CN208393635U - A kind of automatic erecting by overhang of helicopter - Google Patents
A kind of automatic erecting by overhang of helicopter Download PDFInfo
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- CN208393635U CN208393635U CN201820593833.7U CN201820593833U CN208393635U CN 208393635 U CN208393635 U CN 208393635U CN 201820593833 U CN201820593833 U CN 201820593833U CN 208393635 U CN208393635 U CN 208393635U
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- overhang
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- erecting
- cabin
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Abstract
This application discloses a kind of automatic erectings by overhang of helicopter, including carry device and location identification unit, carry device is connect with location identification unit, carry device includes winch, one end of winch connecting steel wire ropes rope, the other end of steel wire cable is equipped with autonomous suspension hook, the first erecting by overhang connection of autonomous suspension hook and mission payload.The automatic erecting by overhang of the helicopter of the application is connect by winch lower wire rope with mission payload, and structure is simply convenient for operating, and can flexibly realize and connect and unload with hanging for mission payload.Location identification unit in the automatic erecting by overhang of the helicopter of the application can identify and position mission payload, to more accurately realize the connection with mission payload, be accurately realized the transport of cargo；It can be realized and carry cargo in tape cabin body, facilitate the transport of cargo in the not increased situation of outer hanging body product, stability is more preferable, and lifting capacity is stronger.
Description
Technical field
The utility model relates to aviation field more particularly to a kind of helicopter hanger devices
Background technique
Transport load-carrying is hung outside modern helicopters to be restricted, complex contour when loading bulk goods, in addition store Combinations are light-weight, i.e.,
Using general container bag also due to small volume, load-carrying are light；It also will affect the operation machine safety of ground service handling personnel simultaneously,
Fall off hanging object when due to excessively high from the ground damage goods；Existing transport helicopter comes real essentially by electric winch or outer hanging
Current task load mounts, but outer hanging, electric winch pass through single hook and be connected with mission payload, thus not can guarantee and mount
Larger volume article stability in-flight, plug-in mode transportation volume large article can not be passed through；Traditional helicopter is hung
Hang relatively backward, and than cumbersome, reliability and stability is poor, and the equipment volume of transport has certain limitation, outer hanging mode
It is biggish to be mainly used for volume, because it is contemplated that driver, is not easy to the transport of freight in cabin；Transport performance is to environment
It is selective, it can not be transported under rugged environment.Even if there is the transport of some unmanned vehicles, the fortune of unmanned vehicle
Defeated positioning accuracy is poor, can not accurately realize the transport of cargo, and it is poor to transport lifting capacity.
Utility model content
The purpose of this utility model is to provide a kind of automatic erectings by overhang of helicopter, including carry device and position identification
Unit can be realized and mount different types of mission payload in unmanned transport helicopter, and passes through accurate Position Fixing Navigation System,
Realize loading and the unloading of mission payload.
A kind of automatic erecting by overhang of helicopter, including carry device and location identification unit, carry device and position identify
Unit connection, carry device include winch, and one end of winch connecting steel wire ropes rope, the other end of steel wire cable, which is equipped with, independently to be hung
First erecting by overhang of hook, autonomous suspension hook and mission payload connects.
As above, wherein mechanical arm, the end clamped wire rope of mechanical arm are equipped in unmanned helicopter；Position identification
Unit is electrically connected with mechanical arm, and location identification unit controls the movement of mechanical arm.
As above, wherein winch includes big winch and puffer, and big winch is mounted on helicopter center.
As above, wherein including cabin, cabin center is equipped with main hanging interface, and main hanging interface is autonomous with big winch
Suspension hook connection, realizes the connection of cabin and helicopter.
As above, wherein cabin is equipped with the second erecting by overhang, the autonomous suspension hook company of the second erecting by overhang and puffer
It connects.
As above, wherein the position of puffer is corresponding with the second erecting by overhang of cabin.
As above, wherein location identification unit includes laser positioning module and picture recognition module；Picture recognition module is used
In identification mission load whether be target object；Laser positioning module is connect with picture recognition module, for location tasks load,
The specific location of the specific location of cabin and the first and second erectings by overhang.
As above, wherein the quantity of puffer is 4.
The application has following technical effect that
(1) the automatic erecting by overhang of the helicopter of the application is connect by winch lower wire rope with mission payload, structure
It is simple to be convenient for operation, it can flexibly realize and connect and unload with hanging for mission payload.
(2) location identification unit in the automatic erecting by overhang of the helicopter of the application can identify and position mission payload,
To more accurately realize the connection with mission payload, it is accurately realized the transport of cargo
(3) the automatic erecting by overhang of the helicopter of the application, which can be realized, carries target goods in tape cabin body, in outer hanging body product
Facilitate the transport of cargo in not increased situation, stability is more preferable, and lifting capacity is stronger.
Detailed description of the invention
In order to illustrate the technical solutions in the embodiments of the present application or in the prior art more clearly, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
The some embodiments recorded in application can also be obtained according to these attached drawings other for those of ordinary skill in the art
Attached drawing.
Fig. 1 is that ground parked state provided by the present application hangs cabin schematic diagram；
Fig. 2 is that hovering state provided by the present application hangs cabin schematic diagram；
Fig. 3 is that hovering band cabin provided by the present application hangs mission payload schematic diagram；
Fig. 4 is hovering provided by the present application and hangs mission payload schematic diagram without cabin；
1-unmanned helicopter；2-cabins；3-steel wire cables；5-mission payloads；
6-big winches；7-puffers.
Specific embodiment
Below with reference to the attached drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out clear
Chu is fully described by, it is clear that the embodiments are a part of the embodiments of the present invention rather than all of the embodiments.
Based on the embodiments of the present invention, those skilled in the art are obtained all without making creative work
Other embodiments are fallen within the protection scope of the utility model.
The purpose of this utility model is to provide a kind of automatic erectings by overhang of helicopter, including carry device and position identification
Unit can be realized and mount different types of mission payload in unmanned transport helicopter, and passes through accurate Position Fixing Navigation System,
Realize loading and the unloading of mission payload.
As shown in Figure 1, the automatic erecting by overhang of helicopter includes unmanned helicopter 1, carry device and location identification unit, hang
It carries to set and be connect with location identification unit, specifically, carry device includes steel wire cable 8 and winch.
Specifically, the other end of one end of winch connecting steel wire ropes rope 3, steel wire cable 3 is equipped with autonomous suspension hook, autonomous suspension hook
It is connect with the erecting by overhang of mission payload 5.
Winch includes big winch 6 and puffer 7, and specifically, big winch 6 is mounted on helicopter center, and puffer 7 is pacified
Mounted in the head and tail portion of helicopter.First autonomous suspension hook of the steel wire cable 3 being connect with big winch 6 and 5 center of mission payload
The main hanging interface of position connects, and realizes the connection of unmanned helicopter 1 and mission payload 5.Further, it is connect with puffer 7
The second autonomous suspension hook of steel wire cable 3 connect with the erecting by overhang of 5 surrounding of mission payload, realize unmanned helicopter 1 and task
The further connection of load 5.
Preferably, mechanical arm is equipped in unmanned helicopter 1, driving unit controls the fortune of mechanical arm by location identification unit
Dynamic, mechanical arm is mounted on inside unmanned helicopter, illustratively, if the length and width of mission payload are oriented in location identification unit identification
Greater than the length and width of unmanned plane, then driving unit drives mechanical arm to extend to the outside of unmanned plane, makes the autonomous suspension hook of steel wire cable
It is docked with the matching of mission payload erecting by overhang.
Preferably, the quantity of puffer 7 is at least 4.
Location identification unit includes laser positioning module and picture recognition module, and task carries picture recognition module for identification
The target objects such as lotus 5 and cabin 2.
Laser positioning module is connect with picture recognition module, for the location tasks load after identification mission load 5 and cabin 2
The erecting by overhang of lotus 5 and cabin 2.
Illustratively, mission payload 5 can be target goods or accommodate the cabin of target goods.
Embodiment one
As one embodiment, mission payload is one.It is cabin 2 that Fig. 2 and 3, which shows mission payload,.2 center of cabin is set
There is main hanging interface, main hanging interface is connect with the first autonomous suspension hook of big winch 6, realizes the company of cabin 2 and unmanned helicopter 1
It connects.
Further, cabin 2 is surrounded by erecting by overhang, and erecting by overhang is connect with the second of puffer 7 from main hook, real
The connection of existing cabin 2 and unmanned helicopter 1.As one embodiment, Fig. 2 shows the cabin 2 of ground parked state, as appointing
Business load.It independently hangs when connecing, unmanned helicopter 1 receives loading instruction, controls the movement of mechanical arm, mechanical arm makes steel wire cable
Angular deflection occurs and then puts down steel wire cable 3 and autonomous suspension hook by cabin 2, automatic loading dress is installed inside cabin 2
It sets, by cargo automatic transportation to cabin 2, closes hatch door mouth, cabin 2 is dragged and dropped into what unmanned helicopter 1 was parked by unmanned trailer
Below the body of position, the location identification unit identification cabin 2 of unmanned helicopter 1 and the autonomous suspension hook and surrounding for positioning cabin 2
The position of erecting by overhang, determines the movement of control mechanical arm behind position, and winch puts down steel wire cable, mechanical arm clamped wire rope
To the surface with 2 erecting by overhang of cabin, docks the autonomous suspension hook of steel wire cable 3 with the matching of the erecting by overhang of cabin 2, complete
Hang termination process.Exemplary, autonomous uninstall process is opposite with autonomous loading process.
The cabin 2 when unmanned helicopter hovering state is shown such as Fig. 3, as mission payload.Specifically, cabin 2
It is loaded to designated position, designated position is docked to after the completion of loading, unmanned helicopter 1 is connected to after loading instruction in cabin 2
Top hovering, the location identification unit identification cabin 2 of unmanned helicopter 1 and the autonomous suspension hook and surrounding hanging dress for positioning cabin 2
The position set determines the movement of control mechanical arm behind position, and winch puts down steel wire cable, and mechanical arm clamped wire rope arrives and cabin
The corresponding top of 2 erecting by overhang of body docks the autonomous suspension hook of steel wire cable 3 with the matching of the erecting by overhang of cabin 2, and completion, which is hung, to be connect
Process, mechanical arm are shunk back in unmanned plane, while winch is upwards collected through steel wire cable 3 and slings cabin 2, and realization is bonded with body
It is fixedly connected.
It is target goods that Fig. 1, which shows mission payload,.Its suspending method is identical as cabin shown in Fig. 3, no longer superfluous herein
It states.
Embodiment two
As shown in figure 4, mission payload includes cabin and target goods.2 center of cabin is equipped with main hanging interface, is surrounded by
Erecting by overhang, main hanging interface are connect with the first autonomous suspension hook of big winch 6, the second autonomous extension of erecting by overhang and puffer 7
Hook connects realize the connection of cabin 2 and unmanned helicopter 1.
As another embodiment, cabin is attached by fixed form and unmanned helicopter, and connection relationship is ability
Domain well-known technique, is no longer repeated herein.
It is illustrated in figure 4 unmanned helicopter 1 and is connect with the realization of cabin 2 with the hanging of mission payload 5, specifically, band cabin 2
Unmanned helicopter 1 when hovering in the sky, open the hatch door of 2 bottom of cabin, the location identification unit of unmanned helicopter 1 identifies mesh
Mark cargo 2 simultaneously positions the autonomous suspension hook of target goods 2 and the position of surrounding erecting by overhang, determines the fortune of control mechanical arm behind position
Dynamic, winch puts down steel wire cable, and mechanical arm clamped wire rope makes steel wire to top corresponding with 2 erecting by overhang of target goods
The autonomous suspension hook of rope 3 is docked with the matching of the erecting by overhang of target goods 2, and termination process is hung in completion.
Specifically, the target goods in cabin or hung out of my cabin are loaded in transport to designated position, pass through autonomous addressing
The selected position for being suitble to launch goods and materials of landing system is launched the cabin 2 with parachute or is hung object, hovering outside extremely using aerial
Low latitude independently launches cabin 2 or object using winch mode, drops to ground dispensing cabin 2；
The application has following technical effect that
(3) the automatic erecting by overhang of the helicopter of the application is connect by winch lower wire rope with mission payload, structure
It is simple to be convenient for operation, it can flexibly realize and connect and unload with hanging for mission payload.
(4) location identification unit in the automatic erecting by overhang of the helicopter of the application can identify and position mission payload,
To more accurately realize the connection with mission payload, it is accurately realized the transport of cargo
(3) the automatic erecting by overhang of the helicopter of the application, which can be realized, carries target goods in tape cabin body, in outer hanging body product
Facilitate the transport of cargo in not increased situation, stability is more preferable, and lifting capacity is stronger.
Although the preferred embodiment of the application has been described, it is created once a person skilled in the art knows basic
Property concept, then additional changes and modifications may be made to these embodiments.So it includes excellent that the following claims are intended to be interpreted as
It selects embodiment and falls into all change and modification of the application range.Obviously, those skilled in the art can be to the application
Various modification and variations are carried out without departing from spirit and scope.If in this way, these modifications and variations of the application
Belong within the scope of the claim of this application and its equivalent technologies, then the application is also intended to encompass these modification and variations and exists
It is interior.
Claims (8)
1. a kind of automatic erecting by overhang of helicopter, which is characterized in that including carry device and location identification unit, the carry dress
It sets and is connect with the location identification unit, the carry device includes winch, one end of the winch connecting steel wire ropes rope, described
The other end of steel wire cable is equipped with autonomous suspension hook, the first erecting by overhang connection of the autonomous suspension hook and mission payload.
2. the automatic erecting by overhang of helicopter as described in claim 1, which is characterized in that mechanical arm is equipped in unmanned helicopter,
The end of the mechanical arm clamps the steel wire cable；The location identification unit is electrically connected with the mechanical arm, the position
Recognition unit controls the movement of the mechanical arm.
3. the automatic erecting by overhang of helicopter as described in claim 1, which is characterized in that the winch includes big winch and rap
Vehicle, the big winch are mounted on helicopter center.
4. the automatic erecting by overhang of helicopter as claimed in claim 3, which is characterized in that including cabin, the cabin center is set
There is main hanging interface, the main hanging interface is connect with the autonomous suspension hook of the big winch, realizes the cabin and helicopter
Connection.
5. the automatic erecting by overhang of helicopter as claimed in claim 4, which is characterized in that the cabin is equipped with the second hanging dress
It sets, second erecting by overhang is connect with the autonomous suspension hook of the puffer.
6. the automatic erecting by overhang of helicopter as claimed in claim 4, which is characterized in that the position of the puffer and the cabin
Second erecting by overhang of body is corresponding.
7. the automatic erecting by overhang of helicopter as claimed in claim 5, which is characterized in that the location identification unit includes laser
Locating module and picture recognition module；
Whether mission payload is target object to described image identification module for identification；
The laser positioning module is connect with described image identification module, for positioning the tool of the mission payload, the cabin
The specific location of body position and the first and second erectings by overhang.
8. the automatic erecting by overhang of helicopter as claimed in claim 3, which is characterized in that the quantity of the puffer is 4.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820593833.7U CN208393635U (en) | 2018-04-24 | 2018-04-24 | A kind of automatic erecting by overhang of helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820593833.7U CN208393635U (en) | 2018-04-24 | 2018-04-24 | A kind of automatic erecting by overhang of helicopter |
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| Publication Number | Publication Date |
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| CN208393635U true CN208393635U (en) | 2019-01-18 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201820593833.7U Active CN208393635U (en) | 2018-04-24 | 2018-04-24 | A kind of automatic erecting by overhang of helicopter |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111846229A (en) * | 2020-07-29 | 2020-10-30 | 中航电测仪器股份有限公司 | Unmanned automatic grabbing, hanging and transporting device and method for helicopter |
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2018
- 2018-04-24 CN CN201820593833.7U patent/CN208393635U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111846229A (en) * | 2020-07-29 | 2020-10-30 | 中航电测仪器股份有限公司 | Unmanned automatic grabbing, hanging and transporting device and method for helicopter |
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