CN216834246U - Multifunctional agricultural automatic pilot - Google Patents

Multifunctional agricultural automatic pilot Download PDF

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Publication number
CN216834246U
CN216834246U CN202122906089.6U CN202122906089U CN216834246U CN 216834246 U CN216834246 U CN 216834246U CN 202122906089 U CN202122906089 U CN 202122906089U CN 216834246 U CN216834246 U CN 216834246U
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rod
groove
wall
abutting
slot
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邸冰
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Pinghu Qianruixiang Agricultural Technology Co ltd
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Pinghu Qianruixiang Agricultural Technology Co ltd
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Abstract

The utility model provides a multifunctional agricultural autopilot, which belongs to the technical field of agricultural equipment and comprises an unmanned aerial vehicle body, wherein the unmanned aerial vehicle body comprises a machine body, wings are arranged on the side walls of two sides of the machine body, and the wings are detachably connected to the machine body.

Description

Multifunctional agricultural automatic pilot
Technical Field
The utility model belongs to the technical field of agricultural equipment, and particularly relates to a multifunctional agricultural automatic pilot.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like.
Agricultural unmanned aerial vehicle is generally undertaken to the seeding of crops, is fertilizeed, is spouted the effect of medicine, and current agricultural unmanned aerial vehicle includes fuselage and wing two parts usually, and the wing is died on the fuselage through the bolt lock usually, and to this kind of unmanned aerial vehicle, the operator carries the bigger space of needs, is unfavorable for unmanned aerial vehicle's transportation.
Disclosure of Invention
The utility model aims to solve the problems in the prior art, provides the multifunctional agricultural automatic pilot, and has the characteristics of reducing the storage space of the unmanned aerial vehicle and facilitating the transportation of a packing box of the unmanned aerial vehicle.
The purpose of the utility model can be realized by the following technical scheme:
the utility model provides a multi-functional agricultural autopilot, includes the unmanned aerial vehicle body, the unmanned aerial vehicle body includes the organism, installs a wing at organism both sides lateral wall, the connection can be dismantled on the organism to the wing.
Further, be equipped with a coupling mechanism between wing and the organism, coupling mechanism includes fixed connection first pole on the organism outer wall, fixed connection second pole on first pole outer wall, set up at the first groove of wing one end, set up the second groove on first groove one end lateral wall and set up the stop gear who is used for spacing wing angle between wing one end terminal surface and organism outer wall, second pole one end sliding connection is in the second groove, first pole sliding connection is in the first groove, be perpendicular setting between first pole and the second pole, be perpendicular setting between first groove and the second groove.
Furthermore, the limiting mechanism comprises a third groove formed in the end face of one end of the wing, a fourth groove formed in the side wall of one end of the third groove, a sliding groove formed in the outer wall of the body, a third rod connected in the sliding groove in a sliding manner, a fourth rod fixedly connected to the outer wall of one end of the third rod, and a clamping member arranged in the sliding groove and used for clamping the fourth rod in the fourth groove, the third rod and the fourth rod are arranged vertically, the third groove and the fourth groove are arranged vertically, the width of the third groove is larger than the sum of the length of the fourth rod and the width of the third rod, the third rod is connected in the third groove in a sliding manner, and the fourth rod is connected in the fourth groove in a sliding manner.
Furthermore, the abutting part comprises an abutting groove formed in the outer wall of the machine body, an abutting rod fixedly connected to the outer wall of the third rod, an abutting spring sleeved on the outer wall of the abutting rod, an abutting hole formed in one end face of the sliding groove and a driving rod fixedly connected to the outer wall of the third rod, the abutting rod is connected to the abutting hole in a sliding mode, the driving rod is connected to the abutting groove in a sliding mode, and the two ends of the abutting spring are fixedly connected to the outer wall of the third rod and the inner wall of one end of the sliding groove respectively.
Furthermore, a locking bolt is connected to the outer wall of the machine body in a threaded manner, and one end of the locking bolt abuts against the outer wall of the driving rod.
Furthermore, a top rod is fixedly connected to the outer wall of the machine body, a top hole is formed in the end face of one end of the wing, a butting spring is installed in the top hole, one end of the butting spring is fixedly connected to the hole bottom of the top hole, and one end of the top rod is abutted against one end of the butting spring.
Furthermore, a butting plate is connected in the top hole in a sliding mode, the butting plate is fixedly connected with one end of the butting spring, and one end of the ejector rod is butted on the butting plate.
Furthermore, the cross sections of the first rod, the second rod, the third rod and the fourth rod are all arranged in a rectangular shape.
Compared with the prior art, the utility model has the following advantages:
1. according to the utility model, the wings and the machine body are detachably connected, so that the storage space of the unmanned aerial vehicle is reduced, and the transportation of a packing box of the unmanned aerial vehicle is facilitated.
2. According to the utility model, the second rod slides into the second groove, the third rod slides, the fourth rod slides into the fourth groove, and the fourth rod is always positioned in the fourth groove under the action of the abutting spring.
Drawings
FIG. 1 is a schematic diagram of the present invention.
Fig. 2 is a schematic view of the structure of the connection mechanism of the present invention.
In the figure, 1, an unmanned aerial vehicle body; 2. a body; 3. an airfoil; 4. a connecting mechanism; 5. a first lever; 6. a second lever; 7. a first groove; 8. a second groove; 9. a limiting mechanism; 10. a third groove; 11. a fourth groove; 12. a sliding groove; 13. a third lever; 14. a fourth bar; 15. an abutting piece; 16. abutting against the groove; 17. a tightening rod; 18. the spring is tightly propped; 19. abutting the hole; 20. a drive rod; 21. locking the bolt; 22. a top rod; 23. a top hole; 24. an abutment spring; 25. abutting against the board.
Detailed Description
The following are specific embodiments of the present invention and are further described with reference to the drawings, but the present invention is not limited to these embodiments.
As shown in fig. 1 and 2, the multifunctional agricultural automatic pilot comprises an unmanned aerial vehicle body 1, wherein the unmanned aerial vehicle body 1 comprises an engine body 2, and wings 3 are detached and connected from side walls on two sides of the engine body 2.
As shown in fig. 1 and 2, a connecting mechanism 4 is arranged between the wing 3 and the body 2, the connecting mechanism 4 includes a first rod 5, a second rod 6, a first groove 7, a second groove 8 and a limiting mechanism 9, the first rod 5 is fixedly connected to the outer wall of the body 2, the second rod 6 is fixedly connected to the outer wall of one end of the first rod 5, the first rod 5 and the second rod 6 are vertically arranged, the cross sections of the first rod 5 and the second rod 6 are both rectangular, the first groove 7 is arranged on the end surface of one end of the wing 3, the second groove 8 is arranged on the side wall of one end of the first groove 7, the first groove 7 and the second groove 8 are vertically arranged, the width of the first groove 7 is greater than the sum of the width of the first rod 5 and the length of the second rod 6, the second rod 6 is connected in the second groove 8 in a sliding mode, the first rod 5 is connected in the first groove 7 in a sliding mode, the limiting mechanism 9 is arranged between the wing 3 and the outer wall of the machine body 2, and the limiting mechanism 9 is used for limiting the angle of the wing 3.
As shown in fig. 1 and fig. 2, the limiting mechanism 9 includes a third rod 13, a fourth rod 14, a sliding groove 12, a third groove 10, a fourth groove 11 and a fastening member 15, the third groove 10 is disposed on an end surface of one end of the wing 3, the fourth groove 11 is disposed on an inner wall of one end of the third groove 10, the third groove 10 and the fourth groove 11 are vertically disposed, the extending directions of the fourth groove 11 and the second groove 8 are opposite, one end of the third rod 13 is slidably connected to an outer wall of the body 2, the sliding groove 12 is disposed on an outer wall of the body 2, one end of the third rod 13 is slidably connected to the sliding groove 12, one end of the fourth rod 14 is fixedly connected to an outer wall of one end of the third rod 13, the third rod 13 and the fourth rod 14 are vertically disposed and have rectangular cross sections, the width of the third groove 10 is greater than the sum of the width of the third rod 13 and the length of the fourth rod 14, the fourth rod 14 is slidably connected to the fourth groove 11, the third rod 13 is slidably connected to the third groove 10, the abutting piece 15 is arranged on the machine body 2, and the abutting piece 15 is used for limiting the fourth rod 14 to always abut against the fourth groove 11.
As shown in fig. 1 and 2, the fastening member 15 includes a fastening groove 16, a fastening rod 17, a fastening spring 18, a fastening hole 19 and a driving rod 20, the fastening groove 16 is disposed on the outer wall of the body 2, one end of the fastening rod 17 is fixedly connected to one end of the third rod 13, the fastening spring 18 is sleeved on the outer wall of the fastening rod 17, the fastening hole 19 is disposed on one end face of the sliding groove 12, one end of the fastening rod 17 is slidably connected to the fastening hole 19, two ends of the fastening spring 18 are respectively fixedly connected to the outer wall of the third rod 13 and the inner wall of one end of the sliding groove 12, the driving rod 20 is fixedly connected to the outer wall of the third rod 13, and the driving rod 20 is slidably connected to the fastening groove 16.
As shown in fig. 1 and fig. 2, in order to improve the positioning stability of the driving rod 20 in the abutting groove 16, a locking bolt 21 is screwed on the outer wall of the body 2, and one end of the locking bolt 21 abuts against the outer wall of the driving rod 20.
As shown in fig. 1 and 2, in order to improve the stability of the second rod 6 in the second slot 8 and the fourth rod 14 in the fourth slot 11, a top rod 22 is fixedly connected to the outer wall of the body 2, a top hole 23 is formed in an end face of the wing 3, an abutment spring 24 is installed in the top hole 23, one end of the abutment spring 24 is fixedly connected to the bottom of the hole of the top hole 23, an abutment plate 25 is slidably connected to the top hole 23, the abutment plate 25 is fixedly connected to one end of the abutment spring 24, and one end of the top rod 22 is slidably connected to the top hole 23 and abuts against the abutment plate 25.
The working principle of the embodiment of the utility model is as follows: the driving rod 20 drives the third rod 13 to slide, so that the fourth rod 14 is aligned with the third groove 10, the second rod 6 is aligned with the first groove 7, the fourth rod 14 is slid into the third groove 10, the second rod 6 is slid into the first groove 7, under the action of the abutting spring 18, the second rod 6 is slid into the second groove 8, the fourth rod 14 is slid into the fourth groove 11, the locking bolt 21 is tightened, and one end of the locking bolt 21 abuts against the outer wall of the driving rod 20;
The top rod 22 slides into the top hole 23, one end of the top rod 22 abuts against the abutting plate 25, the abutting plate 25 compresses the abutting spring 24, the fourth rod 14 abuts against the inner wall of the fourth groove 11 under the action of the abutting spring 24, and the second rod 6 abuts against the inner wall of the second groove 8.
The specific embodiments described herein are merely illustrative of the spirit of the utility model. Various modifications or additions may be made to the described embodiments or alternatives may be employed by those skilled in the art without departing from the spirit or ambit of the utility model as defined in the appended claims.
Although 1, the drone body is used more herein; 2. a body; 3. an airfoil; 4. a connecting mechanism; 5. a first lever; 6. a second lever; 7. a first groove; 8. a second groove; 9. a limiting mechanism; 10. a third groove; 11. a fourth groove; 12. a sliding groove; 13. a third lever; 14. a fourth bar; 15. an abutting piece; 16. abutting against the groove; 17. a tightening rod; 18. the spring is tightly propped; 19. abutting the hole; 20. a drive rod; 21. locking the bolt; 22. a top rod; 23. a top hole; 24. an abutment spring; 25. abutting plates, etc., but does not exclude the possibility of using other terms. These terms are used merely to more conveniently describe and explain the nature of the present invention; they are to be construed as being without limitation to any additional limitations that may be imposed by the spirit of the present invention.

Claims (7)

1. The multifunctional agricultural autopilot is characterized by comprising an unmanned aerial vehicle body (1), wherein the unmanned aerial vehicle body (1) comprises a vehicle body (2), wings (3) are mounted on the side walls of two sides of the vehicle body (2), and the wings (3) are detachably connected to the vehicle body (2); be equipped with a coupling mechanism (4) between wing (3) and organism (2), coupling mechanism (4) include first pole (5) of fixed connection on organism (2) outer wall, second pole (6) of fixed connection on first pole (5) outer wall, set up in first groove (7) that wing (3) one was served, set up second groove (8) on first groove (7) one end lateral wall and set up stop gear (9) that are used for spacing wing (3) angle between wing (3) one end terminal surface and organism (2) outer wall, second pole (6) one end sliding connection is in second groove (8), first pole (5) sliding connection is in first groove (7), be perpendicular setting between first pole (5) and second pole (6), be perpendicular setting between first groove (7) and second groove (8).
2. The multifunctional agricultural autopilot according to claim 1, wherein the limiting mechanism (9) comprises a third slot (10) provided on an end face of one end of the wing (3), a fourth slot (11) provided on a side wall of one end of the third slot (10), a sliding slot (12) provided on an outer wall of the body (2), a third rod (13) slidably connected in the sliding slot (12), a fourth rod (14) fixedly connected to an outer wall of one end of the third rod (13), and a retaining member (15) provided in the sliding slot (12) for retaining the fourth rod (14) in the fourth slot (11), wherein the third rod (13) and the fourth rod (14) are vertically arranged, the third slot (10) and the fourth slot (11) are vertically arranged, and the width of the third slot (10) is greater than the sum of the length of the fourth rod (14) and the width of the third rod (13), the third rod (13) is slidably connected in a third slot (10), and the fourth rod (14) is slidably connected in a fourth slot (11).
3. The multifunctional agricultural autopilot according to claim 2, characterized in that the abutting member (15) comprises an abutting groove (16) formed in the outer wall of the machine body (2), an abutting rod (17) fixedly connected to the outer wall of the third rod (13), an abutting spring (18) sleeved on the outer wall of the abutting rod (17), an abutting hole (19) formed in one end face of the sliding groove (12) and a driving rod (20) fixedly connected to the outer wall of the third rod (13), the abutting rod (17) is slidably connected in the abutting hole (19), the driving rod (20) is slidably connected in the abutting groove (16), and two ends of the abutting spring (18) are fixedly connected to the outer wall of the third rod (13) and the inner wall of one end of the sliding groove (12) respectively.
4. The multifunctional agricultural autopilot according to claim 3, characterized in that a locking bolt (21) is screwed to the outer wall of the machine body (2), and one end of the locking bolt (21) abuts against the outer wall of the driving rod (20).
5. The multifunctional agricultural autopilot according to claim 4, characterized in that a top rod (22) is fixedly connected to the outer wall of the body (2), a top hole (23) is formed in an end face of one end of the wing (3), an abutting spring (24) is installed in the top hole (23), one end of the abutting spring (24) is fixedly connected to the bottom of the top hole (23), and one end of the top rod (22) abuts against one end of the abutting spring (24).
6. The multi-functional agricultural autopilot according to claim 5, characterized in that an abutment plate (25) is slidably connected in the top opening (23), the abutment plate (25) being fixedly connected to one end of an abutment spring (24), the ram (22) abutting against the abutment plate (25) at one end.
7. The multi-functional agricultural autopilot according to claim 6, characterized in that the first (5), second (6), third (13) and fourth (14) bars are each rectangularly arranged in cross-section.
CN202122906089.6U 2021-11-24 2021-11-24 Multifunctional agricultural automatic pilot Active CN216834246U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202122906089.6U CN216834246U (en) 2021-11-24 2021-11-24 Multifunctional agricultural automatic pilot

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202122906089.6U CN216834246U (en) 2021-11-24 2021-11-24 Multifunctional agricultural automatic pilot

Publications (1)

Publication Number Publication Date
CN216834246U true CN216834246U (en) 2022-06-28

Family

ID=82103656

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202122906089.6U Active CN216834246U (en) 2021-11-24 2021-11-24 Multifunctional agricultural automatic pilot

Country Status (1)

Country Link
CN (1) CN216834246U (en)

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