CN106314694A - Unmanned-water-surface-aircraft recovering and deploying device - Google Patents
Unmanned-water-surface-aircraft recovering and deploying device Download PDFInfo
- Publication number
- CN106314694A CN106314694A CN201610858470.0A CN201610858470A CN106314694A CN 106314694 A CN106314694 A CN 106314694A CN 201610858470 A CN201610858470 A CN 201610858470A CN 106314694 A CN106314694 A CN 106314694A
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- China
- Prior art keywords
- hammer
- water surface
- aircraft
- unmanned water
- unmanned
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B27/00—Arrangement of ship-based loading or unloading equipment for cargo or passengers
- B63B27/10—Arrangement of ship-based loading or unloading equipment for cargo or passengers of cranes
-
- B63B2734/00—
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
The invention relates to the technical field of automatic machine recovering and deploying devices, in particular to an unmanned-water-surface-aircraft recovering and deploying device. The unmanned-water-surface-aircraft recovering and deploying device comprises a lifting-machine hooking module and an unmanned-water-surface-aircraft hanging hammer module. The lifting-machine hooking module comprises a bearing mechanism, a conical hanging-hammer receiver and hanging-hammer licking devices, the conical hanging-hammer receiver is arranged at the lower end of the bearing mechanism, and the hanging-hammer locking devices are installed on the two sides of the bearing mechanism and located at the upper end of the conical hanging-hammer receiver; the unmanned-water-surface-aircraft hanging hammer module comprises a lifting hanging head and a conical hammer arranged at the lower end of the lifting hanging head, and the conical hammer is matched with the conical hanging-hammer receiver. As the unmanned-water-surface-aircraft recovering and deploying device is provided with a lifting-hammer receiving device, labors do not need to permit lifting operation on an unmanned water surface aircraft, the connection accuracy of the lifting hammer and the lifting hammer receiver is greatly increased, time is saved, and the lifting cost is reduced.
Description
Technical field
The present invention relates to machine automatization folding and unfolding equipment technology field, particularly relate to unmanned water surface aircraft draw off gear.
Background technology
Although present stage unmanned water surface aircraft can independently return lash ship, but reclaimer is sufficiently complex.Traditional recovery
Mode has two kinds: cage reclaims and guide tracked recovery.Cage recovery is the size of the unmanned water surface aircraft reclaimed as required
Doing a specific cage, during recovery, transfer cage and open to cage to the water surface, unmanned water surface aircraft, hydraulic wireline winch will hang
Cage is sling；Guide tracked recovery is to utilize the hooking device carried on unmanned boat, carries out hook behaviour under operator on unmanned boat
Make.Cage reclaims shortcoming: being required for specific unmanned boat and do specific cage, cost is high, and when unmanned boat enters cage, behaviour's ship is difficult
Degree height, is easily damaged the underwater sound equipment of boat bottom.Guide tracked recovery shortcoming: installing guide rail needs lash ship is carried out bigger changing
Making, increase difficulty, receiving ship time needs personnel to link up with to unmanned boat, and difficulty is big, and operation on the sea is dangerous big.
Lack one on the market to reclaim and need not manually carry out in unmanned water surface aircraft by Quick distributor
Draw off gear that link up with operation, that unmanned water surface aircraft construction is not caused damage.
Summary of the invention
The technical problem to be solved in the present invention is how to overcome the deficiencies in the prior art, it is provided that a kind of unmanned water surface aircraft
Draw off gear.
The present invention the technical scheme is that unmanned water surface aircraft draw off gear for achieving the above object, including loop wheel machine
Hooking module and unmanned water surface aircraft hang hammer module, and described loop wheel machine Hooking module includes that hammer receptor hung by support mechanism, taper
Hammering locking device into shape with hanging, described taper is hung hammer receptor and is arranged on the lower end of described support mechanism, described extension hammer locking device peace
Being contained in described support mechanism both sides, be positioned at described taper and hang the upper end of hammer receptor, unmanned water surface aircraft is hung hammer module and is included
Hanging head and the taper drift being arranged on hanging head lower end, described taper drift and described taper are hung hammer receptor and are matched.
Further, described taper is hung the upper end of hammer receptor and is provided with through hole, and described through hole can be by described hanging head.
Further, the material of described support mechanism is I-steel, uses I steel composite to become cuboid framework.
Further, the inside of described support mechanism is additionally provided with taper and hangs hammer position-detection sensor.
Further, present invention additionally comprises electrical system module and rope bucket, told electrical system module is linked up with described loop wheel machine
Module is connected, and the control for described unmanned water surface aircraft and loop wheel machine Hooking module operates.
Further, described rope bucket is positioned in unmanned water surface aircraft and is positioned at described unmanned water surface aircraft extension hammer module
Side
It is an advantage of the current invention that being provided with sash weight receives device, it is not necessary to manually lift in unmanned water surface aircraft
Operation, has been significantly greatly increased the accuracy that sash weight is connected with sash weight receptor, saves the time and lifting cost is used.
Accompanying drawing explanation
Fig. 1 overall structure of the present invention schematic diagram.
Fig. 2 unmanned water surface of the present invention aircraft hangs hammer module diagram.
Detailed description of the invention
Unmanned water surface aircraft draw off gear, hangs hammer module 2, institute including loop wheel machine Hooking module 1 and unmanned water surface aircraft
Stating loop wheel machine Hooking module 1 and include that support mechanism 11, taper are hung hammer receptor 12 and hang hammer locking device 13, described taper is hung hammer and is connect
Receiving device 12 and be fixedly connected on the lower end of described support mechanism 11, described extension hammer locking device 13 is arranged on described support mechanism 11 liang
Side, is positioned at described taper and hangs the upper end of hammer receptor 12, and unmanned water surface aircraft is hung hammer module 2 and included hanging 21 and install solid
Being scheduled on the taper drift 22 of hanging 21 lower end, described taper drift 22 and described taper are hung hammer receptor 12 and are matched.
Described taper is hung the upper end of hammer receptor 12 and is provided with through hole, and described through hole can be by described hanging 21.
The material of described support mechanism 11 is I-steel, uses I steel composite to become cuboid framework.
The inside of described support mechanism 11 is additionally provided with taper and hangs hammer position-detection sensor 111, hangs hammer when monitoring taper
When having hanging head in receptor through through hole thereon, it is signaled to hang hammer locking device, hanging head is carried out locking operation.
Present invention additionally comprises electrical system module and rope bucket, described electrical system module and described loop wheel machine Hooking module 1 phase
Even, the control for described unmanned water surface aircraft and loop wheel machine Hooking module 1 operates.
Described rope bucket is positioned in unmanned water surface aircraft and is positioned at described unmanned water surface aircraft and hangs the side of hammer module 2,
In order to deposit one end and be fixedly connected on taper drift 22 bottom surface, the other end is fastened on the cable in unmanned water surface aircraft,
During so that unmanned water surface aircraft extension hammer module 2 is lifted by crane, it is possible to drive unmanned water surface aircraft by cable.
The present invention is to utilize taper to hang hammer receptor 12 to hang the taper matched in hammer module 2 with unmanned water surface aircraft
Lifting components, improve and capture success rate, first taper is hung hammer receptor 12 and hangs hammer mould near unmanned water surface aircraft
Block 2, owing to taper extension hammer receptor 12 is in inverted cone, can extract with its hanging 21 extracting small volume in high degree raising
Success rate, after hanging 21 success extracted by taper extension hammer receptor 12, progressively declines, until hanging 21 passes and is arranged on cone
Shape hangs the through hole of hammer receptor 12 upper end, is then hung hammer position-detection sensor 111 by taper and carries out position detection, sends finger
Order, is made extension hammer locking device 13 locking hanging head, finally, is lifted by crane by the hanging device on lash ship, complete unmanned water surface navigation
The recovery operation of device.
Unmanned water surface aircraft to lay work process contrary with recovery operation engineering.
Above-described embodiment simply to illustrate that the technology design of the present invention and feature, its objective is to be to allow in this area
Those of ordinary skill will appreciate that present disclosure and implements according to this, can not limit the scope of the invention with this.All
It is the change according to the equivalence done by the essence of present invention or modification, all should contain within the scope of the present invention.
Claims (6)
1. unmanned water surface aircraft draw off gear, it is characterised in that: include that loop wheel machine Hooking module and unmanned water surface aircraft hang hammer
Module, described loop wheel machine Hooking module includes that support mechanism, taper are hung hammer receptor and hang hammer locking device, and described taper is hung hammer and connect
Receiving device and be arranged on the lower end of described support mechanism, described extension hammer locking device is arranged on described support mechanism both sides, is positioned at described
The upper end of hammer receptor is hung in taper, and unmanned water surface aircraft is hung hammer module and included hanging head and being arranged on the taper of hanging head lower end
Hammer, described taper drift and described taper are hung hammer receptor and are matched.
Unmanned water surface aircraft draw off gear the most according to claim 1, it is characterised in that: hammer receptor is hung in described taper
Upper end be provided with through hole, described through hole can be by described hanging head.
Unmanned water surface aircraft draw off gear the most according to claim 1, it is characterised in that: the material of described support mechanism
For I-steel, I steel composite is used to become cuboid framework.
Unmanned water surface aircraft draw off gear the most according to claim 1, it is characterised in that: the inside of described support mechanism
It is additionally provided with taper and hangs hammer position-detection sensor.
Unmanned water surface aircraft draw off gear the most according to claim 1, it is characterised in that: also include electrical system module
With rope bucket, told electrical system module is connected with described loop wheel machine Hooking module, for described unmanned water surface aircraft and loop wheel machine
The control operation of Hooking module.
Unmanned water surface aircraft draw off gear the most according to claim 5, it is characterised in that: described rope bucket is positioned at unmanned water
In the aircraft of face and be positioned at described unmanned water surface aircraft hang hammer module side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610858470.0A CN106314694A (en) | 2016-09-28 | 2016-09-28 | Unmanned-water-surface-aircraft recovering and deploying device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610858470.0A CN106314694A (en) | 2016-09-28 | 2016-09-28 | Unmanned-water-surface-aircraft recovering and deploying device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106314694A true CN106314694A (en) | 2017-01-11 |
Family
ID=57820215
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610858470.0A Pending CN106314694A (en) | 2016-09-28 | 2016-09-28 | Unmanned-water-surface-aircraft recovering and deploying device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106314694A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3250563A (en) * | 1964-10-02 | 1966-05-10 | Breeze Corp | Cargo hook |
| US3445133A (en) * | 1967-04-10 | 1969-05-20 | Bucyrus Erie Co | Hoist line hook |
| US20070222244A1 (en) * | 2006-03-22 | 2007-09-27 | Cornwell Carl R | Latching apparatus and method |
| CN203581349U (en) * | 2013-11-30 | 2014-05-07 | 中国科学院沈阳自动化研究所 | Recovery system of autonomous underwater vehicle |
| CN104903187A (en) * | 2013-01-04 | 2015-09-09 | 哈尔肯有限公司 | Hoisting system and accompanying connector catch assembly |
| CN105620676A (en) * | 2016-02-03 | 2016-06-01 | 青岛远创机器人自动化有限公司 | Unmanned surface vehicle collecting and releasing device |
| CN105711749A (en) * | 2016-02-03 | 2016-06-29 | 青岛远创机器人自动化有限公司 | Unmanned surface vehicle laying and retrieving method |
-
2016
- 2016-09-28 CN CN201610858470.0A patent/CN106314694A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3250563A (en) * | 1964-10-02 | 1966-05-10 | Breeze Corp | Cargo hook |
| US3445133A (en) * | 1967-04-10 | 1969-05-20 | Bucyrus Erie Co | Hoist line hook |
| US20070222244A1 (en) * | 2006-03-22 | 2007-09-27 | Cornwell Carl R | Latching apparatus and method |
| CN104903187A (en) * | 2013-01-04 | 2015-09-09 | 哈尔肯有限公司 | Hoisting system and accompanying connector catch assembly |
| CN203581349U (en) * | 2013-11-30 | 2014-05-07 | 中国科学院沈阳自动化研究所 | Recovery system of autonomous underwater vehicle |
| CN105620676A (en) * | 2016-02-03 | 2016-06-01 | 青岛远创机器人自动化有限公司 | Unmanned surface vehicle collecting and releasing device |
| CN105711749A (en) * | 2016-02-03 | 2016-06-29 | 青岛远创机器人自动化有限公司 | Unmanned surface vehicle laying and retrieving method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170111 |
|
| RJ01 | Rejection of invention patent application after publication |