CN210822795U - Connecting device for fast mounting and dismounting rotor unmanned aerial vehicle and manipulator - Google Patents

Abstract

The utility model discloses a connecting device that is used for rotor unmanned aerial vehicle and quick installation of manipulator to dismantle, install the dismounting device fast and constitute by connecting rod, the transition base structure spare of being connected with unmanned aerial vehicle, return hook shape structure spare, the structure of taking the splayed spout, the transition base structure spare of being connected with the manipulator, bolt, square hole spare, spring, screw. The utility model discloses following beneficial effect has: the quick installation that can realize manipulator and unmanned aerial vehicle two bodies is designed, and the installation step is few, dismantle simple swiftly to guarantee flight in-process safe and reliable, have important meaning to flying manipulator.

Description

Connecting device for fast mounting and dismounting rotor unmanned aerial vehicle and manipulator

Technical Field

The utility model belongs to the aircraft field, concretely relates to a connecting device that is used for rotor unmanned aerial vehicle and quick installation of manipulator to dismantle.

Background

The current installation of the flight manipulator mainly adopts a bolt connection mode. Namely, the manipulator and the unmanned aerial vehicle base are connected together in a matching way through bolts and nuts. The bolt connection security is higher, and is fixed easily, but the dismouting is got up comparatively trouble, and two holes need align when assembling, especially when the flight receives that junction space is narrow and small, and the dismouting is very inconvenient. In addition, the bolts are frequently disassembled, so that the threaded holes are easily damaged, and further the bolt connection is possibly loosened under the action of long-term dynamic load, so that hidden danger is brought to flight.

Disclosure of Invention

The utility model provides a connecting device that is used for rotor unmanned aerial vehicle and quick installation of manipulator to dismantle aims at solving the technical problem that the aforesaid exists.

The utility model adopts the following technical scheme:

the utility model provides a connecting device that is used for rotor unmanned aerial vehicle and quick installation of manipulator to dismantle, its characterized in that: the quick mounting and dismounting device consists of a connecting rod 1, a transition base structural part 2 connected with the unmanned aerial vehicle, a return hook-shaped structural part 3, a structural part 4 with a splayed sliding chute, a transition base structural part 5 connected with the manipulator, a long bolt 6.1, a short bolt 6.2, a square hole part 7, a spring 8 and a screw 9,

the long bolt 6.1 passes square hole spare 7 and connects connecting rod 1, connecting rod 1 connects back hook shape structure 3 through short bolt 6.2, square hole spare 7 is fixed with spring 8, can slide on taking the structure 4 of splayed spout, take structure 4 of splayed spout to pass through screw 9 and the transition base structure 5 of being connected with the manipulator fixed, back hook shape structure 3 can be dismantled with the transition base structure 2 of being connected with unmanned aerial vehicle and be connected.

Further, the connecting rod is provided with a main body 1.3, one end of the main body 1.3 is a single lug piece 1.1 with a circular through hole, and the other end of the main body 1.3 is a double lug piece 1.2 with a circular through hole.

Furthermore, the upper part of a transition base structural part 2 connected with the unmanned aerial vehicle is a flat plate 2.1 which is mainly used for being connected with the unmanned aerial vehicle; the lower part is mainly a hollow cuboid tubular structure, two first through holes 2.2 and two second through holes 2.3 are respectively arranged on two sides, the first through holes 2.2 are arranged above the second through holes 2.3, and a cutting groove 2.4 is arranged in the front.

Further, the hook-back structural member 3 mainly comprises a circular through hole 3.1 and a ditch-like structure 3.2.

Furthermore, the main structure of the structural member 4 with the splayed sliding groove is a plate-shaped structure, a rectangular through hole 4.1, a splayed through hole 4.2 and a circular through hole 4.3 are formed in the plate, and the splayed through hole 4.2 can realize the up-and-down and left-and-right movement of the sliding block.

Further, the transition base structural member 5 connected with the manipulator mainly comprises two double-lug pieces 5.2 with circular through holes and a seat groove 5.1, wherein the seat groove is used for installing and positioning the structural member 4, and the double-lug pieces 5.2 are used for being fastened and connected with the structural member 4 and the structural member 5 through screws with the two circular through holes of the structural member 4.

The utility model discloses following beneficial effect has: the quick installation that can realize manipulator and unmanned aerial vehicle two bodies is designed, and the installation step is few, dismantle simple swiftly to guarantee flight in-process safe and reliable, have important meaning to flying manipulator.

Drawings

FIG. 1(a) is an exploded view;

FIG. 1(b) is an overall assembly view;

FIG. 1(c) is an overall assembly view;

fig. 2 is a connecting rod 1;

fig. 3(a) is a transition base structure connected to an unmanned aerial vehicle;

fig. 3(b) is a transition base structure connected to the drone;

FIG. 4 is a clip-shaped structure;

FIG. 5 shows a structural member with splayed sliding grooves

FIG. 6 shows a transition base structure connected to a robot

FIG. 7 shows a subassembly II

FIG. 8 shows a sub-assembly III

FIG. 9 shows a lower assembly IV

In the figure, the connecting rod 1, the single lug piece 1.2, the double lug piece 1.2, the main body 1.3, a transition base structural part 2 connected with the unmanned aerial vehicle, a flat plate 2.1, a first through hole 2.2, a second through hole 2.3, a cutting groove 2.4, a back hook-shaped structural part 3, a circular through hole 3.1, a back ditch-shaped structure 3.2, a structural part 4 with a splayed sliding groove, a rectangular through hole 4.1, a splayed through hole 4.2, a circular through hole 4.3, a transition base structural part 5 connected with a manipulator, a seat groove 5.1, the double lug piece 5.2, a long bolt 6.1, a short bolt 6.2, a square hole part 7, a spring 8 and a screw 9.

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.

In the description of the present invention, it is to be understood that the terms "center", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "axial", "circumferential", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

In the present invention, unless otherwise expressly stated or limited, the terms "disposed," "mounted," "connected," and "fixed" are to be construed broadly, e.g., as meaning either a fixed connection or a removable connection; may be a mechanical connection; may be directly connected or indirectly connected through an intermediate. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature.

As shown in fig. 1(a), the utility model provides a connecting device that is used for rotor unmanned aerial vehicle and quick installation of manipulator to dismantle, install the dismounting device fast and constitute by connecting rod 1, the transition base structure 2 of being connected with unmanned aerial vehicle, return hook shape structure 3, take the structure 4 of splayed spout, the transition base structure 5 of being connected with the manipulator, long bolt 6.1, short bolt 6.2, square hole spare 7, spring 8, screw 9.

As shown in fig. 2, the connecting rod 1 of the present invention has a main body 1.3, one end of the main body 1.3 is a single lug piece 1.1 with a circular through hole, and the other end is a double lug piece 1.2 with a circular through hole.

As shown in fig. 3(a), the upper part of the transition base structural member 2 connected with the unmanned aerial vehicle of the present invention is a flat plate 2.1, which is mainly used for connecting with the unmanned aerial vehicle; the lower part is mainly a hollow cuboid tubular structure, two through holes 2.2 and 2.3 are respectively arranged at two sides, and a cutting groove 2.4 is arranged at the front.

As shown in fig. 4, the hook-shaped structure 3 of the present invention mainly includes a circular through hole 3.1 and a return groove-shaped structure 3.2.

As shown in fig. 5, the utility model discloses take 4 major structures of structure of splayed spout to be a board type structure, have rectangle through-hole 4.1, splayed through-hole 4.2, circular through-hole 4.3 on the board, wherein splayed through-hole 4.2 can realize the up-and-down and side-to-side movement of slider.

As shown in fig. 6, the transition base structure 5 connected to the manipulator in the present invention mainly includes two double-lug pieces 5.2 with circular through holes and a seat groove 5.1, wherein the seat groove is used for installing and positioning the structure 4, and the double-lug pieces 5.2 are used for fastening the structure 4 and the structure 5 with two circular through holes of the structure 4 through screws.

The assembly process is divided into the following steps:

assembly of sub-assembly I: the sub-assembly body I is mainly formed by matching a structural part 4 with a splayed sliding groove, a square block 7, a spring 8 and a long bolt 6.1. Sub-assembly I is part of fig. 8 and 9.

As shown in fig. 7, the utility model discloses neutron assembly body II is accomplished by connecting rod 1, the cooperation of returning hook shape slider structure 2, as shown in fig. 7, wherein connecting rod 1 and returning hook shape slider structure 3 are through two auricles 1.2 and circular through-hole 3.1, use short bolt 6.2 to accomplish to be connected, but connecting rod 1 and returning hook shape slider structure 3 automatic relative rotation, or can not automatic relative rotation, need artificial mode manual rotation to return hook shape slider structure 3.

As shown in fig. 8, the present invention combines sub-assembly I with sub-assembly II to obtain sub-assembly III, wherein 1 is used to realize the combination of sub-assembly I and sub-assembly II with long bolt 6.1.

As shown in fig. 9, the sub-assembly III is locked and engaged with the transition base structural member 5 by screws 9, so as to obtain a lower half assembly IV.

And finally, a transition base connected with the unmanned aerial vehicle is matched with a lower half assembly body IV, and locking devices are arranged on two sides of the mechanism.

Description of the working principle of the flying manipulator quick assembling and disassembling device:

connecting action: connect unmanned aerial vehicle and manipulator only need earlier both through transition base structure 2, 5 cooperate earlier, push down spring 8 again, drive connecting rod 1 motion and make and return hook-shaped structure 3 along splayed through-hole 4.2 (splayed spout) stretch out and be connected the first through-hole 2.2 (notch) of transition base structure 2 both sides with unmanned aerial vehicle, manual promotion accomplishes the cooperation with transition base structure 2 that unmanned aerial vehicle is connected, then loosen spring 8, utilize the reply elasticity of spring to make connecting rod 1 rise back and return hook-shaped structure 3 card simultaneously and go into in second through-hole 3.2 (safety notch), above action alright realize the latter half assembly body IV and be connected with the straining of structure 2, and then accomplish being connected of unmanned aerial vehicle and manipulator two parts.

And (3) decomposition action: only need push down spring 8 once more, two upper and lower transition base cooperations are reset simultaneously and are made the return hook shape structure 3 break away from and are connected the first through-hole 2.2 and the second through-hole 3.2 notch of transition base structure 1 both sides with unmanned aerial vehicle, just can kick-back through spring 8 and drive connecting rod 1 and rise and return hook shape structure 3 along with splayed through-hole 4.2 (splayed spout) withdrawal simultaneously, above action just with the separation of the assembly body IV of the latter half and structure 2, and then realize the separation of unmanned aerial vehicle and manipulator.

The above description is only for the specific embodiments of the present invention, but the protection scope of the present invention is not limited thereto, and any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope of the present invention should be covered by the protection scope of the present invention. Therefore, the protection scope of the present invention shall be subject to the protection scope of the claims.

Claims (6)

1. The utility model provides a connecting device that is used for rotor unmanned aerial vehicle and quick installation of manipulator to dismantle, its characterized in that: the quick mounting and dismounting device consists of a connecting rod (1), a transition base structural part (2) connected with the unmanned aerial vehicle, a return hook-shaped structural part (3), a structural part (4) with a splayed sliding chute, a transition base structural part (5) connected with the manipulator, a long bolt (6.1), a short bolt (6.2), a square hole part (7), a spring (8) and a screw (9),

the long bolt (6.1) passes square hole spare (7) and connects connecting rod (1), return hook shape structure (3) are connected through short bolt (6.2) in connecting rod (1), square hole spare (7) are fixed with spring (8), can slide on structure (4) in area splayed spout, structure (4) in area splayed spout are fixed with transition base structure (5) of being connected with the manipulator through screw (9), return hook shape structure (3) can dismantle with transition base structure (2) that unmanned aerial vehicle is connected and be connected.

2. A device for the rapid attachment and detachment of a rotorcraft to and from a robot, according to claim 1, wherein: the connecting rod is provided with a main body (1.3), one end of the main body (1.3) is a single lug piece (1.1) with a circular through hole, and the other end of the main body is a double lug piece (1.2) with a circular through hole.

3. A device for the rapid attachment and detachment of a rotorcraft to and from a robot, according to claim 1, wherein: the upper part of a transition base structural part (2) connected with the unmanned aerial vehicle is provided with a flat plate (2.1) which is mainly used for being connected with the unmanned aerial vehicle; the lower part of the hollow cuboid tube-shaped structure is mainly hollow, two first through holes (2.2) and two second through holes (2.3) are respectively arranged on two sides of the hollow cuboid tube-shaped structure, the first through holes (2.2) are arranged above the second through holes (2.3), and the front surfaces of the first through holes are provided with cutting grooves (2.4).

4. A device for the rapid attachment and detachment of a rotorcraft to and from a robot, according to claim 1, wherein: the hook-shaped structural part (3) mainly comprises a circular through hole (3.1) and a ditch-shaped structure (3.2).

5. A device for the rapid attachment and detachment of a rotorcraft to and from a robot, according to claim 1, wherein: the main structure of the structural member (4) with the splayed sliding groove is a plate structure, a rectangular through hole (4.1), a splayed through hole (4.2) and a circular through hole (4.3) are formed in the plate, and the splayed through hole (4.2) can realize the up-and-down and left-and-right movement of the sliding block.

6. A device for the rapid attachment and detachment of a rotorcraft to and from a robot, according to claim 1, wherein: the transition base structural part (5) connected with the manipulator mainly comprises two double lug plates (5.2) with circular through holes and a seat groove (5.1), wherein the seat groove is used for installing and positioning the structural part (4) with the splayed sliding groove, and the double lug plates (5.2) are used for realizing the fastening connection of the structural part (4) with the splayed sliding groove and the transition base structural part (5) connected with the manipulator through two circular through holes of the structural part (4) with the splayed sliding groove by screws.

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