Unmanned aerial vehicle base with clamping function

Abstract

The unmanned aerial vehicle base with the clamping function comprises a fixed base, a bearing mechanism, an adjusting mechanism and an unmanned aerial vehicle body, and the adjusting mechanism is connected to the top of the fixed base in a sliding mode. Compared with the prior art, the unmanned aerial vehicle has the advantages that by arranging the bearing mechanism and the adjusting mechanism, the unmanned aerial vehicle body abuts against the abutting seat, then the rack is driven to slide, the linkage plate and the clamping plate are synchronously driven to be in linkage, and the clamping plate abuts against the unmanned aerial vehicle body to form a gravity self-locking structure; by means of the gravity self-locking structure, on one hand, the clamping and limiting effect on the unmanned aerial vehicle body is achieved, the unmanned aerial vehicle body is prevented from falling off when being touched and collided by mistake, on the other hand, personnel can operate the unmanned aerial vehicle body conveniently, the unmanned aerial vehicle body can be clamped synchronously when placed, and the unmanned aerial vehicle is simple and practical; and the distance between every two adjacent bearing mechanisms can be adjusted, and therefore the unmanned aerial vehicle base can be suitable for unmanned aerial vehicle bodies of different sizes.

Description

TECHNICAL FIELD

[0001] The utility model relates to an unmanned plane base, specifically an unmanned plane base with clamping function, and belongs to the technical field of unmanned plane base. BACKGROUND

[0002] An unmanned plane is a kind of unmanned aircraft that is controlled by radio remote control equipment and self-provided program control device, and can be divided into unmanned helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aircraft, unmanned airship and unmanned parachute wing aircraft from the technical point of view, and when the unmanned plane is not used or displayed, it is generally placed on a base to ensure the stability of the unmanned plane and avoid falling and damage due to accidental touch and collision.

[0003] However, the existing unmanned plane base has various problems, for example, in the unmanned plane protection base disclosed in the publication No. CN105398574A, the unmanned plane is reinforced by installing the protection base to improve the stability of the unmanned plane, and the base body and the unmanned plane can be detachably connected, can be installed and detached according to the use requirement, the base body can strengthen the collision ability of the unmanned plane after installation, and the reinforced base plate can avoid the occurrence of side turning, the base can only be used to protect the bottom of the unmanned plane and can support and fix the unmanned plane, and although some bases have the supporting and clamping locking function for the unmanned plane, most of the clamping structures need to be manually operated, for example, the clamping head is driven in linkage by the thread linkage of the screw rod to realize the clamping function by abutting against the unmanned plane, this method can fix the unmanned plane, but the operation is too complicated and time-consuming and laborious. UTILITY MODEL CONTENT

[0004] The utility model technical scheme provides a solution significantly different from the prior art to solve the technical problem that the prior art solution is too single, specifically, the purpose of the utility model is to solve the above-mentioned shortcomings in the prior art, and a kind of unmanned plane base with clamping function is proposed.

[0005] In order to realize the above-mentioned purpose, the utility model adopts the following technical scheme:

[0006] An unmanned plane base with clamping function, comprising a fixed base, a supporting mechanism, an adjusting mechanism and an unmanned plane body, the adjusting mechanism is slidably connected to the top of the fixed base, the supporting mechanism is arranged on the top of the adjusting mechanism, and the unmanned plane body is placed on the supporting mechanism.

[0007] The supporting mechanism comprises a supporting seat, a linkage plate, a clamping plate, a rack and an abutting seat, the supporting seat is arranged on the top of the fixed base, one end of the linkage plate is rotationally connected to the supporting seat, the clamping plate is rotationally connected to the other end of the linkage plate, a notch is arranged in the center of the top of the supporting seat, the rack is slidingly connected in the notch, the rack is arranged in the vertical direction, the abutting seat is fixed to the top end of the rack, one end of the clamping plate is rotationally connected to the abutting seat, and the other end of the clamping plate abuts against the body of the unmanned aerial vehicle.

[0008] As a further scheme of the utility model, the supporting mechanism further comprises a limiting plate and a reset spring, the limiting plate is rotationally connected to the supporting seat, and the limiting plate is connected with the rack slot, and the reset spring is arranged between the limiting plate and the supporting seat.

[0009] As a further scheme of the utility model, the adjusting mechanism comprises a sliding groove and a sliding block, the sliding groove is arranged on the top end of the fixed base, the sliding block is slidingly connected in the sliding groove, and the supporting seat is rotationally connected to the sliding block.

[0010] As a further scheme of the utility model, the adjusting mechanism further comprises a butt joint groove, a lock rod and a positioning hole, the butt joint groove is horizontally arranged on the sliding block and penetrates left and right, the lock rod is slidingly connected in the butt joint groove, the positioning hole is concavely arranged on the inner wall of the sliding groove and is equidistantly provided with a plurality of positioning holes, and one end of the lock rod is connected to one of the positioning holes.

[0011] As a further scheme of the utility model, the adjusting mechanism further comprises a driven rod and an adjusting groove, a vertical notch is arranged on the top of the sliding block and penetrates the butt joint groove, the driven rod is fixed to the lock rod and passes through the vertical notch, the adjusting groove is in an elliptical structure and is arranged on the bottom of the supporting seat, and one end of the driven rod is slidingly connected in the adjusting groove.

[0012] As a further scheme of the utility model, the inside of the supporting seat is provided with a reset spring, and one end of the reset spring abuts against the bottom of the rack.

[0013] The utility model has the advantages of:

[0014] The utility model discloses a bearing mechanism and adjusting mechanism are set up, and then through the abutment of unmanned aerial vehicle body and abutment seat, and then drive rack slide, and synchronous linkage board, clamping plate linkage, make clamping plate and unmanned aerial vehicle body abutment constitute gravity self -locking structure, through gravity self -locking structure, on one hand realized for the clamping limiting effect of unmanned aerial vehicle body, avoid unmanned aerial vehicle body when being mistaken touch collision and fall, on the other hand, personnel are also convenient for operation, make unmanned aerial vehicle body when placing can be synchronous clamping, simple and practical, and through the setting of adjusting mechanism, the spacing of adjacent two groups of bearing mechanism can be adjusted, and then the unmanned aerial vehicle base can be applicable to unmanned aerial vehicle body of different size, improve the scope of application. BRIEF DESCRIPTION OF DRAWINGS

[0015] Figure 1 It is overall structure schematic diagram of the utility model;

[0016] Figure 2 It is bearing mechanism structure schematic diagram of the utility model;

[0017] Figure 3 It is adjusting mechanism structure schematic diagram of the utility model;

[0018] Figure 4 It is bearing seat overall connection structure schematic diagram of the utility model;

[0019] Figure 5 It is limiting plate structure schematic diagram of the utility model;

[0020] Figure 6 It is sliding block and its connection structure schematic diagram of the utility model.

[0021] In the drawing: 1, fixed base, 2, bearing mechanism, 21, bearing seat, 22, linkage board, 23, clamping plate, 24, rack, 25, abutment seat, 26, limiting plate, 27, return spring, 3, adjusting mechanism, 31, sliding slot, 32, sliding block, 33, butt joint groove, 34, lock rod, 35, positioning hole, 36, driven rod, 37, adjusting groove, 4, unmanned aerial vehicle body. DETAILED DESCRIPTION

[0022] The technical scheme in the embodiments of the utility model will be described clearly and completely below in conjunction with the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of the utility model. EMBODIMENT

[0023] As Figures 1 to 6As shown, a drone base with clamping function includes a fixed base 1, a support mechanism 2, an adjustment mechanism 3 and a drone body 4. The adjustment mechanism 3 is slidably connected to the top of the fixed base 1, the support mechanism 2 is disposed on the top of the adjustment mechanism 3, and the drone body 4 is placed on the support mechanism 2.

[0024] The support mechanism 2 includes a support seat 21, a linkage plate 22, a clamping plate 23, a rack 24, and an abutment seat 25. The support seat 21 is set on the top of the fixed base 1. One end of the linkage plate 22 is rotatably connected to the support seat 21. The center of the clamping plate 23 is rotatably connected to the other end of the linkage plate 22. A groove is recessed in the center of the top of the support seat 21. The rack 24 is slidably engaged in the groove. The rack 24 is slidably set in the vertical direction. The abutment seat 25 is fixed to the top of the rack 24. One end of the clamping plate 23 is rotatably connected to the abutment seat 25, and the other end abuts against the UAV body 4.

[0025] The supporting mechanism 2 also includes a limiting plate 26 and a return spring 27. The limiting plate 26 is rotatably connected to the supporting seat 21, and the limiting plate 26 is engaged with the tooth groove of the rack 24. The return spring 27 is disposed between the limiting plate 26 and the supporting seat 21.

[0026] The adjustment mechanism 3 includes a slide groove 31 and a slider 32. The slide groove 31 is recessed at the top of the fixed base 1. The slider 32 is slidably engaged in the slide groove 31, and the support seat 21 is rotatably connected to the slider 32.

[0027] In this utility model, by setting up a support mechanism 2 and an adjustment mechanism 3, the drone body 4 abuts against the abutment seat 25, thereby driving the rack 24 to slide, and simultaneously driving the linkage plate 22 and clamping plate 23 to move together, so that the clamping plate 23 abuts against the drone body 4 to form a gravity self-locking structure. The gravity self-locking structure achieves the clamping and limiting effect of the drone body 4, preventing the drone body 4 from falling when accidentally touched or bumped. On the other hand, it also facilitates operation by personnel, so that the drone body 4 can be clamped synchronously when placed. It is simple and practical. By setting up the adjustment mechanism 3, the distance between the two adjacent sets of support mechanisms 2 can be adjusted, so that the drone base can be used for drone bodies 4 of different sizes, thus improving the applicability. Example

[0028] like Figures 1 to 6 As shown, in addition to all the technical features included in Embodiment 1, this embodiment also includes:

[0029] The adjustment mechanism 3 also includes a docking groove 33, a locking rod 34, and a positioning hole 35. The docking groove 33 is horizontally arranged on the slider 32 and extends through it. The locking rod 34 is slidably engaged in the docking groove 33. The positioning hole 35 is recessed in the inner wall of the slide groove 31 and is provided in multiple equidistant locations. One end of the locking rod 34 is engaged in one of the positioning holes 35. By docking the locking rod 34 with the positioning hole 35, the limiting and locking effect of the slider 32 is achieved, preventing the slider 32 from sliding during use.

[0030] The adjustment mechanism 3 also includes a driven rod 36 and an adjustment groove 37. The top of the slider 32 is provided with a vertical groove, which is connected to the docking groove 33. The driven rod 36 is fixed on the locking rod 34 and passes through the vertical groove. The adjustment groove 37 has an elliptical structure and is provided at the bottom of the support 21. One end of the driven rod 36 is slidably engaged in the adjustment groove 37. The rotation of the support 21 drives the adjustment groove 37 to deflect. At the same time as the deflection, the driven rod 36 moves in conjunction in the adjustment groove 37 and simultaneously drives the slider 32 to slide, so that the slider 32 can quickly dock with and separate from the positioning hole 35.

[0031] The support 21 is equipped with a return spring, and one end of the return spring abuts against the bottom of the rack 24. The rack 24 can be quickly reset by the return spring.

[0032] Working principle: When using this drone base, first adjust the distance between the two adjacent sets of support mechanisms 2 according to the actual situation. During adjustment, first rotate the support seat 21 to make the driven rod 36 slide in the adjustment groove 37, thereby driving the locking rod 34 to slide and separate from the positioning hole 35. At this time, slide the slider 32 in the sliding groove 31 until the appropriate position is reached. Then reverse the support seat 21 so that one end of the locking rod 34 is connected to the positioning hole 35. Then, the drone body 4 abuts against the abutment seat 25. The weight of the drone body 4 pushes the rack 24 to slide, and simultaneously drives the linkage plate 22 and the clamping plate 23 to move together, so that the clamping plate 23 abuts against the drone body 4 and locks it.

[0033] It will be apparent to those skilled in the art that this invention is not limited to the details of the exemplary embodiments described above, and that it can be implemented in other specific forms without departing from the spirit or essential characteristics of this invention. Therefore, the embodiments should be considered illustrative and non-limiting in all respects, and the scope of this invention is defined by the appended claims rather than the foregoing description. Thus, it is intended that all variations falling within the meaning and scope of equivalents of the claims be included within this invention. No reference numerals in the claims should be construed as limiting the scope of the claims.

[0034] Furthermore, it should be understood that although this specification describes embodiments, not every embodiment contains only one independent technical solution. This narrative style is merely for clarity. Those skilled in the art should consider the specification as a whole, and the technical solutions in each embodiment can also be appropriately combined to form other embodiments that can be understood by those skilled in the art.

Claims

1. A drone base with clamping function, comprising a fixed base (1), a supporting mechanism (2), an adjusting mechanism (3), and a drone body (4), characterized in that, The adjustment mechanism (3) is slidably connected to the top of the fixed base (1), the support mechanism (2) is set on the top of the adjustment mechanism (3), and the UAV body (4) is placed on the support mechanism (2); The supporting mechanism (2) includes a support seat (21), a linkage plate (22), a clamping plate (23), a rack (24), and an abutment seat (25). The support seat (21) is set on the top of the fixed base (1). One end of the linkage plate (22) is rotatably connected to the support seat (21). The center of the clamping plate (23) is rotatably connected to the other end of the linkage plate (22). A groove is recessed at the center of the top of the support seat (21). The rack (24) is slidably engaged in the groove. The rack (24) is slidably arranged in the vertical direction. The abutment seat (25) is fixed on the top of the rack (24). One end of the clamping plate (23) is rotatably connected to the abutment seat (25), and the other end abuts against the UAV body (4).

2. The drone base with clamping function according to claim 1, characterized in that: The supporting mechanism (2) further includes a limiting plate (26) and a return spring (27). The limiting plate (26) is rotatably connected to the supporting seat (21), and the limiting plate (26) is engaged with the tooth groove of the rack (24). The return spring (27) is disposed between the limiting plate (26) and the supporting seat (21).

3. A drone base with clamping function according to claim 1, characterized in that: The adjustment mechanism (3) includes a groove (31) and a slider (32). The groove (31) is recessed at the top of the fixed base (1). The slider (32) is slidably engaged in the groove (31), and the support (21) is rotatably connected to the slider (32).

4. A drone base with clamping function according to claim 3, characterized in that: The adjustment mechanism (3) also includes a docking groove (33), a locking rod (34) and a positioning hole (35). The docking groove (33) is horizontally arranged on the slider (32) and extends through the left and right sides. The locking rod (34) is slidably engaged in the docking groove (33). The positioning hole (35) is recessed in the inner wall of the slide groove (31) and is provided in multiple equidistant locations. One end of the locking rod (34) is engaged in one of the positioning holes (35).

5. A drone base with clamping function according to claim 4, characterized in that: The adjustment mechanism (3) further includes a driven rod (36) and an adjustment groove (37). The top of the slider (32) is provided with a vertical groove, and the vertical groove is connected to the docking groove (33). The driven rod (36) is fixed on the locking rod (34), and the driven rod (36) passes through the vertical groove. The adjustment groove (37) has an elliptical structure and is provided at the bottom of the support (21). One end of the driven rod (36) is slidably engaged in the adjustment groove (37).

6. A drone base with clamping function according to claim 1, characterized in that: The support (21) is equipped with a return spring inside, and one end of the return spring abuts against the bottom of the rack (24).

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