CN112373695A - Carry cabin and unmanned aerial vehicle - Google Patents
Carry cabin and unmanned aerial vehicle Download PDFInfo
- Publication number
- CN112373695A CN112373695A CN202011347298.5A CN202011347298A CN112373695A CN 112373695 A CN112373695 A CN 112373695A CN 202011347298 A CN202011347298 A CN 202011347298A CN 112373695 A CN112373695 A CN 112373695A
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- Prior art keywords
- clamp
- electrical plug
- mounting
- plug
- cabin
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
Abstract
The invention discloses a mounting cabin and an unmanned aerial vehicle, which comprise a shell; the clamp is arranged on the shell and can clamp the inserting guide rail; and a second electrical plug disposed on the housing, the second electrical plug being capable of communicative connection with the first electrical plug when the second electrical plug is mated with the first electrical plug. When the mounting cabin needs to be replaced, the whole mounting cabin is directly detached, then the mounting cabin is replaced by another mounting cabin for installation, and a second electric plug of the mounting cabin is butted with a first electric plug of the machine body so as to realize communication connection between the second electric plug and the first electric plug. Compared with the prior art, the mounting cabin provided by the invention is connected with the inserting guide rail through the clamp without other connecting pieces, so that the mounting and dismounting efficiency of the mounting cabin is improved.
Description
Technical Field
The invention relates to the technical field of aviation, in particular to a mounting cabin and an unmanned aerial vehicle.
Background
At present, most unmanned aerial vehicle's carry cabin is connected with the fuselage through a plurality of connecting pieces, when the carry cabin is changed to needs, because the connecting piece is more, carry cabin installation effectiveness is lower.
Therefore, how to improve the efficiency of attaching and detaching the mounting compartment becomes a technical problem to be solved urgently by those skilled in the art.
Disclosure of Invention
The invention aims to provide a mounting cabin and an unmanned aerial vehicle, so that the mounting and dismounting efficiency of the mounting cabin is improved.
In order to achieve the above object, the present invention provides a mounting cabin for connecting with a body of an unmanned aerial vehicle, where the body includes a power supply, a first data interaction end, a power output end and a first electrical plug, the power output end is electrically connected with the power supply, the first electrical plug is electrically connected with the first data interaction end and the power output end, and the mounting cabin includes:
the device comprises a shell, wherein one of a clamp and an inserting guide rail is arranged on the shell, the other one is arranged on the machine body, and the clamp can clamp the inserting guide rail;
the second data interaction end and the power input end are arranged in the shell; and
the second electrical plug is arranged on the shell and electrically connected with the second data interaction end and the power input end, when the second electrical plug is in butt joint with the first electrical plug, the first data interaction end and the second data interaction end can be in communication connection, and the power input end is electrically connected with the power output end.
In one embodiment of the invention, the first electrical plug is flexibly or rigidly connected to the body; and/or the second electrical plug is flexibly or rigidly connected to the housing.
In one embodiment of the invention, the first electrical plug and the second electrical plug are of the D-SUB standard electrical plug type.
In one embodiment of the invention, the inserting guide rail is provided with a clamping part locked on the clamp.
In one embodiment of the present invention, the clamping portion is a clamping hole penetrating through two sides of the insertion guide rail.
In one embodiment of the invention, the clamp comprises a clamp body fixed on the shell; and the clamping piece is arranged on the clamp body, and a clamping hole for accommodating the insertion guide rail to pass through is formed between the clamping piece and the clamp body.
In one embodiment of the invention, the clamping piece is arranged on the clamp body through a screw, and the screw is matched with the clamping part.
In one embodiment of the present invention, the number of the clamps is two.
In one embodiment of the invention, two clamps are symmetrically arranged on the shell.
The invention also discloses an unmanned aerial vehicle which comprises a vehicle body and the mounting cabin.
The invention also discloses the unmanned aerial vehicle, and the mounting cabin comprises the photoelectric pod and/or the camera holder and/or the throwing device.
When the mounting cabin is used, the mounting cabin is arranged on the inserting guide rail through the clamp, so that the mounting of the mounting cabin and the machine body is realized, the second electric plug is in butt joint with the first electric plug of the machine body, and the transmission of power supply and data of the mounting cabin and the machine body is realized through the second electric plug and the first electric plug. When the mounting cabin needs to be replaced, the whole mounting cabin is directly detached, then the mounting cabin is replaced by another mounting cabin for installation, and a second electric plug of the mounting cabin is butted with a first electric plug of the machine body so as to realize communication connection between the second electric plug and the first electric plug. Compared with the prior art, the mounting cabin provided by the invention is connected with the inserting guide rail through the clamp, and can be quickly disassembled and assembled without other disassembling and assembling tools, so that the disassembling and assembling efficiency of the mounting cabin is improved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the provided drawings without creative efforts.
Fig. 1 is a schematic perspective view of a mounting cabin according to an embodiment of the present invention;
fig. 2 is a schematic perspective view of another mounting compartment according to an embodiment of the present invention;
fig. 3 is a schematic perspective view of another mounting compartment according to an embodiment of the present invention;
fig. 4 is a schematic perspective view of another mounting cabin according to an embodiment of the present invention;
fig. 5 is a schematic perspective view of a mounting cabin according to an embodiment of the present invention;
fig. 6 is a schematic front view of a mounting compartment according to an embodiment of the present invention;
wherein: 100 is a body, 200 is a mounting cabin, 101 is a first electric plug, 102 is a plug-in guide rail, 1021 is a clamping part, 201 is a shell, 202 is a second electric plug, 203 is a clamp, 2031 is a clamp body, 2032 is a clamping piece, and 2033 is a screw.
Detailed Description
The invention provides a mounting cabin and an unmanned aerial vehicle, which aim to improve the mounting and dismounting efficiency of the mounting cabin.
In order to make the technical solutions of the present invention better understood by those skilled in the art, the present invention will be further described in detail with reference to the accompanying drawings and embodiments.
Referring to fig. 1 to 6, a mounting cabin 200 disclosed in the present invention is used for connecting with a body 100 of an unmanned aerial vehicle, the body 100 includes a power supply, a first data interaction end, a power output end and a first electrical plug 101, the power output end is electrically connected with the power supply, and the first electrical plug 101 is electrically connected with the first data interaction end and the power output end; the mounting cabin 200 comprises a shell 201, a second data interaction end, a power supply input end and a second electrical plug 202, wherein the shell 201 is provided with one of a clamp 203 and a plug-in guide rail 102, the other one is arranged on the machine body 100, and the clamp 203 can clamp the plug-in guide rail 102 to realize connection with the machine body 100; the second electrical plug 202 is arranged on the shell 201 and is electrically connected with the second data interaction end and the power input end, when the second electrical plug 202 is butted with the first electrical plug 101, the first data interaction end and the second data interaction end can be in communication connection, and the power input end is electrically connected with the power output end.
When the mounting cabin 200 of the present invention is used, the mounting cabin 200 is mounted on the insertion guide rail 102 through the clamp 203, so that the mounting of the mounting cabin and the body 100 is realized, the second electrical plug 202 is butted with the first electrical plug 101 of the body 100, and the transmission of power and data between the mounting cabin 200 and the body 100 is realized through the second electrical plug 202 and the first electrical plug 101. When the mounting cabin needs to be replaced, the whole mounting cabin is directly detached, then the mounting cabin is replaced by another mounting cabin for installation, and a second electric plug of the mounting cabin is butted with a first electric plug of the machine body so as to realize communication connection between the second electric plug and the first electric plug. Compared with the prior art, the hanging cabin is connected through the inserting guide rail 102 and the clamp 203 without other connecting pieces, so that the dismounting efficiency of the hanging cabin is improved.
It should be noted that different devices, such as the optoelectronic pod, the camera pan-tilt, the dropping device, etc., can be selected for the mounting chamber 200, and any adjustment of the fuselage 100 is not required for replacing different types of mounting chambers 200.
For example: one end of the body 100 is provided with a plug guide 102, and the housing 201 is provided with a clamp 203 which is matched with the plug guide 102. When the mounting cabin 200 needs to be installed on the fuselage 100, the fuselage 100 and the housing 201 are butted and clamped by the plug-in guide rail 102 and the clamp 203.
The clamp 203 secures the plug rail 102 to the clamp 203 by means of a clamping force, or the clamp 203 is connected to the plug rail 102 by means of another component. For this purpose, the plug rail 102 is provided with a catch portion 1021 locked on the clamp 203, which catch portion 1021 can be understood as a projection, a slot, a catch hole, etc. It is within the scope of the present invention for the mating clamp 203 to secure the plug rail 102.
The clamp 203 of the present invention includes a clamp body 2031 fixed to the housing; and a clamping piece 2032 arranged on the clamp body 2031, wherein a clamping hole for accommodating the insertion guide rail to pass through is arranged between the clamping piece 2032 and the clamp body 2031. The clamp body 2031 and the clamping piece 2032 are connected by a screw 2033, a snap structure, or a torsion spring, and the structure that can realize the clamping fit between the clamp body 2031 and the clamping piece 2032 is within the protection scope of the present invention. Preferably, the clamping piece 2032 is disposed on the clamping body 2031 by a screw 2033, and the screw 2033 is engaged with the engaging portion 1021, when the screw 2033 passes through the clamping body 2031 and the clamping piece 2032, it also passes through the engaging hole, so that the screw 2033 can fix the clamping piece 2032 and the clamping body 2031 and clamp the engaging hole.
In one embodiment of the present invention, to facilitate docking, one of the housing 201 and the body 100 is provided with a guide post, and the other is provided with a guide hole to be matched with the guide post. In order to prevent the butt joint error, the embodiment of the invention is provided with two guide posts, the shapes of the two guide posts are different, and the shapes of the guide holes matched with the two guide posts are different, so the butt joint error can be effectively prevented.
The above is a description of a specific connection manner of the housing 201 and the main body 100, and the relationship between the first electrical plug 101 and the second electrical plug 202 and the housing 201 will be described below, and the first electrical plug 101 is flexibly connected or rigidly connected to the main body 100. The flexible connection is understood to mean that the first electrical plug 101 is in communication connection with the main body 100 through a wire in the middle except for the fixed connection, the position of the first electrical plug 101 can be adjusted through the wire, and the relative position between the main body 100 and the first electrical plug 101 is more flexibly adjusted as the guiding distance between the main body 100 and the first electrical plug 101 is longer. While a rigid connection is in contrast to a flexible connection, the first electrical plug 101 is directly fixed to the body 100, and the relative position between the two cannot be adjusted.
Likewise, the second electrical plug 202 is flexibly or rigidly connected to the housing 201. The flexible connection is understood to mean that the second electrical plug 202 is in communication connection with the housing 201 through a wire in the middle except for the fixed connection, the position of the second electrical plug 202 can be adjusted through the wire, and the relative position between the housing 201 and the second electrical plug 202 is more flexibly adjusted as the guiding distance between the housing 201 and the second electrical plug 202 is longer. Whereas a rigid connection is in contrast to a flexible connection, the second electrical plug 202 is directly fixed to the housing 201, the relative position between the two being not adjustable.
Since the first and second electrical plugs 101 and 202 function to achieve the communication connection between the mounting compartment 200 and the main body 100, it is within the scope of the present invention to achieve the above-mentioned object, and it is preferable that the first and second electrical plugs 101 and 202 are of a D-SUB standard electrical plug type, which can improve the connection reliability and the kind of transmittable data.
In the above embodiment, the body is provided with the insertion guide rail, the mounting cabin is provided with the clamp matched with the insertion guide rail, the body can be provided with the clamp, the mounting cabin is provided with the insertion guide rail matched with the clamp, specifically, the mounting cabin 200 disclosed by the invention is used for being connected with the body 100 of the unmanned aerial vehicle, the body 100 comprises a power supply, a first data interaction end, a power output end, a first electrical plug 101 and the clamp, the power output end is electrically connected with the power supply, the first electrical plug 101 is electrically connected with the first data interaction end and the power output end, the mounting cabin 200 comprises a shell 201, a second data interaction end, a power input end, a second electrical plug 202 and the insertion guide rail, wherein the shell 201 is detachably connected with the clamp of the body 100 through the insertion guide rail; the second electrical plug 202 is arranged on the shell 201 and is electrically connected with the second data interaction end and the power input end, when the second electrical plug 202 is butted with the first electrical plug 101, the first data interaction end and the second data interaction end can be in communication connection, and the power input end is electrically connected with the power output end.
When the mounting cabin 200 of the invention is used, the mounting cabin 200 is arranged on the clamp through the inserting guide rail, so that the mounting of the mounting cabin and the machine body is realized, the second electric plug 202 is in butt joint with the first electric plug 101 of the machine body 100, and the transmission of power supply and data of the mounting cabin 200 and the machine body 100 is realized through the second electric plug 202 and the first electric plug 101. When the mounting cabin needs to be replaced, the whole mounting cabin is directly detached, then the mounting cabin is replaced by another mounting cabin for installation, and a second electric plug of the mounting cabin is butted with a first electric plug of the machine body so as to realize communication connection between the second electric plug and the first electric plug. Compared with the prior art, the mounting cabin is connected through the threads without other connecting pieces, so that the mounting and dismounting efficiency of the mounting cabin is improved.
It should be noted that a clamp is disposed at one end of the body 100, and the housing 201 is provided with an insertion guide rail that is matched with the clamp. When the mounting cabin 200 needs to be installed on the body 100, the body 100 and the shell 201 are butted, and clamping connection is carried out through a clamp and a plug-in guide rail.
The inserting guide rail is fixed on the inserting guide rail through the clamp force, or the inserting guide rail is connected with the clamp through other parts. For this reason, be provided with the joint portion of locking on the anchor clamps on the grafting guide rail, this joint portion can be understood as arch, draw-in groove, joint hole etc.. The invention is in the protection scope as long as the fixture can be fixed by matching with the insertion guide rail.
The clamp comprises a clamp body 2031 fixed on a machine body; and a clamping piece 2032 arranged on the clamp body 2031, wherein a clamping hole for accommodating the insertion guide rail to pass through is arranged between the clamping piece 2032 and the clamp body 2031. The clamp body 2031 and the clamping piece 2032 are connected by a screw 2033, a snap structure, or a torsion spring, and the structure that can realize the clamping fit between the clamp body 2031 and the clamping piece 2032 is within the protection scope of the present invention. Preferably, the clamping piece 2032 is disposed on the clamping body 2031 by a screw 2033, and the screw 2033 is engaged with the engaging portion 1021, when the screw 2033 passes through the clamping body 2031 and the clamping piece 2032, it also passes through the engaging hole, so that the screw 2033 can fix the clamping piece 2032 and the clamping body 2031 and clamp the engaging hole.
In one embodiment of the present invention, to facilitate docking, one of the housing 201 and the body 100 is provided with a guide post, and the other is provided with a guide hole to be matched with the guide post. In order to prevent the butt joint error, the embodiment of the invention is provided with two guide posts, the shapes of the two guide posts are different, and the shapes of the guide holes matched with the two guide posts are different, so the butt joint error can be effectively prevented.
The above is a description of a specific connection manner of the housing 201 and the main body 100, and the relationship between the first electrical plug 101 and the second electrical plug 202 and the housing 201 will be described below, and the first electrical plug 101 is flexibly connected or rigidly connected to the main body 100. The flexible connection is understood to mean that the first electrical plug 101 is in communication connection with the main body 100 through a wire in the middle except for the fixed connection, the position of the first electrical plug 101 can be adjusted through the wire, and the relative position between the main body 100 and the first electrical plug 101 is more flexibly adjusted as the guiding distance between the main body 100 and the first electrical plug 101 is longer. While a rigid connection is in contrast to a flexible connection, the first electrical plug 101 is directly fixed to the body 100, and the relative position between the two cannot be adjusted.
Likewise, the second electrical plug 202 is flexibly or rigidly connected to the housing 201. The flexible connection is understood to mean that the second electrical plug 202 is in communication connection with the housing 201 through a wire in the middle except for the fixed connection, the position of the second electrical plug 202 can be adjusted through the wire, and the relative position between the housing 201 and the second electrical plug 202 is more flexibly adjusted as the guiding distance between the housing 201 and the second electrical plug 202 is longer. Whereas a rigid connection is in contrast to a flexible connection, the second electrical plug 202 is directly fixed to the housing 201, the relative position between the two being not adjustable.
Since the first and second electrical plugs 101 and 202 function to achieve the communication connection between the mounting compartment 200 and the main body 100, it is within the scope of the present invention to achieve the above-mentioned object, and it is preferable that the first and second electrical plugs 101 and 202 are of a D-SUB standard electrical plug type, which can improve the connection reliability and the kind of transmittable data.
The invention also discloses an unmanned aerial vehicle which comprises a fuselage 100 and the mounting cabin 200 in any one of the above manners.
It should be noted that the airframe 100 of the present invention is provided with a motor, a propeller, a flight control system and an actuating device, so as to realize the flight and control of the unmanned aerial vehicle. The mounting cabin 200 can be selected from different devices, such as a photoelectric pod, a camera holder, a throwing device and the like, and the fuselage 100 does not need to be adjusted at all when different types of mounting cabins 200 are replaced.
Because above-mentioned carry cabin 200 has above effect, unmanned aerial vehicle including above-mentioned fuselage also has corresponding effect, and this is no longer repeated here.
The embodiments in the present description are described in a progressive manner, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments are referred to each other.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (11)
1. The utility model provides a carry cabin for be connected with unmanned aerial vehicle's fuselage, a serial communication port, the fuselage includes power supply, the mutual end of first data, power output end and first electric plug, power output end with power supply electricity is connected, first electric plug with the mutual end of first data with power output end electricity is connected, carry the cabin and include:
the device comprises a shell, wherein one of a clamp and an inserting guide rail is arranged on the shell, the other one is arranged on the machine body, and the clamp can clamp the inserting guide rail;
the second data interaction end and the power input end are arranged in the shell; and
the second electrical plug is arranged on the shell and electrically connected with the second data interaction end and the power input end, when the second electrical plug is in butt joint with the first electrical plug, the first data interaction end and the second data interaction end can be in communication connection, and the power input end is electrically connected with the power output end.
2. The mounting bay of claim 1, wherein the first electrical plug is flexibly or rigidly connected to the fuselage; and/or the second electrical plug is flexibly or rigidly connected to the housing.
3. The mounting bay of claim 1, wherein the first electrical plug and the second electrical plug are of the D-SUB standard electrical plug type.
4. The mounting compartment of claim 1 wherein the plug-in guide rail is provided with a snap-in portion that locks onto the clamp.
5. The carrying cabin according to claim 4, wherein the clamping portions are clamping holes penetrating through both sides of the insertion guide rail.
6. The mounting compartment of claim 5 wherein the clamp includes a clamp body secured to the housing; and the clamping piece is arranged on the clamp body, and a clamping hole for accommodating the insertion guide rail to pass through is formed between the clamping piece and the clamp body.
7. The carrying cabin according to claim 6, wherein the clip is disposed on the clip body by a screw, and the screw is engaged with the engaging portion.
8. The mounting bay of claim 6, wherein the number of clamps is two.
9. The mounting bay of claim 8, wherein two of the clamps are symmetrically disposed on the housing.
10. A drone, characterized in that it comprises a fuselage and a mounting bay according to any one of claims 1 to 9.
11. A drone according to claim 10, characterised in that the stowage bin comprises an optoelectronic pod, and/or a camera head and/or a launch device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011347298.5A CN112373695A (en) | 2020-11-26 | 2020-11-26 | Carry cabin and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011347298.5A CN112373695A (en) | 2020-11-26 | 2020-11-26 | Carry cabin and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112373695A true CN112373695A (en) | 2021-02-19 |
Family
ID=74588486
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011347298.5A Pending CN112373695A (en) | 2020-11-26 | 2020-11-26 | Carry cabin and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112373695A (en) |
-
2020
- 2020-11-26 CN CN202011347298.5A patent/CN112373695A/en active Pending
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