Unmanned aerial vehicle remote sensing is with infrared scanning device of equipment of being convenient for
Technical Field
The utility model relates to an information technology device technical field specifically is an unmanned aerial vehicle remote sensing is with infrared scanning device of being convenient for equipment.
Background
The infrared scanner is mainly composed of 4 parts of optical system, detector, signal processing, recorder or display, etc. the scanning mode is divided into mechanical and optical modes, and the target is searched by scanning a large search visual field.
At present can use various different infrared scanning device when carrying out infrared scanning, but these infrared scanning device exist with unmanned aerial vehicle equipment more loaded down with trivial details problem, this can bring certain inconvenience for infrared scanning device's user, consequently improves current infrared scanning device according to infrared scanning device's in-service use condition.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle remote sensing is with infrared scanning device of being convenient for equipment to solve the present infrared scanning device that can use various differences that the above-mentioned background art provided, but these infrared scanning device exist and assemble more loaded down with trivial details problem with unmanned aerial vehicle, and this can bring certain inconvenience for infrared scanning device's user, consequently carries out the problem of improving to current infrared scanning device according to infrared scanning device's in-service use condition.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle remote sensing is with infrared scanning device of equipment of being convenient for, includes unmanned aerial vehicle organism, first cross axle and second cross axle, its characterized in that: one side of the unmanned aerial vehicle body is connected with a connecting block, one side of the connecting block is provided with a clamping groove, one side of the connecting block, which is far away from the unmanned aerial vehicle body, is provided with a butt box, a first spring strip is connected inside the butt box, one end of the first spring strip is connected with a first clamping hook, a first transverse shaft penetrates between the first clamping hook and the butt box, one side of the butt box is provided with a threaded hole, a threaded rod penetrates through the threaded hole, one end of the threaded rod, which is far away from the first clamping hook, is connected with a knob, and one end of the butt box, which is far away from the connecting block, is connected with an infrared scanner;
one side, close to the connecting block, of the unmanned aerial vehicle body is connected with supporting rods, a connecting sheet is connected between the supporting rods, a sliding groove is formed in the surface of the connecting sheet, a sliding block penetrates through the sliding groove, one end of the sliding block is connected with a connecting rod, a second spring strip is connected between the connecting rods, a second transverse shaft penetrates through the connecting rods, one end of the second transverse shaft is connected with a transverse rod, and one side, far away from the supporting rods, of the transverse rod is connected with a supporting frame;
unmanned aerial vehicle organism one side is connected with the blade base, the spring groove has been seted up on blade base surface, spring groove surface is connected with the third spring strip, third spring strip one end is connected with the stopper, keeps away from the third spring strip stopper one side is connected with first fixture block, blade base surface is connected with the second trip, blade base surface has cup jointed the second fixture block, second fixture block one side is connected with the protection casing, is close to first fixture block the circular slot has been seted up on the protection casing surface.
Preferably, the first hook and the first cross shaft are provided with two groups, and a rotating structure is formed between the first hook and the first cross shaft.
Preferably, the threaded holes and the threaded rods are two groups, and the threaded holes are in threaded connection with the threaded rods.
Preferably, the sliding grooves and the sliding blocks are arranged in two groups, and the sliding grooves are in sliding connection with the sliding blocks.
Preferably, the connecting rods and the second transverse shaft are provided with two groups, a rotating structure is formed between the connecting rods and the transverse rod through the second transverse shaft, and a telescopic structure is formed between the connecting rods through the second spring strips.
Preferably, the spring grooves, the third spring strips and the limiting blocks are provided with four groups, and a telescopic structure is formed between the spring grooves and the limiting blocks through the third spring strips.
Compared with the prior art, the beneficial effects of the utility model are that: this unmanned aerial vehicle remote sensing is with infrared scanning device of equipment of being convenient for:
1. rotate the knob during equipment infrared scanner, rotate the knob and can drive the threaded rod and rotate, the threaded rod can make threaded rod lateral motion when screw hole inside rotates, threaded rod lateral motion can extrude first trip, and first trip receives the extrusion can rotate along first cross axle surface, can carry out the centre gripping to the connecting block when first trip one end rotates inside the draw-in groove two first trips, conveniently installs infrared scanner.
2. Unmanned aerial vehicle organism continues downstream according to inertia when falling to the ground, unmanned aerial vehicle organism downstream can drive connection piece downstream through branch, connection piece downstream can drive the connecting rod through the slider and rotate along second cross axle surface, the slider can slide in the spout is inside, because be connected with the second spring strip between the connecting rod, the second spring strip can produce the pulling force to the slider through self elasticity, reduce the rotation angle of connecting rod, reduce the inertial displacement of unmanned aerial vehicle organism, conveniently increase unmanned aerial vehicle's cushioning effect.
3. When the protective cover moves to one end of the blade base, the first clamping block can be extruded when the protective cover moves to one end of the blade base, the protective cover continues to move upwards to drive the second clamping block to slide in the second clamping hook, when the circular groove moves to one side of the first clamping block, the first clamping block can reset through the elastic force of the third spring strip, the first clamping block is connected with the circular groove in a clamping mode, and the protective cover is conveniently fixed on the surface of the blade base.
Drawings
FIG. 1 is a schematic front view of the present invention;
FIG. 2 is a schematic side view of the present invention;
FIG. 3 is a partial schematic view of the blade of the present invention;
FIG. 4 is a schematic view of the structure at the position A of the present invention;
FIG. 5 is a schematic view of the structure at the position B of the present invention;
fig. 6 is a schematic view of the structure at position C of the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. connecting blocks; 3. a card slot; 4. a butt-joint box; 5. a first spring bar; 6. a first hook; 7. a first lateral axis; 8. a threaded hole; 9. a threaded rod; 10. a knob; 11. an infrared scanner; 12. a strut; 13. connecting sheets; 14. a chute; 15. a slider; 16. a connecting rod; 17. a second spring bar; 18. a second lateral axis; 19. a cross bar; 20. a support frame; 21. a blade base; 22. a spring slot; 23. a third spring bar; 24. a limiting block; 25. a first clamping block; 26. a second hook; 27. a protective cover; 28. a second fixture block; 29. a circular groove.
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. 1-6, the present invention provides a technical solution: an infrared scanning device convenient to assemble for remote sensing of an unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a connecting block 2, a clamping groove 3, a butt joint box 4, a first spring strip 5, a first clamping hook 6, a first transverse shaft 7, a threaded hole 8, a threaded rod 9, a knob 10, an infrared scanner 11, a support rod 12, a connecting sheet 13, a sliding groove 14, a sliding block 15, a connecting rod 16, a second spring strip 17, a second transverse shaft 18, a transverse rod 19, a support frame 20, a blade base 21, a spring groove 22, a third spring strip 23, a limiting block 24, a first clamping block 25, a second clamping hook 26, a protective cover 27, a second clamping block 28 and a circular groove 29, wherein the connecting block 2 is connected to one side of the unmanned aerial vehicle body 1, the clamping groove 3 is formed in one side of the connecting block 2, the butt joint box 4 is arranged on the side of the connecting block 2 far away from the unmanned aerial vehicle body 1, the first spring strip 5 is connected to the inside of the butt joint box 4, one end of the first spring strip 5 is connected with the first clamping hook 6, the first clamping hooks 6 and the first cross shaft 7 are provided with two groups, a rotating structure is formed between the first clamping hooks 6 and the first cross shaft 7, the first clamping hooks 6 can rotate along the surface of the first cross shaft 7 when being extruded, when one end of each first clamping hook 6 rotates into the clamping groove 3, the two first clamping hooks 6 can clamp the connecting block 2, the first cross shaft 7 penetrates through the space between the first clamping hook 6 and the butt joint box 4, one side of the butt joint box 4 is provided with a threaded hole 8, the threaded holes 8 and the threaded rod 9 are provided with two groups, the threaded holes 8 and the threaded rod 9 are in threaded connection, the threaded rod 9 can be driven by the rotation of the knob 10, the threaded rod 9 can transversely move when rotating inside the threaded hole 8, the threaded rod 9 can transversely move to extrude the first clamping hooks 6, the threaded rod 9 penetrates through the inside the threaded hole 8, one end, far away from the first clamping hooks 6, of the threaded rod 9 is connected with the knob 10, one end of the butt joint box 4 far away from the connecting block 2 is connected with an infrared scanner 11;
one side of the unmanned aerial vehicle body 1 close to the connecting block 2 is connected with a supporting rod 12, a connecting piece 13 is connected between the supporting rods 12, a sliding groove 14 is formed in the surface of the connecting piece 13, two groups of sliding grooves 14 and two groups of sliding blocks 15 are arranged, the sliding grooves 14 and the sliding blocks 15 are connected in a sliding mode, the sliding blocks 15 are driven to slide in the sliding grooves 14 when the connecting rods 16 rotate along the surface of a second transverse shaft 18, the sliding blocks 15 penetrate through the sliding grooves 14, one end of each sliding block 15 is connected with a connecting rod 16, the connecting rods 16 and the second transverse shaft 18 are arranged in two groups, a rotating structure is formed between each connecting rod 16 and a transverse rod 19 through the second transverse shaft 18, a telescopic structure is formed between the connecting rods 16 through a second spring strip 17, the tops of the two connecting rods 16 are far away from each other when the connecting rods 16 rotate along the surface of the second transverse shaft 18, and the second spring strip 17 can reduce the rotating angle of the connecting rods 16 through self elasticity, a second spring strip 17 is connected between the connecting rods 16, the second transverse shaft 18 penetrates through the connecting rods 16, one end of the second transverse shaft 18 is connected with a transverse rod 19, and one side, far away from the support rod 12, of the transverse rod 19 is connected with a support frame 20;
one side of the unmanned aerial vehicle body 1 is connected with a blade base 21, the surface of the blade base 21 is provided with four groups of spring grooves 22, four groups of third spring strips 23 and four groups of limiting blocks 24, the spring grooves 22 and the limiting blocks 24 form a telescopic structure through the third spring strips 23, when a protective cover 27 moves to one end of the blade base 21, the first fixture block 25 is extruded, when a circular groove 29 moves to one side of the first fixture block 25, the first fixture block 25 can reset through the elastic force of the third spring strips 23, the first fixture block 25 is clamped and connected with the circular groove 29, the surface of the spring groove 22 is connected with the third spring strips 23, one end of the third spring strips 23 is connected with the limiting blocks 24, one side of the limiting blocks 24 far away from the third spring strips 23 is connected with the first fixture block 25, the surface of the blade base 21 is connected with a second clamping hook 26, the surface of the blade base 21 is sleeved with a second fixture block 28, one side of the second fixture block 28 is connected with a protective cover 27, and a circular groove 29 is formed on the surface of the protective cover 27 close to the first fixture block 25.
The working principle is as follows: when the infrared scanning device convenient to assemble for remote sensing of the unmanned aerial vehicle is used, firstly, the infrared scanning device convenient to assemble for remote sensing of the unmanned aerial vehicle needs to be simply known, when the infrared scanner 11 is assembled, the rotary knob 10 can drive the threaded rod 9 to rotate, when the threaded rod 9 rotates in the threaded hole 8, the threaded rod 9 can transversely move, the threaded rod 9 can extrude the first clamping hook 6, the first clamping hook 6 can rotate along the surface of the first transverse shaft 7 when extruded, when one end of the first clamping hook 6 rotates to the inside of the clamping groove 3, the two first clamping hooks 6 can clamp the connecting block 2, the infrared scanner 11 can be fixedly arranged at one end of the unmanned aerial vehicle body 1, when the protective cover 27 moves to one end of the blade base 21, the first clamping block 25 can be extruded, and the protective cover 27 can continuously operate upwards to drive the second clamping block 28 to slide in the second clamping hook 26, when the circular groove 29 moves to one side of the first fixture block 25, the first fixture block 25 can reset through the elastic force of the third spring strip 23, the first fixture block 25 is connected with the circular groove 29 in a clamping manner, the protective cover 27 is fixedly installed on the surface of the blade base 21, the unmanned aerial vehicle body 1 continues to move downwards according to inertia when the unmanned aerial vehicle lands, the unmanned aerial vehicle body 1 can move downwards through the support rod 12 to drive the connecting piece 13 to move downwards, the connecting piece 13 can move downwards to drive the connecting rod 16 to rotate along the surface of the second transverse shaft 18 through the sliding block 15, the sliding block 15 can slide in the sliding groove 14, because the second spring strip 17 is connected between the connecting rods 16, the second spring strip 17 can generate tensile force on the sliding block 15 through self elastic force, the rotation angle of the connecting rod 16 is reduced, the inertial displacement of the unmanned aerial vehicle body 1 is reduced, and the infrared scanning device convenient to assemble for remote sensing of the unmanned aerial vehicle has the characteristics of being convenient to assemble, those not described in detail in this specification are within the skill of the art.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.