CN220199611U - Multifunctional installation bin for aircraft, flight device and flight suite - Google Patents

Abstract

The utility model discloses a multifunctional installation cabin, a flying device and a flying suite for an aircraft, wherein an installation cabin main body is hinged with an installation lifting mechanism through an installation mechanism, can be combined into a foldable and stowable flying device, and a handheld cradle head can be conveniently and rapidly inserted onto the flying device through rapid insertion or disassembly of a first cabin, so that a handheld mode or a flying mode can be randomly switched according to shooting use requirements; the lifting mechanism adopts a full-protection mode lifting mechanism with a rotor wing arranged in a closed shell, so that the flying device can take off and land on the palm; simple and compact structure, small volume, light weight, convenient carrying and high safety coefficient.

Description

Multifunctional installation bin for aircraft, flight device and flight suite

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to a multifunctional installation bin for an aircraft, a flight device and a flight suite.

Background

The mobile phone holder is also called a handheld stabilizer, and comprehensively has the functions of a selfie stick, a chicken head stabilizer and free control, so that better photo and video shooting effects are obtained, and the mobile phone holder can meet the use requirements of application scenes such as live broadcasting, video vlog, time-lapse photography, slow motion, panoramic photography, night scenes, object tracking, overlapping images, push-pull zooming (Seikok) and the like.

The flight tracking shooting equipment can be provided with a corresponding sensor and a control system to track a moving target, so that the rapid identification and tracking of the target are realized, the surrounding environment and the flight state are perceived in real time, the flight attitude and the flight speed are automatically adjusted, and the stable aerial shooting effect is ensured. Intelligent recognition and analysis of the target is performed by techniques such as computer vision and deep learning computer control while tracking the moving target; for example, when the unmanned aerial vehicle encounters a situation that the beagle runs, the computer vision system can recognize the appearance and the movement track of the beagle, then automatically track the behavior of the beagle, and shoot the moment under the optimal angle and light state at any time. The accurate control and the wonderful shooting effect can be realized by matching with corresponding automatic modes and operation instructions in the process of tracking the moving target; for example, a photographer can adopt a free tracking mode to realize omnibearing shooting of a target; the unmanned aerial vehicle can also adopt a tracking flight mode to control the unmanned aerial vehicle to fly along a preset track, so that more accurate and regular shooting is realized. The line tracking shooting device realizes multi-azimuth shooting by tracking a moving target principle, provides richer and changeable visual angles and expression methods, can improve shooting efficiency and quality, and can also develop wider creation space and visual field.

In the prior art, the handheld cradle head and the flight tracking shooting equipment can only be used independently and cannot be switched according to the use requirements of handheld shooting or flight tracking shooting; there is a lack of a mounting structure that can quickly couple a handheld cradle head to an aircraft.

Disclosure of Invention

In order to solve the problems in the prior art, the utility model aims to provide a multifunctional installation cabin, a flying device and a flying suite for an aircraft, which can facilitate the rapid insertion of a handheld tripod head onto the aircraft, so that the handheld mode or the flying mode can be switched at will according to shooting use requirements, and the multifunctional installation cabin is simple and compact in structure and high in safety coefficient.

The technical scheme adopted by the utility model is as follows:

a multifunctional installation cabin for an aircraft comprises an installation cabin main body;

the mounting bin body is provided with a first bin which is used for limiting and inserting the handheld cradle head;

the installation bin is characterized in that an installation mechanism is arranged at the bottom of the installation bin main body and used for hinging and installing a lifting mechanism.

Further, both the top and the front side of the first plenum are open.

Further, at least one pair of slots for mounting the lifting mechanism in a foldable manner in a hinged connection manner are symmetrically arranged at the bottoms of the two side walls of the mounting bin main body, and the mounting mechanism is formed by the at least one pair of slots.

Further, the first bin is arranged on the upper portion of the front section of the installation bin main body, and a control module installation space is arranged on the upper portion of the rear section of the installation bin main body.

Further, a second bin capable of inserting batteries is arranged at the lower part of the installation bin main body, and the second bin is opened on the rear side face of the installation bin main body.

Further, the front end face of the second bin is spaced from the front end face of the mounting main body by a distance, and a space between the front end face of the second bin and the front end face of the mounting main body forms a camera mounting machine position.

Still further, a TYPE C connector is disposed on the aft sidewall of the first plenum;

and the bottom surface of the second bin is also provided with a heat dissipation mechanism, a TOF sensor and a VIO sensor.

Still further, two pairs of slots are symmetrically arranged at the bottoms of two side walls of the installation bin main body, wherein a first pair of slots are arranged between the second bin and the camera installation machine, and a second pair of slots are arranged at the position, close to the rear end, of the side wall of the second bin.

Still further, the utility model also relates to a flying device which comprises a control module, a battery, a first camera, a pair of lifting mechanisms and the multifunctional installation bin for the aircraft;

the control module is arranged in the control module installation space;

the lifting mechanisms are symmetrically arranged at the left side and the right side of the installation bin main body and are connected to the installation bin main body through hinges;

the lifting mechanism comprises a pair of hollow protection shells and a plurality of rotary wings, and each rotary wing is arranged in a hollow inner cavity of each hollow protection shell;

the battery is inserted into the second cabin, and the first camera is rotatably installed on the camera position.

Finally, the utility model also relates to a flight kit, which comprises the handheld cradle head and the flight device, wherein the handheld cradle head is inserted into the first cabin, and the load end of the handheld cradle head extends out of the flight device from the front end of the first cabin; the load end is used for clamping the second camera.

The beneficial effects of the utility model are as follows:

the multifunctional installation bin for the aircraft, the flying device and the flying suite are characterized in that the installation bin main body is hinged with the installation lifting mechanism through the installation mechanism, can be combined into a foldable and contained flying device, and is convenient to quickly insert and install onto the flying device through the first bin or detach the handheld holder, so that the handheld mode or the flying mode can be switched at will according to shooting use requirements; the lifting mechanism adopts a full-protection mode lifting mechanism with a hollow protection shell and a rotor wing arranged in the hollow protection shell, so that the flying device can take off and land on the palm; simple and compact structure, small volume, light weight, convenient carrying and high safety coefficient.

Drawings

FIGS. 1 to 3 are schematic perspective views of a multifunctional mounting bin for an aircraft according to an embodiment of the present utility model;

FIGS. 4-5 are schematic plan view of a multifunctional mounting bin for an aircraft in accordance with an embodiment of the present utility model;

fig. 6 is a schematic perspective view of a flying device according to a second embodiment of the present utility model;

FIG. 7 is an exploded view of a three-dimensional structure of a flying device according to a second embodiment of the present utility model;

FIG. 8 is a schematic plan view of a flying apparatus according to a second embodiment of the present utility model;

FIG. 9 is a schematic bottom view of FIG. 8;

fig. 10 to 11 are schematic perspective views of a flight kit according to a third embodiment of the present utility model;

FIG. 12 is a schematic plan view of a flight kit according to a third embodiment of the utility model;

FIG. 13 is a schematic view of the bottom structure of FIG. 12;

fig. 14 is a schematic view illustrating a process of disassembling a handheld cradle head of a flight kit according to a third embodiment of the utility model.

Detailed Description

The following description of the technical solutions in the embodiments of the present application will be made clearly and completely with reference to the accompanying drawings in the embodiments of the present application, and it is apparent that the described embodiments are only some embodiments of the present application, not all embodiments. All other embodiments, which can be made by one of ordinary skill in the art without undue burden from the present disclosure, are within the scope of the present disclosure.

The terms "first," "second," "third," and the like in this application are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number or order of technical features indicated. All directional indications (such as up, down, left, right, front, back … …) in the embodiments of the present application are merely used to explain the relative positional relationship or movement between the components in a particular posture (as shown in the drawings), etc.; it should be noted that when an element is referred to as being "fixed," "disposed" or "connected" to another element, it may be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or one or more intervening elements may also be present therebetween. The terms "vertical," "horizontal," "left," "right," and the like are used herein for illustrative purposes only and are not meant to be the only embodiment.

As shown in fig. 1 to 14, the utility model provides a multifunctional installation cabin, a flying device and a flying suite for an aircraft, and the overall planning scheme is as follows:

embodiment one:

firstly, the idea is to provide a multifunctional installation cabin for an aircraft, which mainly comprises a transversely arranged installation cabin main body 1 with a cuboid structure; a first bin 11 is arranged on the installation bin main body, and the handheld cradle head 2 can be limited and inserted through the first bin 11; the bottom of the installation bin main body 1 is provided with an installation mechanism, and the lifting mechanism can be hinged through the installation mechanism, so that a portable flight device with the functions of rapidly limiting, inserting or disassembling the handheld cradle head and folding and shrinking is formed, and the handheld cradle head can be inserted into a first bin of the flight device to perform flight shooting, so that the flight cradle head function is realized; after the handheld cradle head is disassembled from the first bin and taken out, shooting can be carried out in a handheld manner; therefore, the handheld shooting or the flying shooting can be switched at any time according to shooting use requirements.

Further, the top and the front side of the first bin 11 are both set to be in an open state, so that the handheld cradle head can be quickly limited to be inserted or detached, and the operation is convenient.

Further, at least one pair of slots 12 are symmetrically arranged at the bottoms of two side walls of the installation bin main body 1, and the lifting mechanism can be installed in a foldable manner through the hinged connection mode through the pair of slots 12, so that the unmanned aerial vehicle and other flying devices are formed, the at least one pair of slots form the installation mechanism, the installation and connection operation are convenient, the occupied space is small, the structure is simple, the number of parts is small, and the size and the weight are light.

Further, the first bin 11 is disposed at an upper portion of a front section of the installation bin main body 1, and the control module installation space 13 is disposed at an upper portion of a rear section of the installation bin main body 1, and the control module can be installed through the control module installation space 13, so that a flight control system can be conveniently provided for the flight device.

Further, a second bin 14 is arranged at the lower part of the installation bin main body 1, and batteries can be inserted into the second bin to form a battery bin, and the second bin 14 is opened on the rear side surface of the installation bin main body 1, so that the batteries can be detached from the rear side of the installation bin main body, the battery detachment operation space is separated from the insertion detachment operation space of the handheld cradle head, and the battery detachment operation and the insertion detachment operation of the handheld cradle head are not interfered with each other, so that the operation is convenient.

Further, the front end face of the second chamber 14 is disposed with a distance from the front end face of the mounting chamber body 1 such that a space between the front end face of the second chamber 14 and the front end face of the mounting chamber body 1 constitutes a camera mounting position. Namely, the length of the second bin 14 is smaller than the total length of the installation bin main body 1, a gap space is arranged at the front side of the second bin 14, and the gap space is used as a camera installation machine position 20 for installing the first camera; be convenient for when follow-up combination flight device, install first camera through the camera mounting plate to the constitution can carry handheld cloud platform and carry out the flight shooting, also can track the flight shooting through flight device alone, makes the installation storehouse main part constitute the multi-functional installation storehouse that can be used for the aircraft.

Still further, a type connector 15 is provided on the rear sidewall of the first chamber 11, and when the handheld cradle head is inserted inside the first chamber, it may be connected to the control module and the battery through the type connector, thereby providing power and driving control.

The bottom surface at the second bin still is provided with heat dissipation mechanism 16, VIO sensor 17 and TOF sensor 18, and the supplementary heat that gives off in the battery course of working that gives off of through heat dissipation mechanism can realize real-time tracking shooting through TOF sensor and VIO sensor.

Specifically, a plurality of rectangular heat dissipation grooves are arranged side by side on a bottom plate of the second bin to form a heat dissipation mechanism; a VIO sensor is arranged in the middle of the position, close to the front end, of the bottom surface of the second bin, a TOF sensor can be arranged on the outer side of the VIO sensor, and two TOF sensors can be symmetrically arranged on two sides of the VIO sensor. Through VIO sensor and TOF sensor can realize first camera unmanned aerial vehicle and clap the function with taking a photo.

Still further, two pairs of slots are symmetrically arranged at the bottoms of the two side walls of the installation bin main body 1, wherein the first pair of slots are arranged at the position between the second bin and the camera installation machine, and the second pair of slots are arranged at the position, close to the rear end, of the side wall of the second bin. The lifting mechanisms can be symmetrically installed through the two pairs of slots when the functions of the flying device are realized subsequently.

The wall of the second compartment in this example is thicker so that the wall of the slot has sufficient hinge mounting locations and the folding and stretching process does not affect the normal operation of the battery inside the second compartment.

Embodiment two:

still further, there is provided a flying device having a basic structure consisting of a control module, a battery 19, a first camera 21, a lifting mechanism 3 and the above-described multifunctional mounting bin for an aircraft.

The control module is arranged in the control module installation space, and a power indicator lamp 25 can be arranged on the control module to visually display the electric quantity of the battery.

The lifting mechanisms 3 are symmetrically arranged at the left side and the right side of the installation bin main body 1, and the lifting mechanisms 3 are connected to the installation bin main body 1 in a hinged manner;

the specific structure of the lifting mechanism 3 is as follows: the main structure of the lifting mechanism 3 is a pair of hollow protecting shells 31 and four groups of rotary wings 32, and the left side and the right side of the installation bin main body 1 are respectively provided with one hollow protecting shell 31 and two groups of rotary wings 32;

the two sets of rotor wings 32 of each side are arranged in the hollow inner cavity of the hollow protection shell 31 to form a full protection mode lifting mechanism, so that the flight device can take off and land on the palm.

The battery 19 is inserted inside the second compartment 14, and the first camera 21 is rotatably installed in the space of the camera position. When the flying device flies alone, the flying tracking shooting function can be realized through the first camera; after the handheld cradle head is inserted into the first bin of the installation bin main body 1, the flying device can also drive the handheld cradle head to realize the flying cradle head function; the handheld shooting function of the handheld cradle head can be independently performed after the handheld cradle head is detached from the first bin of the installation bin main body 1.

The specific structure of the lifting mechanism in this example is as follows: each hollow protective shell 31 is of a groove box-shaped structure capable of being opened or closed, a plurality of first hollow slots 312 are formed in a top plate 311 of each hollow protective shell 31, and a plurality of second hollow slots 314 are formed in a bottom plate 313, so that a convection channel is formed.

The shape and the number of the first hollow slots 312 on the top plate 311 are different from those of the second hollow slots 314 on the bottom plate 313, and the projection of each first hollow slot 312 in the vertical direction overlaps with the projection part of the second hollow slot 314 in the corresponding position in the vertical direction, so that the air flow of the rotor 32 is ensured to be unobstructed when rotating.

In the first embodiment, four isosceles triangle first hollow slots 312 are disposed on the top plate 311 corresponding to the positions of each set of rotors 32, and the four isosceles triangle first hollow slots 312 are uniformly arranged around the center of each set of rotors 32.

Four rectangular first hollowed-out slots 314 are arranged on the bottom plate 312 corresponding to the positions of each rotor wing 32, and four isosceles rectangular second hollowed-out slots 314 are uniformly arranged around the center of each rotor wing 32.

The third hollow slot holes 315 with a plurality of rectangles can be respectively formed in the peripheral side walls of the hollow protection shell 31, so that the flying effect of the rotor 32 during rotation is further improved.

In the first embodiment, the hollowed-out protective housing 31 substantially forms a hollowed-out net-shaped box-shaped blade protective cover structure through the first hollowed-out slot 312, the first hollowed-out slot 314 and the third hollowed-out slot 315.

In the first embodiment, two sets of rotors are symmetrically arranged in the inner cavity of the hollow protecting shell 31, and each set of rotors is rotatably installed on the bottom plate of the hollow protecting shell 31 through a motor 33 respectively; a first group of hollow slotted holes are respectively arranged on the top plate of the hollow protective shell 31 at positions corresponding to each group of flying paddles, and a second group of hollow slotted holes are respectively arranged on the bottom plate at positions corresponding to each group of flying paddles; each motor is arranged on the central position of the area where a group of second hollow slotted holes are arranged on the bottom plate of the hollow protective shell 31. So that the hollowed-out protective shell 31 is also of a symmetrical structure around the transverse center line; the pair of hollowed-out protective cases 31 are symmetrically distributed around the longitudinal center line of the installation bin main body, so that the row device has a structure which is symmetrical to each other along the transverse center line and the longitudinal center line, and has good balance stability. The direction does not need to be distinguished in the assembly and use process, the combination can be carried out in any direction, the production process flow is simplified, and the operation is convenient.

The specific structure of the lifting mechanism can also adopt the lifting mechanism structure of the full-protection unmanned aerial vehicle structure in the prior art.

In this example, the lifting mechanisms on two sides of the installation bin main body 1 may be hinged in the slots on two sides of the installation bin main body 1 according to the installation mode of the foldable portable aircraft in the prior art, for example, the installation modes shown in the appearance patent with the patent number of CN202230717173.0 and the patent name of unmanned aerial vehicle and the appearance patent with the patent number of CN202230717222.0 and the patent name of unmanned aerial vehicle. The lifting mechanism structure in the appearance patent can also be directly adopted.

Embodiment III:

providing an application scene of a flight kit, through the first embodiment and the second embodiment, realizing the combination of a handheld cradle head and a flight device, combining the handheld cradle head 2 into a first bin of an installation bin main body 1 of the flight device to form the flight kit, and enabling a load end of the handheld cradle head to extend out of the flight device from the front end of the first bin so as to ensure the shooting effect of the flight cradle head; the first camera can be clamped and installed through the load end in a limiting mode, other occasions can be popularized and applied, and other loads can be carried according to the use requirements of different application scenes.

The multifunctional installation cabin, the flying device and the flying suite for the aircraft are characterized in that the installation cabin body is hinged with the installation lifting mechanism through the installation mechanism, can be combined into the foldable and stowable flying device, and the handheld cradle head can be conveniently and rapidly inserted onto the flying device through rapid insertion or disassembly of the first cabin, so that the handheld mode or the flying mode can be randomly switched according to shooting use requirements; the lifting mechanism adopts a full-protection mode lifting mechanism with a hollow protection shell and a rotor wing arranged in the hollow protection shell, so that the flying device can take off and land on the palm; simple and compact structure, small volume, light weight, convenient carrying and high safety coefficient.

The utility model is not limited to the above-described alternative embodiments, and any person who may derive other various forms of products in the light of the present utility model, however, any changes in shape or structure thereof, all falling within the technical solutions defined in the scope of the claims of the present utility model, fall within the scope of protection of the present utility model.

Claims (10)

1. A multifunctional mounting bin for an aircraft, characterized by: comprises a mounting bin main body;

the mounting bin body is provided with a first bin which is used for limiting and inserting the handheld cradle head;

the installation bin is characterized in that an installation mechanism is arranged at the bottom of the installation bin main body and used for hinging and installing a lifting mechanism.

2. The multi-purpose mounting bin for an aircraft of claim 1, wherein: the top and front sides of the first plenum are both open.

3. The multi-functional mounting cartridge for an aircraft of claim 2, wherein: at least one pair of slots for mounting the lifting mechanism in a foldable manner in a hinged connection mode are symmetrically arranged at the bottoms of the two side walls of the mounting bin main body, and the mounting mechanism is formed by the at least one pair of slots.

4. The multi-purpose mounting bin for an aircraft of claim 1, wherein: the first bin is arranged on the upper portion of the front section of the installation bin main body, and a control module installation space is arranged on the upper portion of the rear section of the installation bin main body.

5. The multi-purpose mounting bin for an aircraft of claim 4, wherein: the lower part of the installation bin main body is provided with a second bin which can be used for inserting batteries, and the second bin is opened on the rear side surface of the installation bin main body.

6. The multi-purpose mounting bin for an aircraft of claim 5, wherein: the front end face of the second bin is provided with a spacing distance from the front end face of the installation main body, and a space between the front end face of the second bin and the front end face of the installation main body forms a camera installation machine position.

7. The multi-purpose mounting bin for an aircraft of claim 6, wherein: a TYPE C connector is arranged on the rear side wall of the first bin;

and the bottom surface of the second bin is also provided with a heat dissipation mechanism, a TOF sensor and a VIO sensor.

8. The multi-functional mounting cartridge for an aircraft of claim 2, wherein: two pairs of slots are symmetrically arranged at the bottoms of two side walls of the installation bin main body, wherein the first pair of slots are arranged between the second bin and the camera installation machine, and the second pair of slots are arranged at the position, close to the rear end, of the side wall of the second bin.

9. A flying device, characterized in that: comprising a control module, a battery, a first camera lifting mechanism and a multifunctional mounting bin for an aircraft according to one of claims 1 to 8;

the control module is arranged in the control module installation space;

the lifting mechanisms are symmetrically arranged at the left side and the right side of the installation bin main body and are connected to the installation bin main body through hinges;

the lifting mechanism comprises a pair of hollow protection shells and a plurality of rotary wings, and each rotary wing is arranged in a hollow inner cavity of each hollow protection shell;

the battery is inserted into the second cabin, and the first camera is rotatably installed on the camera position.

10. A flight kit, characterized by: the flying device comprises a handheld cradle head and the flying device of claim 9, wherein the handheld cradle head is inserted into the first bin, and the load end of the handheld cradle head extends out of the flying device from the front end of the first bin; the load end is used for clamping the second camera.