Quick release structure for pod of unmanned aerial vehicle

Abstract

The utility model discloses an unmanned aerial vehicle pod quick-release structure which comprises a fuselage connecting piece and a pod connecting piece, and the fuselage connecting piece is detachably connected with the pod connecting piece. The machine body connecting piece comprises a first boss, a second boss and a mortise and tenon joint part, the first boss, the second boss and the mortise and tenon joint part are sequentially connected and integrally formed, the mortise and tenon joint part is located on the side, away from the first boss, of the second boss, and the mortise and tenon joint part is provided with two symmetrically-distributed mortise and tenon joint part cavities. The unmanned aerial vehicle pod quick-release structure has the advantages that when the protruding part in the body is completely screwed into the concave cavity of the mortise and tenon joint part, the fuselage connecting piece and the pod connecting piece are detachably connected, the mortise and tenon joint part rotates to the limiting position of the inner cavity of the pod connecting piece, and the unmanned aerial vehicle pod quick-release structure is high in firmness, not prone to loosening, convenient to disassemble and assemble and high in practicability. And the replacement efficiency can be improved.

Description

TECHNICAL FIELD

[0001] The utility model belongs to the field of unmanned aerial vehicle accessories, specifically relates to a quick release structure of unmanned aerial vehicle pod. BACKGROUND

[0002] The utility model discloses a quick release device of unmanned aerial vehicle holder, and its IPC classification number is B64D47 / 08, and its technical scheme discloses "the quick release device of unmanned aerial vehicle holder includes clamping device, holder clamping claw hook, holder clamping claw hook cooperation piece.

[0003] Therefore, the above utility model patent has disclosed one of the technical schemes of the quick release structure of unmanned aerial vehicle holder. However, the technical scheme disclosed by the above utility model patent focuses on realizing the suspension of different cameras, and does not further solve the problem of improving the firmness of the limit position by referring to the mortise and tenon principle, and needs to be further improved. UTILITY MODEL CONTENTS

[0004] The utility model provides a quick release structure of unmanned aerial vehicle pod in view of the prior art condition, and overcomes the above defects.

[0005] The utility model adopts the following technical scheme, and the quick release structure of unmanned aerial vehicle pod includes body connecting piece and pod connecting piece, the body connecting piece is detachably connected with the pod connecting piece, wherein:

[0006] The body connecting piece includes a first boss, a second boss and a mortise and tenon part, the first boss, the second boss and the mortise and tenon part are sequentially connected and integrally formed, the mortise and tenon part is located on the side, away from the first boss, of the second boss, and the mortise and tenon part has two symmetrical mortise and tenon part cavities;

[0007] The pod connecting piece includes a pod connecting piece body, the pod connecting piece body has a pod connecting piece inner cavity, the pod connecting piece inner cavity is provided with two symmetrical body inner protrusions, the body inner protrusions are integrally formed with the pod connecting piece body, and the body inner protrusions are matched with the mortise and tenon part cavities.

[0008] As a preferred technical scheme of the above technical scheme, the mortise and tenon part is provided with a mortise and tenon part body and two mortise and tenon part long shaft extension segments, the mortise and tenon part long shaft extension segments are located on the two sides of the mortise and tenon part body, and the mortise and tenon part long shaft extension segments are integrally formed with the mortise and tenon part body.

[0009] As a preferred technical scheme of the above technical scheme, the mortise and tenon part cavities are located at the ends, away from the mortise and tenon part body, of the mortise and tenon part long shaft extension segments.

[0010] As the preferred technical scheme of the above technical scheme, the inner protruding part of the body is a hemisphere.

[0011] As the preferred technical scheme of the above technical scheme, the inner cavity of the pod connecting piece has two symmetrically distributed inner extension cavities of the pod connecting piece, and the inner protruding part of the body is located in the inner extension cavity of the pod connecting piece.

[0012] The unmanned aerial vehicle pod quick disassembly structure has the beneficial effects that when the inner protruding part of the body is completely screwed into the mortise part cavity, the detachable connection of the fuselage connecting piece and the pod connecting piece is completed, the mortise part is rotated to the limit position of the inner cavity of the pod connecting piece, has strong firmness, is not easy to loosen, and is convenient to disassemble and assemble, and the replacement efficiency can be improved. BRIEF DESCRIPTION OF DRAWINGS

[0013] Figure 1 is a perspective view of one angle of the present application.

[0014] Figure 2 is a perspective view of another angle of the present application.

[0015] Figure 3 is a front view of the present application.

[0016] Figure 4 is a sectional view along the AA direction of the present application. Figure 3

[0017] Figure 5 is a perspective view of the fuselage connecting piece of the present application.

[0018] Figure 6 is a top view of the fuselage connecting piece of the present application.

[0019] Figure 7 is a perspective view of one angle of the pod connecting piece of the present application.

[0020] Figure 8 is a perspective view of another angle of the pod connecting piece of the present application.

[0021] The reference signs include: 100-fuselage connecting piece; 110-first boss; 120-second boss; 130-mortise part; 131-mortise part cavity; 132-mortise part body; 133-mortise part long axis extension section; 134-mortise part concave surface; 200-pod connecting piece; 201-inner cavity of the pod connecting piece; 202-inner extension cavity of the pod connecting piece; 210-body of the pod connecting piece; 220-inner protruding part of the body. DETAILED DESCRIPTION

[0022] The utility model discloses an unmanned aerial vehicle pod quick disassembly structure, below combining preferred embodiment (example 1), referring to the Figures 1 to 8 ​The specific embodiments of the utility model are further described.

[0023] Referring to the drawings Figure 1 To the figure, Figures 1 to 8 , Figures 1 to 3 Respectively show the unmanned plane nacelle quick release structure of different visual angle, Figure 4 Show the cross section structure of unmanned plane nacelle quick release structure, Figure 5 And Figure 6 Respectively show the fuselage connecting piece of different visual angle, Figure 7 And Figure 8 Respectively show the nacelle connecting piece of different visual angle.

[0024] Embodiment 1.

[0025] Preferably, the unmanned plane nacelle quick release structure includes fuselage connecting piece 100 and nacelle connecting piece 200, fuselage connecting piece 100 is detachably connected (specifically, is screwed) with nacelle connecting piece 200, fuselage connecting piece 100 is further connected to the unmanned plane fuselage (not shown in the figure), nacelle connecting piece 200 is further connected to the unmanned plane nacelle (not shown in the figure), wherein:

[0026] Fuselage connecting piece 100 includes first boss 110, second boss 120 and mortise and tenon part 130, first boss 110, second boss 120 and mortise and tenon part 130 are sequentially connected and integrally formed, mortise and tenon part 130 is located on the side of second boss 120 away from first boss 110, and mortise and tenon part 130 has two symmetrical mortise and tenon part cavities 131; So that first boss 110 is connected to the unmanned plane fuselage, and mortise and tenon part 130 is screwed to nacelle connecting piece body 210;

[0027] Nacelle connecting piece 200 includes nacelle connecting piece body 210, and the nacelle connecting piece body 210 has nacelle connecting piece inner cavity 201, and the two body inner protrusions 220 symmetrically distributed are built-in in the nacelle connecting piece inner cavity 201, the body inner protrusions 220 are integrally formed with the nacelle connecting piece body 210, and the body inner protrusions 220 are matched with the mortise and tenon part cavities 131;So that mortise and tenon part 130 can be inserted into nacelle connecting piece inner cavity 201, so that fuselage connecting piece 100 and nacelle connecting piece 200 are detachably connected (specifically, are screwed);Further, when the body inner protrusions 220 are completely screwed into the mortise and tenon part cavities 131, the fuselage connecting piece 100 and the nacelle connecting piece 200 are detachably connected (specifically, are screwed) and completed, the mortise and tenon part 130 is rotated to the limit position of the nacelle connecting piece inner cavity 201, has strong firmness, is not easy to loosen and is convenient to disassemble and assemble, and the replacement efficiency can be improved.

[0028] The mortise part 130 is provided with a mortise part body 132 and two mortise part long shaft extension segments 133, the mortise part long shaft extension segments 133 are located at two sides of the mortise part body 132, and the mortise part long shaft extension segments 133 are integrally formed with the mortise part body 132.

[0029] The mortise part concave cavity 131 is located at the end of the mortise part long shaft extension segment 133 away from the mortise part body 132.

[0030] The mortise part concave cavity 131 is provided with a mortise part concave surface 134, so that the curvature of the mortise part concave surface 134 is consistent with the curvature of the body inner protrusion 220.

[0031] Preferably, the body inner protrusion 220 is a hemisphere.

[0032] The gondola connecting piece inner cavity 201 has two symmetrically distributed gondola connecting piece inner extension cavities 202, and the body inner protrusion 220 is located at the end of the gondola connecting piece inner extension cavity 202.

[0033] The working principle of the quick release structure of the unmanned aerial vehicle gondola disclosed in the embodiment is described below.

[0034] Specifically, the quick release structure of the unmanned aerial vehicle gondola, the fuselage connecting piece 100 is installed on the unmanned aerial vehicle fuselage, and the gondola connecting piece 200 is installed on the unmanned aerial vehicle gondola. The fuselage connecting piece 100 and the gondola connecting piece 200 are rotatably fastened, wherein the fuselage connecting piece 100 is usually installed on the unmanned aerial vehicle fuselage and does not need to be frequently disassembled; the gondola connecting piece 200 is usually installed on the unmanned aerial vehicle gondola and does not need to be frequently disassembled. When installing, the gondola connecting piece 200 is inserted into the fuselage connecting piece 100 and then rotated and clamped.

[0035] The quick release structure of the unmanned aerial vehicle gondola disclosed in the embodiment, by referring to the mortise structure and the mortise principle, has strong firmness after clamping, is not easy to loosen, and is convenient to disassemble and assemble, so that the replacement efficiency can be improved; it can also be applied to various types of unmanned aerial vehicles at the same time, and has strong universal adaptability. By using the quick release structure of the unmanned aerial vehicle gondola disclosed in the embodiment, the unmanned aerial vehicle operator can conveniently replace and maintain the unmanned aerial vehicle gondola, and the task execution efficiency and reliability of the unmanned aerial vehicle are indirectly improved.

[0036] It is worth mentioning that the material and other technical features of the hemisphere involved in the utility model patent application should be regarded as prior art, the specific structure, working principle and possible control mode and spatial arrangement mode of these technical features can be selected by using the conventional selection in the field, and should not be regarded as the invention point of the utility model patent, and the utility model patent will not be further expanded and described in detail.

[0037] Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application should be included in the protection scope of the present application.

Claims

1. A quick-disassembly structure for a drone pod, characterized in that: It includes a fuselage connecting piece and a pod connecting piece, and the fuselage connecting piece and the pod connecting piece are detachably connected, wherein: The fuselage connecting member includes a first boss, a second boss and a mortise and tenon portion, which are sequentially connected and integrally formed. The mortise and tenon portion is located on a side of the second boss away from the first boss, and has two symmetrically distributed mortise and tenon cavities. The pod connector includes a pod connector body, which has a pod connector inner cavity. The pod connector inner cavity contains two symmetrically distributed body protrusions, the body protrusions and the pod connector body are integrally formed, and the body protrusions cooperate with the mortise and tenon cavity.

2. The UAV pod quick-detachable structure according to claim 1, characterized in that: The mortise and tenon part is provided with a mortise and tenon part body and two mortise and tenon long axis extension sections, the mortise and tenon long axis extension sections are located on both sides of the mortise and tenon part body, and the mortise and tenon long axis extension sections are integrally formed with the mortise and tenon part body.

3. The UAV pod quick-detachable structure according to claim 2, characterized in that: The mortise and tenon cavity is located at the end of the mortise and tenon long axis extension section away from the mortise and tenon body.

4. The UAV pod quick-detachable structure according to claim 1, characterized in that: The protruding part in the main body is a hemispherical body.

5. The UAV pod quick-detachable structure according to claim 1, characterized in that: The inner cavity of the pod connector is provided with two symmetrically distributed inner extension cavities of the pod connector, and the protruding portion in the body is located in the inner extension cavities of the pod connector.

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