Fixing device for mounting and debugging vertical fixed-wing unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicle auxiliary tools, and discloses a vertical fixed wing unmanned aerial vehicle installation debugging fixing device which comprises a first supporting leg and a second supporting leg, the second supporting leg is rotationally installed on the inner side of the first supporting leg through an installation bolt, and a fixing supporting pad is fixedly installed at the top end of the first supporting leg and the top end of the second supporting leg. A lock disc is fixedly connected to the center of one side of the second supporting leg, a pull rod is slidably installed in the first supporting leg, a clamping rod is fixedly connected to the lower end of the pull rod, a plurality of buckles matched with the clamping rod in an adaptive mode are arranged on the outer ring of the lock disc, and a pull handle is fixedly connected to the end, away from the clamping rod, of the pull rod. Through the second supporting legs, the second locking rotary knobs, the supporting rods, the first locking rotary knobs, the supporting rods, the fixing plates and the inserting needles, the extending distance of the supporting rods can be adjusted according to the ground condition, the applicability is high, and the sliding probability of the supporting rods after arrangement is reduced.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned aerial vehicle auxiliary tool technical field, concretely is a vertical takeoff fixed wing unmanned aerial vehicle installation debugging fixing device. BACKGROUND

[0002] The vertical takeoff fixed wing unmanned aerial vehicle is a kind of aircraft that combines the advantages of fixed wing and multi-rotor unmanned aerial vehicle, has vertical takeoff and landing capability, and can also realize the efficient flight of fixed wing, without long runway, can vertically take off and land in narrow space, adapt to complex terrain.

[0003] Chinese patent provides a kind of unmanned aerial vehicle fixed wing platform with clamping connection structure, and the publication number is CN221273591U, including two bottom plates, the upper surface of two bottom plates is equipped with clamping mechanism, the clamping mechanism includes two mounting plates, two mounting plates are fixedly connected on the upper surface of bottom plate, the upper surface of mounting plate is all equipped with clamping groove.

[0004] The takeoff platform described above is provided with clamping mechanism, when installing the device body, rotating the rotating plate, so that the rotating plate supports the bottom plate, when the rotating rod is clamped with the clamping groove, the insertion rod is inserted through the mounting plate, when the insertion rod is installed, the clamping block is clamped with the insertion rod, so that the insertion rod limits the rotating rod, which is convenient for staff to install and disassemble, and prepares for the takeoff work of fixed wing unmanned aerial vehicle, improves work efficiency;

[0005] But it can only adjust takeoff angle, it is difficult to adjust the height of supporting leg, when taking off in complex terrain, it is difficult to lay out, affect the debugging efficiency, and directly flat on the ground, when supporting unmanned aerial vehicle on soft ground, the bottom may slide, affect the stability of support. Utility model content

[0006] The utility model aims at providing a kind of vertical takeoff fixed wing unmanned aerial vehicle installation debugging fixing device, can effectively solve the problems in the background art.

[0007] To achieve the above object, the utility model provides the following technical scheme:

[0008] A vertical takeoff fixed wing unmanned aerial vehicle installation debugging fixing device, including support leg one, support leg two, the support leg two is rotatably installed in the inner side of support leg one by mounting bolt, the top of support leg one and support leg two is fixedly installed with fixed support pad;

[0009] The side center position of the supporting leg two is fixedly connected with a lock disc, the inside of the supporting leg one is slidably installed with a pull rod, the lower end of the pull rod is fixedly connected with a clamping rod, the outer ring of the lock disc is provided with a plurality of buckles adaptively matched with the clamping rod, the end of the pull rod away from the clamping rod is fixedly connected with a pull handle, the inside of the supporting leg one and close to the end of the clamping rod is fixedly installed with a push plate, the outer ring of the pull rod and close to one of the push plates is fixedly connected with an abutting block, a reset spring is arranged around the outer ring of the pull rod, and the opposite surfaces of the push plate and the abutting block are respectively abutted with the two ends of the reset spring.

[0010] Preferably, the pull rod and the clamping rod are combined to be arranged in an "L" shape, and the clamping rod is clamped into one of the buckles on the lock disc.

[0011] Preferably, the bottom end of the supporting leg two is movably installed with a supporting leg two, and a locking knob two is threadedly connected through one side of the supporting leg two and close to the lower position, a plurality of adjusting holes two adaptively matched with the locking knob two are formed in one side of the supporting leg two.

[0012] Preferably, the bottom end of the supporting leg one is slidably installed with a supporting leg one, a locking knob one is threadedly connected through one side of the supporting leg one and away from the supporting leg two and close to the lower position, and a plurality of adjusting holes one adaptively matched with the supporting leg one are formed in one side of the supporting leg one away from the supporting leg two.

[0013] Preferably, the front end and the rear end of the supporting rod are both sleeved with anti-skid rubber sleeves, and the outer ring of the supporting rod is fixedly connected with a fixed plate close to the middle position and both ends.

[0014] Preferably, a plug pin is arranged through the upper end and the lower end of the fixed plate, and the lower part of the plug pin is arranged in a sharp shape.

[0015] Compared with the prior art, the utility model has the advantages that:

[0016] The utility model discloses a supporting leg two, a locking knob two, a supporting rod, a locking knob one and a supporting leg one are matched with each other, when the fixed supporting pad is arranged, the extension distance of the supporting rod can be adjusted according to the ground condition, the applicability is higher, the probability that the uneven ground influences the debugging efficiency is reduced, and the distance between the fixed supporting pads can be adjusted according to the size of the unmanned aerial vehicle through the pull handle, the lock disc, the pull rod, the clamping rod and the reset spring, and the use flexibility is higher.

[0017] The supporting rod, the fixed plate and the plug pin are matched with each other, when the ground is relatively soft, the plug pin can be inserted into the soil through the fixed plate by means of a tool, so that the overall ground holding capacity of the supporting rod is improved, the supporting stability is facilitated to be improved, the probability that the supporting rod slides after being arranged is reduced, and the supporting rod can be stored and carried by being rotated when not in use. BRIEF DESCRIPTION OF DRAWINGS

[0018] Figure 1 It is the overall structure schematic view of the vertical fixed-wing unmanned aerial vehicle installation and debugging fixing device in the embodiment of the utility model;

[0019] Figure 2 It is the connection place schematic view of the support leg two and the locking knob two in the embodiment of the utility model;

[0020] Figure 3 It is the structure schematic view of the pull rod and the reset spring in the embodiment of the utility model;

[0021] Figure 4 It is the demonstration view after the fixed support pad is stored in the embodiment of the utility model.

[0022] In the drawing: 1, support leg one; 2, support leg two; 3, fixed support pad; 4, lock disc; 5, pull rod; 6, clamping rod; 7, push plate; 8, reset spring; 9, pull handle; 10, support leg one; 11, locking knob one; 12, support leg two; 13, locking knob two; 14, support rod; 15, fixed plate; 16, insertion pin. DETAILED DESCRIPTION

[0023] The technical scheme in the embodiment of the utility model will be clearly and completely described below in combination with the drawings in the embodiment of the utility model, and obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by the person skilled in the art without creative labor fall within the protection scope of the utility model.

[0024] Embodiment one

[0025] In combination with Figures 1-4 A vertical fixed-wing unmanned aerial vehicle installation and debugging fixing device, comprising support leg one 1, support leg two 2, the support leg two 2 is rotatably installed on the inner side of the support leg one 1 through mounting bolts, and the top end of the support leg one 1 and the support leg two 2 is fixedly installed with a fixed support pad 3.

[0026] Referring to Figure 2 And Figure 3, further get, the side of the supporting leg two 2 is fixedly connected with a lock disc 4 at the central position, the inside of the supporting leg one 1 is slidably installed with a pull rod 5, the lower end of the pull rod 5 is fixedly connected with a clamping rod 6, the outer ring of the lock disc 4 is provided with a plurality of buckles adaptively matched with the clamping rod 6, the end of the pull rod 5 away from the clamping rod 6 is fixedly connected with a pull handle 9, the inside of the supporting leg one 1 and close to the end of the clamping rod 6 is fixedly installed with a push plate 7, the outer ring of the pull rod 5 and close to the end of one of the push plates 7 is fixedly connected with an abutting block, a return spring 8 is arranged around the outer ring of the pull rod 5, the two ends of the return spring 8 are respectively in abutment with the opposite surfaces of the push plate 7 and the abutting block, the pull rod 5 and the clamping rod 6 are combined to be arranged in the shape of "L", and the clamping rod 6 is clamped into one of the buckles on the lock disc 4, the bottom end of the supporting leg two 2 is movably installed with a supporting leg two 12, a locking knob two 13 is threadedly connected through the lower side of the supporting leg two 12, a plurality of adjusting holes two adaptively matched with the locking knob two 13 are formed in the side of the supporting leg two 12, the bottom end of the supporting leg one 1 is slidably installed with a supporting leg one 10, a locking knob one 11 is threadedly connected through the lower side of the side of the supporting leg one 1 away from the supporting leg two 2, and a plurality of adjusting holes one adaptively matched with the supporting leg one 10 are formed in the side of the supporting leg one 10 away from the supporting leg two 2.

[0027] Specifically, when laying, the pull handle 9 can be pulled away from the lock disc 4, the pull rod 5 is slidably driven in the supporting leg one 1 by the pull handle 9, the clamping rod 6 is separated from the fixed buckle of the lock disc 4, the fixing of the supporting leg two 2 and the supporting leg one 1 is released, then the two fixed supporting pads 3 can be pulled away, after the fixed supporting pads 3 are unfolded, they are placed on the ground through the supporting rod 14, and then the vertically fixed wing unmanned aerial vehicle can be placed on the fixed supporting pads 3 to complete the fixed placement process, subsequent debugging and take-off can be carried out, and when placing, the clamping rod 6 can be clamped in different buckles of the lock disc 4 according to the size of the unmanned aerial vehicle to limit the distance between the fixed supporting pads 3, and when the supporting rod 14 supports, the locking knob two 13 or the locking knob one 11 can be screwed to release the fixing of the supporting leg two 12 and the supporting leg one 10, then the supporting leg two 12 or the supporting leg one 10 can be pulled out according to the ground conditions to adjust the supporting height, so as to adapt to different road surfaces.

[0028] Embodiment two

[0029] Referring to Figure 2 and Figure 4 , and on the basis of embodiment one, further get that the front and rear ends of the supporting rod 14 are sleeved with anti-skid rubber sleeves, the outer ring of the supporting rod 14 is fixedly connected with a fixed plate 15 close to the central position and the two ends, the upper and lower ends of the fixed plate 15 are provided with insertion pins 16, and the lower part of the insertion pin 16 is provided in the shape of a sharp.

[0030] Specifically, when being arranged in a relatively soft soil body, the insertion needle 16 can be inserted into the ground soil through the fixing plate 15 by means of a tool after the support rod 14 is stably supported, so as to improve the ground adhesion of the support rod 14, avoid displacement of the support rod 14 caused by collision, improve the fixing stability, and reset the fixing support pad 3 when not in use, so as to reduce the occupied space of the fixing support pad 3 and facilitate personnel carrying.

[0031] In actual operation, when being arranged, the pull handle 9 can be pulled away from the lock disc 4, the pull rod 5 is driven to slide in the support leg one 1, the clamping rod 6 is driven to disengage from the fixing buckle at the lock disc 4, the fixing of the support leg two 2 and the support leg one 1 is released, then the two fixing support pads 3 are pulled away, and after the fixing support pads 3 are unfolded, they are placed on the ground by the support rod 14, and then the vertically fixed wing unmanned aerial vehicle can be placed on the fixing support pad 3 to complete the fixing and placing process, and subsequent take-off debugging can be performed.

[0032] When being placed, the clamping rod 6 can be clamped in different buckles at the lock disc 4 according to the size of the unmanned aerial vehicle, so as to limit the distance between the fixing support pads 3, thereby providing support and fixing effect for unmanned aerial vehicles of different sizes, and when the support rod 14 is supported, the locking knob two 13 or the locking knob one 11 can be screwed, so as to release the fixing of the support leg two 12 or the support leg one 10, then the support leg two 12 or the support leg one 10 is pulled out according to the ground condition to adjust the support height, so as to adapt to different road surfaces.

[0033] When being arranged in a relatively soft soil body, the insertion needle 16 can be inserted into the ground soil through the fixing plate 15 by means of a tool after the support rod 14 is stably supported, so as to improve the ground adhesion of the support rod 14, avoid displacement of the support rod 14 caused by collision, improve the fixing stability, and reset the fixing support pad 3 when not in use, so as to reduce the occupied space of the fixing support pad 3 and facilitate personnel carrying.

[0034] Although the embodiments of the present application have been shown and described, it can be understood by those skilled in the art that various changes, modifications, replacements and modifications can be made to the embodiments without departing from the principles and spirits of the present application, the scope of the present application is defined by the appended claims and their equivalents.

Claims

1. A mounting and fixing device for a vertical take-off and landing fixed-wing unmanned aerial vehicle (UAV), characterized in that: Including support leg one (1), support leg two (2), support rod (14), support leg two (2) is rotatably mounted on the inner side of support leg one (1) by mounting bolt, the top end of support leg one (1) and support leg two (2) is fixedly installed with fixed support pad (3); The side of the support leg two (2) is fixedly connected with the lock disc (4) in the middle position, the inside of the support leg one (1) is slidably installed with the pull rod (5), the lower end of the pull rod (5) is fixedly connected with the clamping rod (6), the outer ring of the lock disc (4) is provided with a plurality of buckles adaptively matched with the clamping rod (6), the end of the pull rod (5) away from the clamping rod (6) is fixedly connected with the pull handle (9), the inside of the support leg one (1) and close to one end of the clamping rod (6) is fixedly installed with the push plate (7), the outer ring of the pull rod (5) and close to one end of the push plate (7) is fixedly connected with the abutment, the outer ring of the pull rod (5) is provided with the reset spring (8), and the two ends of the reset spring (8) are respectively abutted with the opposite surfaces of the push plate (7) and the abutment.

2. The installation and debugging fixing device for vertical take-off fixed-wing unmanned aerial vehicle according to claim 1, characterized in that: The pull rod (5) and the clamping rod (6) are combined to be provided in the shape of "L", and the clamping rod (6) is clamped into one of the buckles on the lock disc (4).

3. The installation and debugging fixing device for vertical take-off fixed-wing unmanned aerial vehicle according to claim 1, characterized in that: The bottom end of the support leg two (2) is movably installed with the support leg two (12), and the lock knob two (13) is threadedly connected through one side of the support leg two (12) close to the lower position, and a plurality of adjustment holes two adaptively matched with the lock knob two (13) are formed in one side of the support leg two (12).

4. The installation and debugging fixing device for vertical take-off fixed-wing unmanned aerial vehicle according to claim 1, characterized in that: The bottom end of the support leg one (1) is slidably installed with the support leg one (10), and the lock knob one (11) is threadedly connected through one side of the support leg one (1) away from the support leg two (2) close to the lower position, and a plurality of adjustment holes one adaptively matched with the support leg one (10) are formed in one side of the support leg one (10) away from the support leg two (2).

5. The installation and debugging fixing device for vertical take-off fixed-wing unmanned aerial vehicle according to claim 1, characterized in that: The front and rear ends of the support rod (14) are provided with anti-skid rubber sleeves, and the outer ring of the support rod (14) is fixedly connected with the fixed plate (15) close to the middle and both ends.

6. The installation and debugging fixing device for vertical take-off fixed-wing unmanned aerial vehicle according to claim 5, characterized in that: The upper and lower ends of the fixed plate (15) are provided with the insertion needle (16), and the lower part of the insertion needle (16) is provided in the shape of a sharp.

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