CN118494760A - Unmanned aerial vehicle combined type fast hoisting bearing frame structure - Google Patents
Unmanned aerial vehicle combined type fast hoisting bearing frame structure Download PDFInfo
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- CN118494760A CN118494760A CN202410943463.5A CN202410943463A CN118494760A CN 118494760 A CN118494760 A CN 118494760A CN 202410943463 A CN202410943463 A CN 202410943463A CN 118494760 A CN118494760 A CN 118494760A
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Abstract
The invention discloses an unmanned aerial vehicle combined type rapid hoisting bearing frame structure, in particular to the technical field of unmanned aerial vehicle hoisting, which comprises the following steps: the unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein a connecting frame is fixed at the bottom end of the unmanned aerial vehicle body, two bearing arms are connected to the two ends of the connecting frame in a threaded mode, and bearing frames are connected to one ends of the two bearing arms in a threaded mode; the two groups of locating components are used for stabilizing and conveniently taking out lifting pieces on the bearing frame, each group of locating components comprises a mounting frame arranged at one end of the bearing frame, a locating groove arranged at the top end of the mounting frame and two locating plates symmetrically arranged in the locating groove, and particle cushions are fixed on the two locating plates. According to the invention, through the arrangement of the positioning assembly, the positioning installation between the lifting piece and the bearing frame can be realized, the lifting piece can be quickly assembled and disassembled on the bearing frame, the lifting piece can be prevented from shifting on the bearing frame, and the convenience of the bearing frame is improved.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle hoisting, in particular to a combined type rapid hoisting bearing frame structure of an unmanned aerial vehicle.
Background
Unmanned aerial vehicle is the abbreviation of unmanned aerial vehicle, utilize unmanned aerial vehicle of radio remote control equipment and self-contained program control device manipulation, it can accomplish the flight mission through autonomous control or remote control, unmanned aerial vehicle uses in civil field, it includes inspection and monitoring, agricultural sprays, meteorological detection, exploration survey etc., unmanned aerial vehicle type is various, can select suitable type according to different task demands, install the carriage on the current unmanned aerial vehicle, be used for carrying out hoist and mount transport operation to square hoist and mount, when square hoist and mount, contain carrier arm in the current carriage, crossbeam and bolt, can be with quick combination between it and the unmanned aerial vehicle, be convenient for unmanned aerial vehicle to put into use fast on the scene, as shown in figure 1, when current carriage is in use, firstly alternate more cingulum in proper order in the bottom of carriage, and expose the both ends of cingulum, then square lifting pieces are placed on the bearing frame, at the moment, the two ends of the buckle belt cross the square lifting pieces and are buckled and locked, the buckle belt is tightly abutted against the square lifting pieces, then the rest buckle belts are repeatedly operated in sequence, the square lifting pieces are bound on the bearing frame in a groined shape, the square lifting pieces are prevented from shaking on the bearing frame, when the existing bearing frame is in actual use, when the square lifting pieces are bound by the buckle belt, most of buckle belts are paved on the bottom of the bearing frame, the two ends of the buckle belt are reserved for a proper length, however, the bearing frame cannot position the square lifting pieces, the square lifting pieces are not matched with the reserved length of the buckle belt, so that an operator needs to repeatedly adjust the positions of the square lifting pieces or the buckle belt above the bearing frame, each time of replacement of the lifting pieces is required to be manually adjusted, the operation time is prolonged, the overall operation efficiency is also affected, and the convenience of the bearing frame is reduced.
Disclosure of Invention
The invention aims to provide an unmanned combined type rapid hoisting bearing frame structure so as to solve the defects in the technology.
In order to achieve the above object, the present invention provides the following technical solutions: an unmanned combined type quick hoisting bearing frame structure, comprising:
the unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein a connecting frame is fixed at the bottom end of the unmanned aerial vehicle body, two bearing arms are connected to the two ends of the connecting frame in a threaded mode, and bearing frames are connected to one ends of the two bearing arms in a threaded mode;
The two groups of positioning components are used for stabilizing lifting pieces on the bearing frame and facilitating the taking out, each group of positioning components comprises a mounting frame arranged at one end of the bearing frame, a positioning groove arranged at the top end of the mounting frame and two positioning plates symmetrically arranged in the positioning groove, particle cushions are fixed on the two positioning plates, a moving groove is arranged in the positioning groove, a rotatable threaded column is arranged in the moving groove, moving blocks are fixed at the bottom ends of the two positioning plates, the two moving blocks are positioned in the moving groove and sleeved outside the threaded column, a servo motor is arranged at one end of the mounting frame and used for driving the threaded column to rotate, two groups of displacement components for dismounting the servo motor and the bearing frame are arranged on the mounting frame, and a guide component for protecting the lifting pieces is arranged in the positioning groove; the positioning groove is used for positioning and placing the lifting piece on the bearing frame, so that the situation that the lifting piece is inclined due to gravity center deviation caused by the placement position deviation on the bearing frame can be avoided, and the unmanned aerial vehicle body can be kept balanced; and the granule cushion self is soft material, because of the extrusion between locating plate and the hoist and mount spare, takes place to warp granule cushion self, makes between granule cushion one side and the hoist and mount spare in close contact, reduces the clearance between locating plate and the hoist and mount spare, strengthens the stability of hoist and mount spare in the constant head tank.
Preferably, each group of displacement components comprises a displacement block fixed on one side of the mounting frame and an annular limiting groove arranged outside the bearing frame, one end of the displacement block is fixedly provided with a limiting block, the limiting block is connected with the annular limiting groove in a plugging manner, one sides of the displacement block, the limiting block and the annular limiting groove are provided with first screw holes, movable fixing bolts are screwed into the first screw holes, the displacement block is provided with a bolt component for positioning the displacement block and the bearing frame, one side of the displacement block is provided with an adjusting component, the adjusting component is used for keeping the bearing frame horizontal on the ground, and the annular limiting groove is internally provided with second screw holes for screwing the movable fixing bolts; and the second screw that sets up in the annular spacing inslot and the first screw that sets up in the annular spacing inslot are adjacent symmetry setting, the second screw can change displacement subassembly mounted position moreover, make the position of locating component on bearing the frame adjust, thereby can stabilize fixedly to adapting to not unidimensional hoist and mount, when hoist and mount can't pass the bearing arm inside, thereby change the position of displacement component, make hoist and mount avoid appearing the condition of mutual interference with bearing the arm on bearing the frame, the convenience of the device of increase.
Preferably, the bolt assembly comprises a second bolt block fixed at the top of the displacement block and an L-shaped groove arranged at one side of the bearing frame, a first bolt block is fixed in the L-shaped groove, and the second bolt block is inserted into the L-shaped groove and is spliced with the first bolt block; and the setting of bolt subassembly can be with pegging graft the location in advance between displacement piece and the load-bearing frame, makes stable linking between displacement piece and the load-bearing frame, avoids removing the dead bolt when fixed with the displacement piece, and the displacement piece rotates or the displacement piece appears not hard up condition along with removing the dead bolt in step between displacement piece and the load-bearing frame, provides extra stability between with displacement piece and the load-bearing frame.
Preferably, the adjusting component comprises a supporting block fixed on one side of the displacement block, a thread moving column screwed on the supporting block and a thread moving groove formed at the top end of the supporting block and used for screwing the thread moving column, one end of the thread moving column is provided with a pad seat, and one end of the thread moving column opposite to the pad seat is fixed with a rotating disc; and under the effect of adjusting part, can carry out the free adjustment with four corners of bearing frame, make and bear and keep stabilizing between frame and the ground, avoid bearing frame and the ground after the condition that appears the slope, the hoist and mount piece of being convenient for is on bearing frame stable installation.
Preferably, the guide assembly comprises a guide frame arranged on the bottom wall of the inside of the positioning groove and guide rods fixed at four corners of the bottom end of the guide frame, four guide posts corresponding to the four guide rods are fixed at the bottom of the inside of the positioning groove, sliding grooves for the four guide rods to slide are formed in the four guide posts, sliding rings are fixed in the four sliding grooves by the four guide rods, four springs are jointly arranged between the four sliding rings and the four sliding grooves, and a collision assembly for pushing the guide frame to move is arranged on the positioning plate; can protect square hoist and mount piece when putting and getting to under the effect of spring self elasticity, can absorb impact force to a certain extent, can effectively reduce hoist and mount piece and take place the collision between the frame, help the protection to hoist and mount piece when placing.
Preferably, the abutting component comprises a linking groove formed in the top end of the guide frame, an abutting groove formed in the top end of the positioning plate and an abutting block which is installed in the abutting groove in a pluggable manner, a slidable abutting rod is installed in the linking groove, one end of the abutting rod extends into the abutting groove and is fixed at the bottom end of the abutting block, and a stabilizing component for fixing the abutting block is arranged on one side of the positioning plate; when the both ends of lifting part are just inside locating component to need hold up lifting part both ends, can continue the downwardly push with the leading truck in the constant head tank under the effect of conflict subassembly, make there is the distance between leading truck and the lifting part, and can hold up lifting part's both ends through this distance, promote lifting part and get the convenience of putting on bearing frame.
Preferably, the stabilizing component comprises a first thread groove formed in the top of the positioning plate and a plurality of rotating discs formed on one side of the abutting block, a bolt is screwed on one side of the positioning plate, and the bolt is screwed into one of second thread grooves corresponding to the first thread groove through the first thread groove; through the setting of stabilizing assembly, can keep stable motionless with the distance behind the leading truck condition, avoid appearing the condition of mutual interference with the operator between, hoisting device's flexibility.
Preferably, the guide frame is in a shape of a loop; the guide frame can be prevented from being interfered with the locating plate and the moving block in the locating groove, so that the locating plate, the moving block and the guide frame can stably slide.
In the technical scheme, the invention has the technical effects and advantages that:
Through positioning assembly's setting, not only can realize the hoist and mount and bear the frame between the location installation, can also be with hoist and mount quick assembly disassembly on bearing the frame, can prevent that hoist and mount from appearing the skew on bearing the frame, avoided hoist and mount to change at every turn and all need the condition of manual adjustment, promoted the convenience of bearing the frame.
Through displacement assembly's setting, can realize that locating component changes in the position of bearing the frame, can adapt to not unidimensional hoist and mount and fix a position the installation, can avoid hoist and mount to appear the condition of mutual interference on bearing the frame with bearing between the arm to ensure the correct installation of hoist and mount, further promoted the application scope that bears the frame.
Through the setting of direction subassembly, can protect square hoist and mount when putting to under the elastic effect of spring self, can absorb impact force to a certain extent, can effectively reduce hoist and mount and take place the collision between the frame when placing, help the protection to hoist and mount.
Through adjusting the setting of subassembly, can keep the level between frame and the ground bear, can ensure to bear and keep stable between frame and the ground, avoided bearing the frame and park the circumstances that the unstable emergence of focus was inclined at the ground, help the steady placement of hoist and mount.
Drawings
In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for the embodiments will be briefly described below, and it is apparent that the drawings in the following description are only some embodiments described in the present application, and other drawings may be obtained according to these drawings for a person having ordinary skill in the art.
FIG. 1 is a schematic diagram of the overall structure of a prior art device;
FIG. 2 is a schematic diagram of the overall structure of the present invention;
FIG. 3 is a schematic view of the structure of the mounting frame of the present invention adjusted on one side of the carrying frame;
FIG. 4 is a partial cross-sectional view of the mounting bracket of the present invention;
FIG. 5 is a schematic diagram of a displacement block according to the present invention;
FIG. 6 is a schematic view of an assembly of a first latch block and a second latch block according to the present invention;
FIG. 7 is a schematic view of a second screw hole according to the present invention;
FIG. 8 is a schematic view of the structure of the guide frame of the present invention;
FIG. 9 is a schematic view of the structure of the spring of the present invention;
FIG. 10 is a schematic view of the structure of the interference block of the present invention;
FIG. 11 is an enlarged view of a portion of FIG. 8A in accordance with the present invention;
FIG. 12 is a schematic view of the structure of the cushion of the present invention.
Reference numerals illustrate:
1. an unmanned aerial vehicle body; 11. a connecting frame; 12. a load-bearing arm; 13. a load-bearing frame;
2. A positioning assembly; 21. a mounting frame; 22. a positioning groove; 23. a positioning plate; 24. a granular cushion; 25. a moving block; 26. a moving groove; 27. a threaded column; 28. a servo motor;
3. A displacement assembly; 31. a displacement block; 32. a first latch block; 33. a second latch block; 34. a limiting block; 35. an annular limit groove; 36. moving the fixing bolt; 37. a first screw hole; 38. a second screw hole;
4. A guide assembly; 41. a guide frame; 42. a guide post; 43. a guide rod; 44. a slip ring; 45. a spring;
5. A collision component; 51. a collision block; 52. a touch-up rod; 53. a collision groove; 54. a first thread groove; 55. a bolt; 56. a second thread groove; 57. a connection groove;
6. An adjustment assembly; 61. a thread moving column; 62. a pad seat; 63. a thread moving groove; 64. a support block; 65. and rotating the disc.
Detailed Description
In order to make the technical scheme of the present invention better understood by those skilled in the art, the present invention will be further described in detail with reference to the accompanying drawings.
The invention provides an unmanned combined type rapid hoisting bearing frame structure as shown in fig. 1-7, which comprises the following components: the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, wherein a connecting frame 11 is fixed at the bottom end of the unmanned aerial vehicle body 1, two bearing arms 12 are connected to two ends of the connecting frame 11 in a threaded manner, and one ends of the two bearing arms 12 are connected to a bearing frame 13 in a threaded manner;
The two groups of positioning components 2 are used for stabilizing and conveniently taking out lifting pieces on the bearing frame 13, each group of positioning components 2 comprises a mounting frame 21 arranged at one end of the bearing frame 13, a positioning groove 22 arranged at the top end of the mounting frame 21 and two positioning plates 23 symmetrically arranged in the positioning groove 22, particle cushions 24 are fixed on the two positioning plates 23, a moving groove 26 is arranged in the positioning groove 22, a rotatable threaded column 27 is arranged in the moving groove 26, moving blocks 25 are fixed at the bottom ends of the two positioning plates 23, the two moving blocks 25 are positioned in the moving groove 26 and sleeved outside the threaded column 27, a servo motor 28 is arranged at one end of the mounting frame 21 and used for driving the threaded column 27 to rotate, two groups of displacement components 3 for dismounting the mounting frame 21 and the bearing frame 13 are arranged on the mounting frame 21, and a guide component 4 for protecting the lifting pieces is arranged in the positioning groove 22; and the external screw thread of the screw thread post 27 is positive and negative, and the internal screw thread has been seted up to two movable blocks 25 in addition to the internal screw thread that sets up in two movable blocks 25 closes the cooperation with the external screw thread of screw thread post 27 soon.
Before square lifting pieces are lifted, firstly, stable connection is kept between the bearing arms 12 and the connecting frame 11 under the connection of bolts, namely, the bearing frame 13 and the unmanned aerial vehicle body 1 are quickly combined, the bearing frame 13 and the unmanned aerial vehicle body 1 are conveniently put into use on site, square lifting pieces are placed and supported through the bearing frame 13, then the square lifting pieces penetrate through the inside of the two groups of the bearing arms 12 on the bearing frame 13, at the moment, two ends of the square lifting pieces are respectively inside the two positioning grooves 22, the square lifting pieces are positioned on the bearing frame 13 in advance, a servo motor 28 drives and drives one of the threaded columns 27 to rotate in the moving groove 26, in addition, the outside of the threaded column 27 is in screwing transmission with the two moving blocks 25, the two moving blocks 25 are relatively or relatively moved in the moving groove 26, so that the two positioning plates 23 and the two particle cushions 24 are relatively moved in the positioning groove 22, then the square lifting pieces in the positioning groove 22 are relatively clamped and fixed, the square lifting pieces are accurately positioned and stably fixed on the bearing frame 13, and the lifting pieces are stably lifted on the bearing frame 13.
Referring to fig. 1-7, each group of displacement assemblies 3 includes a displacement block 31 fixed on one side of the mounting frame 21 and an annular limiting groove 35 arranged outside the bearing frame 13, one end of the displacement block 31 is fixed with a limiting block 34, the limiting block 34 is connected with the annular limiting groove 35 in a plugging manner, one sides of the displacement block 31, the limiting block 34 and the annular limiting groove 35 are provided with first screw holes 37, a movable fixing bolt 36 is screwed in the first screw holes 37, a bolt assembly for positioning the displacement block 31 and the bearing frame 13 is arranged on the displacement block 31, one side of the displacement block 31 is provided with an adjusting assembly 6, the adjusting assembly 6 is used for keeping the bearing frame 13 horizontal on the ground, and a second screw hole 38 for screwing the movable fixing bolt 36 is arranged in the annular limiting groove 35; the bolt assembly comprises a second bolt block 33 fixed at the top of the displacement block 31 and an L-shaped groove formed on one side of the bearing frame 13, a first bolt block 32 is fixed in the L-shaped groove, and the second bolt block 33 is inserted into the L-shaped groove and is spliced with the first bolt block 32.
Through the technical scheme:
when the square lifting member collides with the bearing arm 12, the movable fixing bolt 36 is rotated to rotate and take out the square lifting member along the first screw hole 37, the movable fixing bolt 31 is prevented from being limited by the first screw hole 37, the movable fixing bolt 31 is conveniently taken out from one side of the bearing frame 13, the movable fixing bolt 31 is reinserted into the other side of the bearing frame 13, and when the movable fixing bolt 31 is inserted into the other side of the bearing frame 13, the movable fixing bolt 31 is attached to one side of the bearing frame 13, the second bolt 33 is inserted into the L-shaped groove, the first bolt 32 in the second bolt 33 and the L-shaped groove is pre-inserted and limited, the movable fixing bolt 31 is pre-positioned and installed on one side of the bearing frame 13, the movable fixing bolt 31 is ensured to be stable on one side of the bearing frame 13, however, the limiting block 34 installed on one side of the movable fixing bolt 31 is inserted into the annular limiting groove 35, the first screw hole 37 is kept coincident with the second screw hole 38 formed in the annular limiting groove 35 along with the insertion of the limiting block 34, the movable fixing bolt 36 is rotationally combined with the first screw hole 37 on one side of the first screw hole 37, the movable fixing bolt 36 is sufficiently rotatably connected with the first screw hole 37 on one side of the first screw hole 37, and then the movable fixing bolt 36 is positioned and screwed and fixed between the first bolt 31 and the bearing frame 13, and the square lifting member is positioned and the first fixing bolt is positioned between the two side of the square lifting member and the square lifting member is positioned and the first fixing bolt 13, and the first fixing bolt is positioned between the fixed bolt and the position and the first fixing bolt 31 and the position is positioned and the fixed between the frame 13 and the fixed frame 13, and the fixed bolt 2.
Referring to fig. 2,5, 8, 9, 10 and 11, the guide assembly 4 includes a guide frame 41 mounted on the bottom wall of the inside of the positioning slot 22 and guide rods 43 fixed at four corners of the bottom end of the guide frame 41, four guide posts 42 corresponding to the four guide rods 43 are fixed at the bottom of the inside of the positioning slot 22, sliding grooves for sliding the four guide rods 43 are formed in the four guide posts 42, sliding rings 44 are fixed in the four sliding grooves of the four guide rods 43, four springs 45 are mounted between the four sliding rings 44 and the four sliding grooves, and a collision assembly 5 for pushing the guide frame 41 to move is arranged on the positioning plate 23; the guide frame 41 has a loop-shaped structure.
The abutting component 5 comprises a linking groove 57 formed at the top end of the guide frame 41, an abutting groove 53 formed at the top end of the positioning plate 23 and an abutting block 51 which is installed in the abutting groove 53 in a pluggable manner, a slidable abutting rod 52 is installed in the linking groove 57, one end of the abutting rod 52 extends into the abutting groove 53 and is fixed at the bottom end of the abutting block 51, and a stabilizing component for fixing the abutting block 51 is arranged on one side of the positioning plate 23; the stabilizing assembly comprises a first thread groove 54 formed at the top of the locating plate 23 and a plurality of rotating discs 65 formed at one side of the abutting block 51, a bolt 55 is screwed at one side of the locating plate 23, and the bolt 55 is screwed into one of the second thread grooves 56 corresponding to the first thread groove 54 through the first thread groove 54.
Through the technical scheme:
When the square hoisting member is placed in the positioning groove 22, firstly, the guide frame 41 is used for contacting the square hoisting member in the positioning groove 22 in advance, then the guide frame 41 supports the square hoisting member, heavy pressure is formed at the top end of the guide frame 41, at this time, the guide frame 41 moves downwards along the positioning groove 22, the guide frame 41 moves downwards to push the guide rod 43 to slide downwards along the sliding groove, the guide rod 43 moves to push the sliding ring 44 to synchronously move in the sliding groove, the spring 45 is extruded between the sliding ring 44 and the sliding groove, so that the guide frame 41 slides downwards in the positioning groove 22, the top of the guide frame 41 and the top of the bearing frame 13 are kept horizontal, the square hoisting member is stably placed on the bearing frame 13, however, the guide frame 41 moves downwards to drive the engagement groove 57 formed at the top end of the square hoisting member to synchronously slide downwards, the engagement groove 57 moves downwards to pull the abutment rod 52 downwards along the positioning plate 23 and the abutment groove 53, the abutment rod 52 moves to drive the abutment block 51 to slide downwards along the abutment groove 53, and then one of the second thread grooves 56 and the first thread grooves 54 keep coincident with each other, so that the first thread grooves 55 and the first thread grooves 54 are screwed into the first thread grooves 54 and the second thread grooves 53, and one of the second thread grooves 54 are well stable.
Referring to fig. 2,3, 5 and 12, the adjusting unit 6 includes a support block 64 fixed to one side of the displacement block 31, a screw moving column 61 screw-mounted on the support block 64, and a screw moving groove 63 provided at the top end of the support block 64 for screwing the screw moving column 61, a pad 62 is mounted at one end of the screw moving column 61, and a rotating disk 65 is fixed to one end of the screw moving column 61 opposite to the pad 62.
Through the technical scheme:
When the bearing frame 13 is placed on the ground, the rotating disc 65 drives the screw moving column 61 to rotate, then the screw moving column 61 and the screw moving groove 63 rotate and move the screw moving column 61 downwards in the screw moving groove 63, at the moment, the screw moving column 61 moves to push the cushion seat 62 to slide downwards, the bottom of the cushion seat 62 contacts the ground, and the rotating disc 65 stops rotating the screw moving column 61, so that the cushion seat 62 supports the bearing frame 13 and the ground, the bearing frame 13 and the ground can be kept horizontal, and stability between the bearing frame 13 and the ground can be ensured.
While certain exemplary embodiments of the present invention have been described above by way of illustration only, it will be apparent to those of ordinary skill in the art that modifications may be made to the described embodiments in various different ways without departing from the spirit and scope of the invention. Accordingly, the drawings and description are to be regarded as illustrative in nature and not as restrictive of the scope of the invention, which is defined by the appended claims.
Claims (8)
1. An unmanned aerial vehicle combined type fast hoisting bearing frame structure, which is characterized by comprising:
The unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), a connecting frame (11) is fixed at the bottom end of the unmanned aerial vehicle body (1), two bearing arms (12) are connected to the two ends of the connecting frame (11) in a threaded mode, and a bearing frame (13) is connected to one end of each of the two bearing arms (12) in a threaded mode;
Two sets of locating component (2) for with bear on frame (13) hoist and mount piece stable and be convenient for take out, every group locating component (2) all including install at mounting bracket (21) of bearing frame (13) one end, set up two locating plates (23) on mounting bracket (21) top and symmetry install in locating slot (22), and all be fixed with granule cushion (24) on two locating plates (23), set up movable groove (26) in locating slot (22), install rotatable screw thread post (27) in movable groove (26), the bottom of two locating plates (23) all is fixed with movable block (25), and two movable blocks (25) are located movable groove (26) and the cover is established in the outside of screw thread post (27), servo motor (28) are installed to one end of mounting bracket (21), and servo motor (28) are used for driving screw thread post (27) rotation, be equipped with on mounting bracket (21) with two sets of displacement components (3) of its and bearing frame (13) dismouting, the bottom of two locating plates (23) all are equipped with movable block (25) and are equipped with in movable block (22) with the guide piece (4).
2. An unmanned combined quick hoist and mount carrier structure according to claim 1, wherein: every group displacement subassembly (3) all include fixed displacement piece (31) in mounting bracket (21) one side and set up annular spacing groove (35) outside frame (13) bear, the one end of displacement piece (31) is fixed with stopper (34), and plug connection between stopper (34) and annular spacing groove (35), first screw (37) have all been seted up to one side of displacement piece (31), stopper (34) and annular spacing groove (35), and the spiro union has movable dead bolt (36) in first screw (37), be equipped with on displacement piece (31) with its bolt subassembly that fixes a position with frame (13), one side of displacement piece (31) is equipped with adjusting component (6), and adjusting component (6) are used for keeping frame (13) bear subaerial level, second screw (38) that movable dead bolt (36) were screwed have been seted up in annular spacing groove (35).
3. An unmanned combined quick hoist and mount carrier structure according to claim 2, wherein: the bolt assembly comprises a second bolt block (33) fixed at the top of the displacement block (31) and an L-shaped groove formed in one side of the bearing frame (13), a first bolt block (32) is fixed in the L-shaped groove, and the second bolt block (33) is inserted into the L-shaped groove and is spliced with the first bolt block (32).
4. An unmanned combined quick hoist and mount carrier structure according to claim 2, wherein: the adjusting component (6) comprises a supporting block (64) fixed on one side of the displacement block (31), a thread moving column (61) screwed on the supporting block (64) and a thread moving groove (63) formed in the top end of the supporting block (64) and used for screwing the thread moving column (61), a pad seat (62) is mounted at one end of the thread moving column (61), and a rotating disc (65) is fixed at one end of the thread moving column (61) opposite to the pad seat (62).
5. An unmanned combined quick hoist and mount carrier structure according to claim 1, wherein: the guide assembly (4) comprises a guide frame (41) arranged on the bottom wall inside a positioning groove (22) and guide rods (43) fixed at four corners at the bottom end of the guide frame (41), four guide posts (42) corresponding to the guide rods (43) are fixed at the bottom inside the positioning groove (22), sliding grooves for the four guide rods (43) to slide are formed in the guide posts (42), sliding rings (44) are fixed in the four sliding grooves, four springs (45) are jointly arranged between the sliding rings (44) and the sliding grooves, and a pushing assembly (5) for pushing the guide frame (41) to move is arranged on the positioning plate (23).
6. The unmanned combined type rapid hoisting carrier structure as claimed in claim 5, wherein: the utility model discloses a guide frame, including the linking groove (57) of setting up on guide frame (41) top, set up conflict groove (53) and pluggable in conflict groove (53) of setting up on locating plate (23) top conflict piece (51), install slidable conflict pole (52) in linking groove (57), and the one end of conflict pole (52) extends to in conflict groove (53) and fix in conflict piece (51) bottom, one side of locating plate (23) is equipped with the stable subassembly fixed with conflict piece (51).
7. The unmanned combined type rapid hoisting carrier structure as claimed in claim 6, wherein: the stabilizing assembly comprises a first thread groove (54) formed in the top of the positioning plate (23) and a plurality of rotating discs (65) formed in one side of the abutting block (51), a bolt (55) is arranged on one side of the positioning plate (23) in a threaded mode, and the bolt (55) is screwed into one of second thread grooves (56) corresponding to the first thread groove (54) through the first thread groove (54).
8. The unmanned combined type rapid hoisting carrier structure as claimed in claim 5, wherein: the guide frame (41) is of a return structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202410943463.5A CN118494760B (en) | 2024-07-15 | 2024-07-15 | Unmanned aerial vehicle combined type fast hoisting bearing frame structure |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202410943463.5A CN118494760B (en) | 2024-07-15 | 2024-07-15 | Unmanned aerial vehicle combined type fast hoisting bearing frame structure |
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| CN118494760A true CN118494760A (en) | 2024-08-16 |
| CN118494760B CN118494760B (en) | 2024-09-27 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
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| CN118494760B (en) | 2024-09-27 |
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