Wing seat structure of unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicle wing seats, in particular to an unmanned aerial vehicle wing seat structure which comprises an unmanned aerial vehicle wing seat body, a circular ring is fixedly connected to the upper side of the unmanned aerial vehicle wing seat body, two mounting holes are formed in the upper side of the unmanned aerial vehicle wing seat body, and a wing support is fixedly arranged in the circular ring. The wing seat and the wing support of the unmanned aerial vehicle can be mutually fixed by the aid of the two elastic movable sliding seats and the two telescopic insertion rods, so that the wing seat and the wing support of the unmanned aerial vehicle can be fixed by the aid of the two elastic movable sliding seats and the two telescopic insertion rods; the wing seat and the wing support of the unmanned aerial vehicle are assembled in an inserting mode to form the unmanned aerial vehicle, the assembling efficiency of the whole wing seat structure of the unmanned aerial vehicle is improved, installation of the wing support is reinforced through a rubber rotating block, a positioning block and a displacement clamping plate, the stability of the wing seat structure of the unmanned aerial vehicle during installation of the wing support is ensured, and the safety of the unmanned aerial vehicle is improved. And meanwhile, the wing support can be quickly replaced, and the quick release effect is achieved.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned aerial vehicle wing seat technical field, concretely is a kind of unmanned aerial vehicle wing seat structure. BACKGROUND

[0002] Unmanned aerial vehicle as air platform, with flexible, easy to use, stable, low cost and other characteristics;Different equipment can be carried to realize corresponding function, complete a specific operation target, application range is very extensive, and unmanned aerial vehicle wing seat structure is often used to fix wing, to form unmanned aerial vehicle by assembly.

[0003] Prior art discloses patent application number "CN202320616987.4", a mounting seat for unmanned aerial vehicle rotor, it includes that bottom base body middle part is equipped with circular through-hole, through-hole inner wall is provided with one fixed platform around, the fixed platform is equipped with threaded hole towards through-hole center, cross mounting frame is connected with each fixed platform respectively, cross mounting frame middle part upper side is provided with rotor mounting base, rotor mounting base middle part is equipped with through-hole, bearing is installed in through-hole, the upper end surface of rotor mounting base is circular array with fastening bolt with through-hole center as center point. Rotor base is born in an emergency, as the external device of supporting rotor unmanned aerial vehicle, provides stable flight environment and control function for it.

[0004] The mounting seat of the unmanned aerial vehicle rotor can only provide stable flight environment and control function, but in actual use, since unmanned aerial vehicle wing seat and wing are mostly integrally formed or fixed by bolt, the two cannot be conveniently disassembled for maintenance work, and the assembly efficiency of unmanned aerial vehicle is also affected. UTILITY MODEL CONTENT

[0005] The utility model aims at providing a kind of unmanned aerial vehicle wing seat structure to solve the problems raised in the above background.

[0006] The utility model can be realized by the following technical solutions:

[0007] A kind of unmanned aerial vehicle wing seat structure, including unmanned aerial vehicle wing seat main body, the upper side of unmanned aerial vehicle wing seat main body is fixedly connected with circular ring, the upper side of unmanned aerial vehicle wing seat main body is equipped with two installation holes, the inside of circular ring is fixedly provided with wing support, the both ends of wing support are slidably connected with two movable sliding seat for fixing wing support;

[0008] First springs are arranged and connected between the two movable sliding seats and the wing support, the inside of the ring is slidably connected with two telescopic inserting rods for fixing the wing support, second springs are fixedly installed between the two telescopic inserting rods and the ring, rubber round pads are arranged and fixed on the outer surfaces of the two telescopic inserting rods, one side of the telescopic inserting rod penetrates through the ring and extends to the other side of the ring, and a circular plate is fixedly installed on one side of each of the two telescopic inserting rods.

[0009] Preferably, two clamping grooves are formed in the two sides of the wing support, and two rubber swivels are rotatably connected to the upper side of the ring and located in the clamping grooves.

[0010] Preferably, two elastic connecting pieces are symmetrically fixed on the upper side of the unmanned aerial wing seat body, positioning blocks are fixedly connected to the upper sides of the two elastic connecting pieces, recesses are formed in the sides of the two movable sliding seats, and the positioning blocks are located in the recesses.

[0011] Preferably, adaptive grooves are formed in the two ends of the ring, the adaptive grooves are matched with the movable sliding seats, and the sides of the movable sliding seats are slidably connected with the two ends of the ring through the adaptive grooves.

[0012] Preferably, two fixing blocks are symmetrically fixed on the upper side of the unmanned aerial wing seat body, circular grooves are formed in the upper sides of the two fixing blocks, two mounting blocks are symmetrically fixed on the upper side of the unmanned aerial wing seat body, a bottom plate is fixedly connected to the lower side of the wing support, two displacement clamping plates for fixing the bottom plate are slidably connected in the unmanned aerial wing seat body, buckle grooves are formed in the lower sides of the two displacement clamping plates, and the inner sides of the displacement clamping plates penetrate through the bottom plate and extend into the bottom plate.

[0013] Preferably, positioning grooves are formed in the two sides of the wing support, the positioning grooves are matched with the telescopic inserting rods, and the inner sides of the telescopic inserting rods are clamped with the two sides of the wing support through the positioning grooves.

[0014] The unmanned aerial wing seat and the wing support can be fixed to each other through the two movable sliding seats and the two telescopic inserting rods, the unmanned aerial wing seat and the wing support are assembled in the form of insertion, the assembly efficiency of the unmanned aerial wing seat structure is improved, and the unmanned aerial wing seat and the wing support can be conveniently disassembled for maintenance work.

[0015] 1、The two movable sliding seats and the two telescopic inserting rods are used to fix the unmanned aerial wing seat and the wing support, the unmanned aerial wing seat and the wing support are assembled in the form of insertion, the assembly efficiency of the unmanned aerial wing seat structure is improved, and the unmanned aerial wing seat and the wing support can be conveniently disassembled for maintenance work.

[0016] 2、The rubber swivel, the positioning block and the displacement clamping plate are used to reinforce the installation of the wing support, the stability of the unmanned aerial wing seat structure when the wing support is installed is ensured, bolts are not needed for fixing, the wing support can be quickly replaced, and the quick disassembly effect is achieved, time and labor are saved. DRAWINGS

[0017] In order to more clearly illustrate the technical schemes in the embodiments of the present application or the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly introduced as follows. Obviously, for those skilled in the art, other drawings can be obtained from these drawings without any creative effort.

[0018] Figure 1 is a schematic diagram of the overall structure of the present application;

[0019] Figure 2 is a schematic diagram of the installation of the movable sliding seat and the first spring in the present application Figure 1 ;

[0020] Figure 3 is a schematic diagram of the structure of the elastic connecting piece and the positioning block in the present application Figure 2 ;

[0021] Figure 4 is an enlarged view of position A in the present application Figure 3 ;

[0022] Figure 5 is a schematic diagram of the structure of the displacement clamping plate and the buckle groove in the present application Figure 1 ;

[0023] Figure 6 is a schematic diagram of the structure of the wing support and the positioning groove in the present application Figure 1 ;

[0024] The reference signs in the drawings are as follows:

[0025] 1, unmanned wing seat main body; 2, mounting hole; 3, wing support; 4, movable sliding seat; 5, first spring; 6, fixed block; 7, round groove; 8, telescopic insertion rod; 9, second spring; 10, round plate; 11, rubber round pad; 12, circular ring; 13, mounting block; 14, rubber rotating block; 15, elastic connecting piece; 16, positioning block; 17, groove; 18, clamping groove; 19, bottom plate; 20, displacement clamping plate; 21, buckle groove; 100, adaptive groove; 200, positioning groove. DETAILED DESCRIPTION

[0026] The technical schemes in the embodiments of the present application will be described clearly and completely in combination with the drawings in the embodiments of the present application. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without any creative effort fall within the protection scope of the present application.

[0027] For example, Figures 1 to 6As shown, a kind of unmanned aircraft wing seat structure, including unmanned aircraft wing seat body 1, the upper side of unmanned aircraft wing seat body 1 is fixedly connected with circular ring 12, the upper side of unmanned aircraft wing seat body 1 is equipped with two mounting holes 2, the inside of circular ring 12 is fixedly provided with wing support 3, the both ends of wing support 3 are slidably connected with two movable sliding seat 4 for fixing wing support 3, just press two movable sliding seat 4 simultaneously, so as to retract two movable sliding seat 4 into wing support 3, for taking out wing support 3, convenient to use;

[0028] First spring 5 is arrayed and connected between two movable sliding seat 4 and wing support 3, two telescopic inserting rods 8 for fixing wing support 3 are slidably connected in the inside of circular ring 12, second spring 9 is fixedly installed between two telescopic inserting rods 8 and circular ring 12, arrayed rubber round pad 11 is fixedly connected on the outer surface of two telescopic inserting rods 8, one side of telescopic inserting rod 8 penetrates through circular ring 12 and extends to the other side of circular ring 12, circular plate 10 is fixedly installed on the side of two telescopic inserting rods 8, through the setting of circular plate 10, telescopic inserting rod 8 with elasticity can be moved by circular plate 10, so that telescopic inserting rod 8 is retracted into the inside of circular ring 12, so that rubber round pad 11 at telescopic inserting rod 8 can drive telescopic inserting rod 8 to be stored in position, to remove wing support 3 from circular ring 12.

[0029] Two clamping grooves 18 are formed on the both sides of wing support 3, two rubber swivel blocks 14 are rotatably connected on the upper side of circular ring 12, and the rubber swivel blocks 14 are located in the clamping grooves 18.

[0030] Two elastic connecting pieces 15 are fixedly installed on the upper side of unmanned aircraft wing seat body 1, the upper side of two elastic connecting pieces 15 is fixedly connected with positioning block 16, recess 17 is formed on the side of two movable sliding seat 4, and positioning block 16 is located in recess 17.

[0031] Two adaptive grooves 100 are formed on the both ends of circular ring 12, the adaptive grooves 100 are matched with movable sliding seat 4, and the side of movable sliding seat 4 is slidably connected with the both ends of circular ring 12 through adaptive grooves 100.

[0032] Two fixed blocks 6 are fixedly installed on the upper side of unmanned aircraft wing seat body 1, circular groove 7 is formed on the upper side of two fixed blocks 6, two mounting blocks 13 are fixedly connected on the upper side of unmanned aircraft wing seat body 1, bottom plate 19 is fixedly connected on the lower side of wing support 3, two displacement clamping plates 20 for fixing bottom plate 19 are slidably connected in the inside of unmanned aircraft wing seat body 1, buckle groove 21 is formed on the lower side of two displacement clamping plates 20, through the setting of buckle groove 21, displacement clamping plate 20 can be moved back and forth by buckle groove 21, so as to assemble and disassemble wing support 3, and the inside of displacement clamping plate 20 penetrates through bottom plate 19 and extends to the inside of bottom plate 19.

[0033] The positioning groove 200 is matched with the telescopic inserting rod 8, and the inner side of the telescopic inserting rod 8 is clamped with the two sides of the wing support 3 through the positioning groove 200.

[0034] The working principle of the unmanned aerial wing seat structure is as follows:

[0035] When the wing support 3 is installed in place, the two movable sliding seats 4 with elasticity are automatically elongated and clamped in the adaptive groove 100 of the circular ring 12, then the two circular plates 10 are moved respectively, so as to drive the two telescopic inserting rods 8 provided with the second spring 9 to be clamped in the positioning groove 200 of the wing support 3, and the unmanned aerial wing seat body 1 and the wing support 3 are assembled in the form of insertion, so as to form an unmanned aerial vehicle, improve the assembly efficiency of the whole unmanned aerial wing seat structure, and conveniently disassemble the two for maintenance work.

[0036] The two rubber rotating blocks 14 are clamped in the two clamping grooves 18 for positioning the wing support 3, then the two displacement clamping plates 20 are moved towards each other and inserted into the inside of the bottom plate 19, so as to further clamp and fix the wing support 3, then the two positioning blocks 16 provided with the elastic connecting plates 15 are clamped in the grooves 17 of the two movable sliding seats 4, so as to limit and fix the two movable sliding seats 4, ensure the stability of the unmanned aerial wing seat structure when the wing support 3 is installed, do not need to use bolts for fixing, and can quickly replace the wing support 3, realize quick disassembly, save time and effort.

[0037] The basic principle, main features and advantages of the utility model are shown and described above. It should be understood by those skilled in the art that the utility model is not limited by the above embodiments, and the above embodiments and descriptions in the specification are only to illustrate the principle of the utility model, and various changes and improvements can be made without departing from the spirit and scope of the utility model, and these changes and improvements all fall within the scope of the utility model claimed.

Claims

1. An unmanned wing seat structure comprising an unmanned wing seat body (1), characterized in that: The upper side of the unmanned aircraft wing seat body (1) is fixedly connected with a circular ring (12), two mounting holes (2) are formed in the upper side of the unmanned aircraft wing seat body (1), the inside of the circular ring (12) is fixedly provided with a wing support (3), and the two ends of the wing support (3) are slidably connected with two movable sliding seats (4) for fixing the wing support (3). First springs (5) are arranged and connected between the two movable sliding seats (4) and the wing support (3), two telescopic inserting rods (8) for fixing the wing support (3) are slidably connected in the inside of the circular ring (12), second springs (9) are fixedly installed between the two telescopic inserting rods (8) and the circular ring (12), rubber round pads (11) are fixedly connected in an array on the outer surfaces of the two telescopic inserting rods (8), one side of each of the two telescopic inserting rods (8) penetrates through the circular ring (12) and extends to the other side of the circular ring (12), and a circular plate (10) is fixedly installed on one side of each of the two telescopic inserting rods (8).

2. The winged drone airframe structure of claim 1, wherein, Two clamping grooves (18) are formed in the two sides of the wing support (3), and two rubber rotating blocks (14) are rotatably connected to the upper side of the circular ring (12) and located in the clamping grooves (18).

3. The unmanned wingbed structure of claim 1, wherein, Two symmetrically arranged elastic connecting pieces (15) are fixedly installed on the upper side of the unmanned aircraft wing seat body (1), a positioning block (16) is fixedly connected to the upper side of each of the two elastic connecting pieces (15), and a recess (17) is formed in one side of each of the two movable sliding seats (4), with the positioning block (16) located in the recess (17).

4. The unmanned wingbed structure of claim 1, wherein, Two adaptive grooves (100) are formed in the two ends of the circular ring (12), the adaptive grooves (100) are adapted to the movable sliding seats (4), and one side of each of the movable sliding seats (4) is slidably clamped to the two ends of the circular ring (12) through the adaptive grooves (100).

5. The unmanned wingbed structure of claim 1, wherein, Two symmetrically arranged fixing blocks (6) are fixedly installed on the upper side of the unmanned aircraft wing seat body (1), a circular groove (7) is formed in the upper side of each of the two fixing blocks (6), two symmetrically arranged mounting blocks (13) are fixedly connected to the upper side of the unmanned aircraft wing seat body (1), a bottom plate (19) is fixedly connected to the lower side of the wing support (3), two displacement clamping plates (20) for fixing the bottom plate (19) are slidably clamped in the inside of the unmanned aircraft wing seat body (1), a buckle groove (21) is formed in the lower side of each of the two displacement clamping plates (20), and the inner side of each of the displacement clamping plates (20) penetrates through the bottom plate (19) and extends into the inside of the bottom plate (19).

6. The unmanned wingbed structure of claim 1, wherein, Two positioning grooves (200) are formed in the two sides of the wing support (3), the positioning grooves (200) are adapted to the telescopic inserting rods (8), and the inner sides of the telescopic inserting rods (8) are clamped to the two sides of the wing support (3) through the positioning grooves (200).

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