Quick-release pipe clamp for unmanned aerial vehicle arm carbon pipe

Abstract

The utility model discloses an unmanned aerial vehicle arm carbon tube quick-release pipe clamp which is used for connecting an unmanned aerial vehicle arm carbon tube and a main beam and comprises a quick-release pipe clamp body, the quick-release pipe clamp body comprises a connecting pipe and a carbon tube clamping pipe, outer threads are arranged on the outer walls of the opposite parts of the connecting pipe and the carbon tube clamping pipe, and the outer threads are connected with the connecting pipe. When the connecting pipe and the carbon pipe clamping pipe are in butt joint, the outer threads of the connecting pipe and the outer threads of the carbon pipe clamping pipe are connected, the outer portions of the opposite parts of the connecting pipe and the carbon pipe clamping pipe are jointly connected with an inner thread locking sleeve in a threaded mode, the inner thread locking sleeve can rotate to the tail end of the carbon pipe clamping pipe along the carbon pipe clamping pipe, and the end of the arm carbon pipe is inserted into the carbon pipe clamping pipe. An end plate is fixed to the end, opposite to the main beam, of the connecting pipe, and a threading hole is formed in the end plate. According to the quick-release pipe clamp for the carbon pipe, the carbon pipe can be separated from the main beam, and the carbon pipe is perpendicular to the main beam, namely, the carbon pipe is vertically downward, so that under the condition that the number of arms is large, the arms are stored in the height space of the unmanned aerial vehicle, and the plane area of the unmanned aerial vehicle is reduced.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane technical field, concretely is a kind of unmanned plane arm carbon pipe quick-release pipe clamp. BACKGROUND

[0002] For the unmanned plane with loading, carrying capacity, its body size is larger, and it occupies a certain space every time it is placed, transported, etc., the existing unmanned plane, the arm is directly detached as a whole, and is placed separately after being detached, some of the arms can be folded on the unmanned plane, and the folded arms are located outside the main beam of the unmanned plane body, without being placed separately, and in order to achieve lightweight, two-thirds of the length of the arm is made of carbon material, which is a carbon pipe. The carbon pipe needs to be connected to the one-third part of the arm using a pipe clamp. However, the pipe clamp cannot be removed from the carbon pipe. For such unmanned planes, the number of arms is large, and even if the arms are folded twice, they cannot be folded on the outside of the main beam.

[0003] Therefore, in order to correct the above-mentioned defects, we propose a quick-release pipe clamp for the arms of an unmanned plane. CONTENT OF THE UTILITY MODEL

[0004] The utility model solves the technical problem of providing a quick-release pipe clamp for the arms of an unmanned plane.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical scheme: a quick-release pipe clamp for the arms of an unmanned plane, which is used to connect the carbon pipe of the arm of the unmanned plane and the main beam, and includes a quick-release pipe clamp body. The quick-release pipe clamp body includes a connecting pipe and a carbon pipe clamping pipe. The outer walls of the opposite parts of the connecting pipe and the carbon pipe clamping pipe are provided with external threads. When the connecting pipe and the carbon pipe clamping pipe are connected, the external threads of the two are connected. An internally threaded locking sleeve is connected to the outer part of the opposite parts of the connecting pipe and the carbon pipe clamping pipe. The internally threaded locking sleeve can be rotated to the end of the carbon pipe clamping pipe. The end of the arm carbon pipe is inserted into the carbon pipe clamping pipe. One end of the connecting pipe opposite the main beam is fixed with an end plate. The end plate is provided with a threading hole.

[0006] Further, a screw hole is formed in the outer wall of the carbon pipe clamping pipe. When the end of the arm carbon pipe is inserted into the carbon pipe clamping pipe, a screw is screwed into the screw hole.

[0007] Further, two opposite contraction joints are formed in the outer wall of the carbon pipe clamping pipe from the end to the other end, and a locking hoop is movably sleeved on the outside of the end of the carbon pipe clamping pipe. The two ends of the locking hoop are locked by a screw.

[0008] Further, a positioning hoop is sleeved on the outside of the part of the connecting pipe close to the end plate. The positioning hoop is used to limit the over-forward movement of the internally threaded locking sleeve on the connecting pipe. The two ends of the positioning hoop are provided with threaded holes, and the two ends are locked by a threaded rod and a nut.

[0009] Further, the positioning hoop has a sleeve between two end heads, a threaded rod passes through the sleeve, the outer wall of the sleeve is connected with a special-shaped arm, the special-shaped arm is connected with a straight arm, the straight arm is connected with the carbon tube clamping pipe, the positioning hoop, the sleeve, the straight arm and the threaded rod cooperatively form a hinge, and the hinge is connected between the carbon tube clamping pipe and the adapter pipe.

[0010] Further, the bottom of the adapter pipe is provided with a containing groove, the containing groove is used for containing the straight arm, the straight arm is connected with the end of the carbon tube clamping pipe, when the internal thread locking sleeve locks the adapter pipe and the carbon tube clamping pipe, the straight arm is in the containing groove, the special-shaped arm is in a vertical state and is in an S shape, and the special-shaped arm is close to the positioning hoop and does not hinder the internal thread locking sleeve.

[0011] Further, the bottom of the straight arm is in an arc shape, and the containing groove is also in an arc shape, so that the straight arm fills the adapter pipe to be complete when the straight arm is contained in the containing groove.

[0012] Further, the bottom of the straight arm is also provided with an external thread, and the external thread of the straight arm is connected with the external thread of the adapter pipe.

[0013] Further, the inside of the adapter pipe and the carbon tube clamping pipe is provided with a partition plate, so that the inner cavities of the adapter pipe and the carbon tube clamping pipe are divided into two parts.

[0014] Compared with the prior art, the beneficial effects of the utility model are that the carbon tube quick release pipe clamp can separate the carbon tube from the main beam, and make the carbon tube and the main beam form perpendicular to each other, that is, make the carbon tube vertically downward, so that the height space of the unmanned aerial vehicle is used to store the machine arm under the condition that the number of machine arms is large, and the plane area of the unmanned aerial vehicle is reduced. BRIEF DESCRIPTION OF DRAWINGS

[0015] Figure 1 It is a structure schematic view of the quick release pipe clamp installed on the unmanned aerial vehicle arm.

[0016] Figure 2 It is a structure schematic view of the quick release pipe clamp.

[0017] Figure 3 It is a plane structure schematic view of the quick release pipe clamp.

[0018] Figure 4 It is a bending structure schematic view of the quick release pipe clamp.

[0019] Figure 5 It is a side view structure schematic view of the adapter pipe.

[0020] Figure 6 It is a side view structure schematic view of the carbon tube clamping pipe.

[0021] Mark in the figure:

[0022] 100, quick release pipe clamp body; 101, adapter pipe; 102, end plate; 103, external thread; 104, carbon pipe clamping pipe; 105, internal thread locking sleeve; 106, screw hole; 107, locking hoop; 108, shrink joint; 109, positioning hoop; 111, threaded rod; 112, special-shaped arm; 113, straight arm; 114, containing groove; 115, partition plate. DETAILED DESCRIPTION

[0023] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. 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 those skilled in the art without creative labor fall within the scope of protection of the utility model.

[0024] The utility model provides a technical scheme:

[0025] Please refer to Figures 1-6 A quick release pipe clamp for unmanned aerial vehicle arm carbon pipe and main beam (also the front aluminum alloy part of the whole arm), comprising a quick release pipe clamp body 100, the quick release pipe clamp body 100 comprises an adapter pipe 101 and a carbon pipe clamping pipe 104, the outer wall of the opposite part of the adapter pipe 101 and the carbon pipe clamping pipe 104 is provided with external thread 103, and when the adapter pipe 101 and the carbon pipe clamping pipe 104 are connected, the external thread 103 of the two is connected, the external thread of the opposite part of the adapter pipe 101 and the carbon pipe clamping pipe 104 is connected with the internal thread locking sleeve 105, the internal thread locking sleeve 105 can be rotated to the end of the carbon pipe clamping pipe 104, that is, the adapter pipe 101 and the carbon pipe clamping pipe 104 are separated and combined by rotating the internal thread locking sleeve 105, the end of the arm carbon pipe is inserted into the carbon pipe clamping pipe 104, one end of the adapter pipe 101 relative to the main beam is fixed with an end plate 102, a threading hole is formed in the end plate 102, and the power supply line of the arm end propeller is inserted into the quick release pipe clamp body 100 from the end plate 102.

[0026] Through the above, when the unmanned aerial vehicle does not work, the adapter pipe 101 and the carbon pipe clamping pipe 104 are separated by rotating the internal thread locking sleeve 105, that is, the arm is disassembled from the main beam of the unmanned aerial vehicle, if the arm is divided into an aluminum alloy front part and a carbon pipe, the carbon pipe is disassembled from the aluminum alloy front part, and the whole arm is divided into two parts.

[0027] In order to remove the carbon tube from the quick release tube clamp body 100, a screw hole 106 is formed on the outer wall of the carbon tube clamp tube 104, and when the end of the carbon tube is inserted into the carbon tube clamp tube 104, the screw is screwed into the screw hole 106. The outer wall of the carbon tube clamp tube 104 is provided with two opposite shrinkage seams 108 from the end to the other end, and the end of the carbon tube clamp tube 104 is externally sleeved with a locking hoop 107. The two ends of the locking hoop 107 are locked by a screw, that is, the carbon tube clamp tube 104 and the carbon tube are movably inserted and connected. After insertion, the screw and the carbon tube clamp tube 104 are locked. When the carbon tube needs to be removed, the carbon tube clamp tube 104 and the screw only need to be loosened.

[0028] The outer part of the part of the adapter tube 101 close to the end plate 102 is sleeved with a positioning hoop 109, which is used to limit the excessive forward movement of the internally threaded locking sleeve 105 on the adapter tube 101. The two ends of the positioning hoop 109 are provided with threaded holes, and the two ends are locked by a threaded rod 111 and a nut. The positioning hoop 109 limits the maximum movement range of the internally threaded locking sleeve 105 on the adapter tube 101, preventing the internally threaded locking sleeve 105 from being separated from the carbon tube clamp tube 104.

[0029] Based on the above, although the carbon tube can be removed, it will be separated from the unmanned aerial vehicle body, that is, it needs to be placed separately. Therefore, the two ends of the positioning hoop 109 have a sleeve 116, the threaded rod 111 passes through the sleeve 116, the outer wall of the sleeve 116 is connected with a special-shaped arm 112, the special-shaped arm 112 is connected with a straight arm 113, the straight arm 113 is connected with the carbon tube clamp tube 104, and the positioning hoop 109, the sleeve 116, the straight arm 113 and the threaded rod 111 form a hinge. The hinge is connected between the carbon tube clamp tube 104 and the adapter tube 101, that is, the carbon tube can be hung, and since the unmanned aerial vehicle has a supporting part, it has a certain height, and the height space is used to accommodate the carbon tube.

[0030] In order to prevent the above-mentioned hinge structure from hindering the internally threaded locking sleeve 105, the bottom of the adapter tube 101 is provided with an accommodation groove 114, which is used to accommodate the straight arm 113. The end of the straight arm 113 is connected with the carbon tube clamp tube 104. When the internally threaded locking sleeve 105 locks the adapter tube 101 and the carbon tube clamp tube 104, the straight arm 113 is in the accommodation groove 114, the special-shaped arm 112 is in a vertical state and has an S shape, and the special-shaped arm 112 is close to the positioning hoop 109, which does not hinder the internally threaded locking sleeve 105.

[0031] Based on the above, the bottom of the straight arm 113 is arc-shaped, and the accommodation groove 114 is also arc-shaped. When the straight arm 113 is accommodated in the accommodation groove 114, the straight arm 113 fills the adapter tube 101 to be complete, so that the rotation of the internally threaded locking sleeve 105 is more smooth.

[0032] In addition, the inner part of the adapter pipe 101 and the carbon pipe clamping pipe 104 are both provided with a partition plate 115, so as to divide the inner cavity of the two into two parts, that is, to separate the two power supply lines.

[0033] Although the embodiments of the present application have been shown and described, it is to be understood that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present application, and the scope of the present application is defined by the appended claims and their equivalents.

Claims

1. A quick release tube clamp for connecting a UAV arm carbon tube and a main beam, comprising a quick release tube clamp body (100), characterized in that: The quick release pipe clamp body (100) comprises a connecting pipe (101) and a carbon pipe clamping pipe (104), the outer wall of the opposite parts of the connecting pipe (101) and the carbon pipe clamping pipe (104) is provided with external threads (103), and when the connecting pipe (101) and the carbon pipe clamping pipe (104) are connected, the external threads (103) of the two are connected, and the outer parts of the opposite parts of the connecting pipe (101) and the carbon pipe clamping pipe (104) are connected by internal thread locking sleeves (105), the internal thread locking sleeves (105) can be rotated to the end of the carbon pipe clamping pipe (104), the end of the arm carbon pipe is inserted into the carbon pipe clamping pipe (104), and one end of the connecting pipe (101) is fixed with an end plate (102) relative to the main beam, and a threading hole is formed in the end plate (102).

2. The UAV arm carbon tube quick release tube clamp of claim 1, wherein: The outer wall of the carbon pipe clamping pipe (104) is provided with a screw hole (106), and when the end of the arm carbon pipe is inserted into the carbon pipe clamping pipe (104), the screw is screwed into the screw hole (106).

3. The carbon-tube quick release clamp of claim 1 or 2, wherein: The outer wall of the carbon pipe clamping pipe (104) is provided with two opposite shrinkage joints (108) from the end to the other end, and the end of the carbon pipe clamping pipe (104) is movably sleeved with a locking hoop (107), and the two end portions of the locking hoop (107) are locked by a screw.

4. The UAV arm carbon tube quick release tube clamp of claim 1, wherein: The outer part of the connecting pipe (101) close to the end plate (102) is sleeved with a positioning hoop (109), the positioning hoop (109) is used for limiting the excessive forward movement of the internal thread locking sleeve (105) on the connecting pipe (101), the two end heads of the positioning hoop (109) are provided with threaded holes, and the two end heads are locked by a threaded rod (111) and a nut.

5. The UAV arm carbon tube quick release tube clamp of claim 4, wherein: The two end heads of the positioning hoop (109) are provided with a sleeve (116), the threaded rod (111) passes through the sleeve (116), the outer wall of the sleeve (116) is connected with a special-shaped arm (112), the special-shaped arm (112) is connected with a straight arm (113), the straight arm (113) is connected with the carbon pipe clamping pipe (104), and the positioning hoop (109), the sleeve (116), the straight arm (113) and the threaded rod (111) cooperatively form a hinge, and the hinge is connected between the carbon pipe clamping pipe (104) and the connecting pipe (101).

6. The UAV arm carbon tube quick release tube clamp of claim 5, wherein: The bottom of the connecting pipe (101) is provided with a containing groove (114), the containing groove (114) is used for containing the straight arm (113), the end of the carbon pipe clamping pipe (104) is connected with the straight arm (113), when the internal thread locking sleeve (105) locks the connecting pipe (101) and the carbon pipe clamping pipe (104), the straight arm (113) is in the containing groove (114), the special-shaped arm (112) is in a vertical state and an S shape, and the special-shaped arm (112) is close to the positioning hoop (109) and does not hinder the internal thread locking sleeve (105).

7. The UAV arm carbon tube quick release tube clamp of claim 6, wherein: The bottom of the straight arm (113) is arc-shaped, the containing groove (114) is also arc-shaped, and when the straight arm (113) is contained in the containing groove (114), the straight arm (113) fills the connecting pipe (101) to be complete.

8. The UAV arm carbon tube quick release tube clamp of claim 7, wherein: The bottom of the straight arm (113) is also provided with external thread (103), and the external thread (103) of the straight arm (113) is connected with the external thread (103) of the connecting pipe (101).

9. The UAV arm carbon tube quick release tube clamp of claim 1, wherein: The connecting pipe (101) and the carbon pipe clamping pipe (104) are both provided with a partition plate (115) inside, which divides the inner cavities of the two into two parts.

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