt I5, a push rod 6, an unmanned aerial vehicle sliding skid clamping mechanism 7, a servo motor speed reducer II 71, a rack 72, a guide rail sliding block II 73, a fixed hook 74, a belt pulley 75, a conveyor belt 77, a limiter 78 and a connecting plate 8 are arranged for matching use, can meet the requirements of rapid correction of the posture and the position of the unmanned aerial vehicle after the unmanned aerial vehicle falls under specific environment, is convenient for the effective fixation of a platform or a ground fixing mechanism, meanwhile, the requirements of various types of unmanned aerial vehicles and various sizes of landing areas can be met, and the unmanned aerial vehicles can be automatically and rapidly clamped, fixed and loosened in specific environments, the interval and the frame 72 size of adjusting fixed hook 74 simultaneously satisfy polytypic unmanned aerial vehicle's the tight fixed requirement of clamp, have solved under the specific environment unmanned aerial vehicle and can't press from both sides the problem of fixing according to specific gesture and position after descending.
In the description of the present invention, it should be understood that the indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, and is only for convenience of description and simplification of description, and does not indicate or imply that the indicated device or element must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be construed as limiting the present invention.
In the present invention, unless otherwise explicitly specified or limited, for example, it may be fixedly connected, detachably connected, or integrated; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate medium, and may be connected through the inside of two elements or in an interaction relationship between two elements, unless otherwise specifically defined, and the specific meaning of the above terms in the present invention will be understood by those skilled in the art according to specific situations.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (4)
1. The utility model provides an unmanned aerial vehicle descends back position and gesture guiding mechanism, includes rail block one (3) and unmanned aerial vehicle skid clamping mechanism (7), its characterized in that: the two guide rail sliders I (3) are distributed in the front and back direction, connecting plates (8) are sleeved on two sides of each guide rail slider I (3), push rods (6) are fixedly connected to one side of each connecting plate (8) which corresponds to the corresponding connecting plate in the longitudinal direction, a rack (2) is fixedly connected to the front surface of each guide rail slider I (3) at the front side, a servo motor reducer I (1) is fixedly connected to the front surface of each connecting plate (8) at the front side, a gear (4) meshed with the rack (2) is sleeved on the rear side of the output end of the servo motor reducer I (1), and a line following belt I (5) is arranged at the bottom of the servo motor reducer I (1);
the unmanned aerial vehicle skid clamping mechanism (7) is positioned between the two guide rail sliding blocks I (3) and the two push rods (6), the unmanned aerial vehicle skid clamping mechanism (7) comprises two racks (72), the two racks (72) are distributed left and right, two sides of the inner cavity of the racks (72) are longitudinally and fixedly connected with a second guide rail sliding block (73), the front side and the rear side of the inner cavity of the second guide rail sliding block (73) and the front side and the rear side of the inner cavity of the frame (72) are both fixedly connected with belt pulleys (75), a conveying belt (77) is sleeved between the front and rear corresponding sides of the two belt pulleys (75), the front side of the left side surface and the rear side of the right side surface of the conveyor belt (77) are fixedly connected with fixing hooks (74) through bolts, the rear side of the left side of the top surface of the rack (72) is fixedly connected with a limiter (78), and the top of the rear side belt pulley (75) is fixedly connected with a servo motor reducer II (71).
2. The mechanism of claim 1, wherein the mechanism is adapted to correct the position and attitude of the unmanned aerial vehicle after landing, and comprises: the gear (4) is located at the top of the rack (2), the inner ring of the connecting plate (8) is in sliding contact with the surface of the first guide rail sliding block (3), and two sides of the back surface of the rack (2) are fixedly connected with two sides of the front surface of the first front guide rail sliding block (3).
3. The mechanism of claim 1, wherein the mechanism is adapted to correct the position and attitude of the unmanned aerial vehicle after landing, and comprises: the bottom of the second servo motor speed reducer (71) is fixedly connected with the rear side of the top surface of the rack (72), and the bottom of the output end of the second servo motor speed reducer (71) is fixedly connected with the belt pulley (75).
4. The mechanism of claim 1, wherein the mechanism is adapted to correct the position and attitude of the unmanned aerial vehicle after landing, and comprises: the bottom of the front side of one side corresponding to the two racks (72) is transversely and fixedly connected with a connecting bottom plate (76), the bottom of the rear side of one side corresponding to the two racks (72) is transversely provided with a movable plate (710), the top of the movable plate (710) is fixedly connected with a second wire-following belt (79), and the right side of the movable plate (710) penetrates through the right side rack (72) and is fixedly connected with a positioning plate (711).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120099831.4U CN214986135U (en) | 2021-01-14 | 2021-01-14 | Unmanned aerial vehicle descending back position and posture correction mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120099831.4U CN214986135U (en) | 2021-01-14 | 2021-01-14 | Unmanned aerial vehicle descending back position and posture correction mechanism |
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| Publication Number | Publication Date |
|---|---|
| CN214986135U true CN214986135U (en) | 2021-12-03 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120099831.4U Active CN214986135U (en) | 2021-01-14 | 2021-01-14 | Unmanned aerial vehicle descending back position and posture correction mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214986135U (en) |
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2021
- 2021-01-14 CN CN202120099831.4U patent/CN214986135U/en active Active
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