CN209870769U - Unmanned aerial vehicle launcher - Google Patents

Abstract

The utility model provides an unmanned aerial vehicle launcher belongs to unmanned air vehicle technical field, including foot rest, well core rod and place the board, well core rod has been cup jointed in the activity of foot rest top, and well core rod and foot rest junction cup joint from bottom to top and are provided with connecting shaft section of thick bamboo and lifting sleeve, and well core rod top swing joint has places the board, places the board upper surface and passes through screw fixedly connected with bearing seat, places the board and openly imbeds and is provided with the level bubble, places the board lower fixed surface and is connected with the connecting block. This kind of unmanned aerial vehicle launcher sets up bearing seat and bell and spigot joint pipe, the solenoid that utilizes to be equipped with in the bearing seat circular telegram and produces magnetic field, and then makes the bell and spigot joint pipe cup joint on the unmanned aerial vehicle foot rest for the magnetic field that solenoid produced adsorbs the fixed action to the bell and spigot joint pipe production, and then reaches the purpose of facilitating the fixing to unmanned aerial vehicle.

Description

Unmanned aerial vehicle launcher

Technical Field

The utility model relates to an unmanned air vehicle technique field, more specifically the utility model relates to a launcher.

Background

Unmanned aerial vehicle is under the scientific and technological help of growing day by day, divide gradually into civilian unmanned aerial vehicle and for military use unmanned aerial vehicle that get into civilian market, wherein the most sizes of civilian unmanned aerial vehicle are less, many adopt vertical takeoff or take off the mode of gliding takeoff, wherein the unmanned aerial vehicle of vertical takeoff is when rugged topography uses, need utilize to help its stable support to assist and take off, but the current support is most to the unmanned aerial vehicle of vertical takeoff not have fixed measure or fixed means too complicated, be unfavorable for the use, lead to unmanned aerial vehicle to receive external factor influence easily at the in-process of taking off and cause the unsuccessful situation of taking off to take place, the rectangular form that current unmanned aerial vehicle foot rest bottom was made for light material mostly simultaneously is in order to improve.

Therefore, further research needs to be carried out on the basis of the existing launcher, and a new unmanned aerial vehicle launcher is provided.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the technical problem that current launching cradle is fixed inconvenient to unmanned aerial vehicle, provide an unmanned aerial vehicle launching cradle, set up bearing seat and cup joint pipe among the device, utilize the solenoid circular telegram that is equipped with in the bearing seat to produce magnetic field, and then make the cup joint pipe cup joint on the unmanned aerial vehicle foot rest for the magnetic field that solenoid produced adsorbs the fixed action to cup joint pipe production, and then reaches the purpose of facilitating the fixing to unmanned aerial vehicle.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle launcher comprises a foot rest, a central rod and a placing plate, wherein the central rod is movably sleeved at the top end of the foot rest, a connecting shaft barrel and a lifting sleeve are sleeved at the joint of the central rod and the foot rest from bottom to top, and the placing plate is movably connected at the top of the central rod;

the improved socket is characterized in that the upper surface of the placing plate is provided with a bearing seat through a screw fixedly connected with, the front surface of the placing plate is embedded with a horizontal bubble, the lower surface of the placing plate is fixedly connected with a connecting block, the top opening of the bearing seat is provided with a clamping groove, the inner wall of the clamping groove is embedded with a magnetic plate, the bearing seat is internally embedded with an electromagnetic coil, a socket pipe is embedded in the clamping groove in a movable manner, the upper side and the lower side of the socket pipe are fixedly connected with clamping plates, the clamping plates are internally provided with fixing screws in a penetrating mode, the socket pipe is internally embedded with an anti-.

Further preferred embodiments: the clamping groove is in a trapezoid shape with a large upper part and a small lower part, and the width of the clamping groove is matched with the diameter of the sleeve pipe.

Further preferred embodiments: the sleeve joint pipe is formed by assembling two halves in a split mode, and the two clamping plates are arranged on the edge of the sleeve joint pipe in a group.

Further preferred embodiments: the outer wall of the sleeving pipe is made of an iron material, and the magnetic plate is also made of the iron material.

Further preferred embodiments: the thickness of the anti-skid layer is at least 5mm, and the anti-skid layer is made of rubber materials.

Further preferred embodiments: the anti-skid convex edge is obliquely arranged on the outer surface of the sleeve pipe in a cross shape, and the surface of the magnetic plate is provided with a groove matched with the magnetic plate.

Further preferred embodiments: the electromagnetic coil is electrically connected with an external control terminal through a lead.

Has the advantages that:

1. this kind of unmanned aerial vehicle launcher, through setting up the bearing seat, the bearing seat utilizes solenoid circular telegram to produce magnetic field, and the pipe cup joints the unmanned aerial vehicle foot rest simultaneously and places at the draw-in groove, adsorbs the pipe cup with the magnetic field that solenoid produced, and then makes unmanned aerial vehicle fix and prevent to remove on the bearing seat.

2. Through setting up anti-skidding chimb, the pipe cup utilizes anti-skidding chimb to agree with mutually with the recess on the magnetic force board and fixes, and further effectively prevents that the pipe cup from sliding at the draw-in groove, improves pipe cup stability.

Drawings

Fig. 1 is a schematic view of the overall plane structure of the present invention.

Fig. 2 is a schematic view of the overlooking structure of the foot stool and the connecting shaft cylinder of the present invention.

Fig. 3 is a schematic view of a three-dimensional structure of the bearing seat of the present invention.

Fig. 4 is a schematic side sectional view of the bearing seat of the present invention.

Fig. 5 is a schematic view of the ferrule plane structure of the present invention.

In FIGS. 1-5: 1-a foot rest; 101-connecting shaft cylinder; 102-a lifting sleeve; 2-a central rod; 3, placing a plate; 301-a bearing seat; 3011-a card slot; 3012-magnetic plate; 3013-an electromagnetic coil; 302-horizontal bubble; 303-connecting block; 304-a ferrule; 3041-a splint; 3042-an anti-slip layer; 3043-a set screw; 3044-anti-slip flange.

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.

Example (b):

referring to fig. 1-5, in the embodiment of the present invention, an unmanned aerial vehicle launcher includes a foot rest 1, a connecting shaft cylinder 101, a lifting sleeve 102, a central rod 2, a placing plate 3, a bearing seat 301, a clamping groove 3011, a magnetic plate 3012, an electromagnetic coil 3013, a horizontal bubble 302, a connecting block 303, a sleeve 304, a clamping plate 3041, an anti-slip layer 3042, a fixing screw 3043 and an anti-slip flange 3044, wherein the central rod 2 is movably sleeved on the top end of the foot rest 1, the connecting shaft cylinder 101 and the lifting sleeve 102 are sleeved at the joint of the central rod 2 and the foot rest 1 from bottom to top, the placing plate 3 is movably connected to the top of the central rod 2, the bearing seat 301 is fixedly connected to the upper surface of the placing plate 3 through a screw, the horizontal bubble 302 is embedded in the front surface of the placing plate 3, the connecting block 303 is fixedly connected to the lower surface of the placing plate 3, the clamping, the inside embedding of support seat 301 is provided with solenoid 3013, and the inside activity embedding of draw-in groove 3011 has cup joint pipe 304, and the equal fixedly connected with splint 3041 in both sides about the cup joint pipe 304, splint 3041 is inside to run through and is provided with set screw 3043, and the inside embedding of cup joint pipe 304 is provided with skid resistant course 3042, and the sculpture of cup joint pipe 304 surface is provided with antiskid chimb 3044.

In a preferable scheme, the clamping groove 3011 is in a trapezoid shape with a large upper part and a small lower part, and the width of the clamping groove 3011 is matched with the diameter of the sleeve 304, so that the support legs of the unmanned aerial vehicle with different diameters can be put down, and the practicability of the clamping groove 3011 is improved;

the socket 304 is formed by two halves of split bodies, and the clamp plate 3041 is provided with two clamp plates which are set at the edge of the socket 304, so that the socket 304 can be fixed on the legs of the unmanned aerial vehicle with different diameters;

the outer wall of the sleeve 304 is made of an iron material, and the magnetic plate 3012 is also made of an iron material, so that the sleeve 304 can be effectively adsorbed by a magnetic field generated by the electromagnetic coil 3013, and the connection stability between the sleeve 304 and the supporting base 301 is improved;

the thickness of the anti-slip layer 3042 is at least 5mm, and the anti-slip layer 3042 is made of a rubber material, so that when the sleeve 304 is fixed on the surface of the unmanned aerial vehicle support leg, no slip occurs, and the stability is improved;

the anti-slip flange 3044 is obliquely arranged on the outer surface of the ferrule 304 in a cross shape, the surface of the magnetic plate 3012 is provided with a groove matched with the surface of the ferrule 304, and the ferrule 304 is fixed by matching the anti-slip flange 3044 with the groove on the magnetic plate 3012, so that the ferrule 304 is further effectively prevented from sliding in the clamping groove 3011, and the stability of the ferrule 304 is improved;

solenoid 3013 passes through wire and external control terminal electric connection for solenoid 3013 circular telegram produces the magnetic field and adsorbs pipe sleeve 304, reaches the purpose that prevents unmanned aerial vehicle and remove.

The working principle is as follows: use the utility model relates to an unmanned aerial vehicle launcher, at first, place foot rest 1 at required operating position, place board 3 reference level bubble 302 adjustment horizontal position after that, utilize the wire to overlap solenoid 3013 and external control terminal electric connection simultaneously, cup joint pipe 304 at unmanned aerial vehicle stabilizer blade surface afterwards, utilize set screw 3043 solid fixed splint 3041, make skid resistant course 3042 closely laminate at unmanned aerial vehicle stabilizer blade surface, move unmanned aerial vehicle to draw-in groove 3011 afterwards in, utilize the magnetic field of solenoid 3013 circular telegram production to adsorb cup joint pipe 304, and then make unmanned aerial vehicle fix and prevent moving on bearing seat 301, when unmanned aerial vehicle need take off, make magnetic field disappear with solenoid 3013 outage, unmanned aerial vehicle can break away from magnetic field adsorption force and take off.

The above is only the preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, without departing from the concept of the present invention, several modifications and improvements can be made, which should also be regarded as the protection scope of the present invention, and these will not affect the effect of the implementation of the present invention and the practicability of the patent.

Claims (7)

1. An unmanned aerial vehicle launcher comprises a foot rest (1), a central rod (2) and a placing plate (3), wherein the central rod (2) is movably sleeved at the top end of the foot rest (1), a connecting shaft barrel (101) and a lifting sleeve (102) are sleeved at the joint of the central rod (2) and the foot rest (1) from bottom to top, and the placing plate (3) is movably connected to the top of the central rod (2);

the method is characterized in that: the novel multifunctional table rack is characterized in that the upper surface of the placing plate (3) is fixedly connected with a bearing seat (301) through screws, a horizontal bubble (302) is embedded into the front surface of the placing plate (3), the lower surface of the placing plate (3) is fixedly connected with a connecting block (303), a clamping groove (3011) is formed in the top opening of the bearing seat (301), a magnetic plate (3012) is embedded into the inner wall of the clamping groove (3011), an electromagnetic coil (3013) is embedded into the bearing seat (301), a sleeve pipe (304) is movably embedded into the clamping groove (3011), clamping plates (3041) are fixedly connected to the upper side and the lower side of the sleeve pipe (304), fixing screws (3043) penetrate through the clamping plates (3041), an anti-slip layer (3042) is embedded into the sleeve pipe (304), and an anti-slip convex edge (3044) is carved on.

2. An unmanned aerial vehicle launcher according to claim 1, wherein: the clamping groove (3011) is in a trapezoid shape with a large upper part and a small lower part, and the width of the clamping groove (3011) is matched with the diameter of the sleeve pipe (304).

3. An unmanned aerial vehicle launcher according to claim 1, wherein: the sleeve pipe (304) is formed by assembling two halves in a split mode, and the two clamping plates (3041) are arranged on the edge of the sleeve pipe (304) in a group.

4. An unmanned aerial vehicle launcher according to any one of claims 1 or 3, wherein: the outer wall of the sleeve pipe (304) is made of a ferrous material, and the magnetic plate (3012) is also made of the ferrous material.

5. An unmanned aerial vehicle launcher according to claim 1, wherein: the thickness of the anti-slip layer (3042) is at least 5mm, and the anti-slip layer (3042) is made of a rubber material.

6. An unmanned aerial vehicle launcher according to claim 1, wherein: the anti-skid convex edge (3044) is obliquely arranged on the outer surface of the sleeve pipe (304) in a cross shape, and the surface of the magnetic plate (3012) is provided with a groove matched with the magnetic plate.

7. An unmanned aerial vehicle launcher according to claim 1, wherein: the electromagnetic coil (3013) is electrically connected with an external control terminal through a lead.