CN204250326U - A kind of unmanned plane air life-saving device - Google Patents
A kind of unmanned plane air life-saving device Download PDFInfo
- Publication number
- CN204250326U CN204250326U CN201420509051.2U CN201420509051U CN204250326U CN 204250326 U CN204250326 U CN 204250326U CN 201420509051 U CN201420509051 U CN 201420509051U CN 204250326 U CN204250326 U CN 204250326U
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- unmanned plane
- rescue
- life
- excitor
- saving device
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Abstract
The utility model discloses a kind of unmanned plane air life-saving device, insert hanger, ejector, excitor, drag-line, pulley etc. soon by module to form, ejector, excitor, drag-line, pulley are arranged on the fast inserting or hanging member of module, excitor is connected with pulley by drag-line, and carbon dioxide canister and buoy quoit are arranged on below unmanned plane air life-saving device.The utility model is by UAV flight's mode, rescue region can be rushed in time, repeat prestowage buoy quoit quantity, buoy quoit is accurately thrown in rescuing region by sighting system, mobility strong, be swift in response, buoyant apparatus adopts from air inflator system, reliably safe and efficient, and it is low to rescue region environmental requirement, implement rescue cost low, rescue distance more than 125 times can be increased, 2.5 km are promoted to by traditional 20 meters, throw in accuracy rate and improve more than 5 times, accurate radius is brought up within 1 meter by 5 meters, using can disposable carry 4 life saving appliance from inflatable life preserver, so rescue efficiency also improves 4 times.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, particularly relates to a kind of unmanned plane air life-saving device.
Background technology
Along with the development of science and technology, at unmanned plane sciemtifec and technical sphere, especially applicating technology is to the needs of the quick reply of water life-saving, be swift in response because unmanned plane has, the advantages such as maneuverability is strong, application is more and more extensive, therefore requires also more and more higher to the science and technology of water life-saving itself.Because water life-saving built-in problem, so finding this method of UAV flight's air life-saving device is a kind of new requirement and thinking.
The mode of existing input buoy quoit is artificial input, is difficult to accurately throw, and has and manyly waterbornely need rescue region to be manually cannot arrive region, can not rescue in time, adopt aircraft to implement rescue cost high, and maneuverability be poor.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane air life-saving device, the mode being intended to solve existing input buoy quoit is artificial input, be difficult to accurately throw, and have many waterborne need rescue region be manually cannot arrive region, can not rescue in time, aircraft is adopted to implement rescue cost high, and the problem of maneuverability difference.
The utility model realizes like this, by module, slotting hanger, ejector, excitor, drag-line, pulley, carbon dioxide canister, buoy quoit form a kind of unmanned plane air life-saving device soon, described ejector, excitor, drag-line, pulley are arranged on the fast inserting or hanging member of module, excitor is connected with pulley by drag-line, and carbon dioxide canister and buoy quoit are arranged on below unmanned plane air life-saving device.
Further, excitor is actuator, and start is the ejector pulling drag-line to open to be connected between buoy quoit with hanger, by the spring in ejector, buoy quoit is ejected ejector.
effect gathers
Unmanned plane air life-saving device of the present utility model is by UAV flight's mode, rescue region can be rushed in time, repeat prestowage buoy quoit quantity, buoy quoit is accurately thrown in rescuing region by sighting system, mobility strong, be swift in response, buoyant apparatus adopts from air inflator system, reliably safe and efficient, and it is low to rescue region environmental requirement, implement rescue cost low, rescue distance more than 125 times can be increased, 2.5 km are promoted to by traditional 20 meters, throw in accuracy rate and improve more than 5 times, accurate radius is brought up within 1 meter by 5 meters, and can disposable carry 4 life saving appliance from inflatable life preserver because use, so rescue efficiency also improves 4 times.
Accompanying drawing explanation
Fig. 1 is the front view of the unmanned plane air life-saving device that the utility model embodiment provides;
Fig. 2 is the lateral plan of the unmanned plane air life-saving device that the utility model embodiment provides;
Fig. 3 is the birds-eye view of the unmanned plane air life-saving device that the utility model embodiment provides;
In figure: 1, module inserts hanger soon; 2, ejector; 3, excitor; 4, drag-line; 5, pulley; 6, carbon dioxide canister; 7, buoy quoit.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
Fig. 1-Fig. 3 shows the structure of unmanned plane air life-saving device of the present utility model, as shown in the figure, the utility model realizes like this, by module, slotting hanger 1, ejector 2, excitor 3, drag-line 4, pulley 5, carbon dioxide canister 6, buoy quoit 7 form a kind of unmanned plane air life-saving device soon, described ejector 2, excitor 3, drag-line 4, pulley 5 are arranged on the fast inserting or hanging member 1 of module, excitor 3 is connected with pulley 5 by drag-line 4, and carbon dioxide canister 6 and buoy quoit 7 are arranged on below unmanned plane air life-saving device.
Further, excitor 3 is actuator, and start pulls drag-line 4 to open buoy quoit 7 and the ejector 2 be connected between hanger, by the spring in ejector 2, buoy quoit 7 ejected ejector 2.
Neighbour's target to be rescued is flown by unmanned plane carry life saving system, ground handling operator sends firing command at a distance by telecommand equipment, unmanned plane to receive after signal by excitor 3 ejection survival circle 7, pulls open carbon dioxide canister 6 simultaneously and inflates to buoy quoit 7, reach the object of relief target.
Unmanned plane air life-saving device of the present utility model is by UAV flight's mode, rescue region can be rushed in time, repeat prestowage buoy quoit quantity, buoy quoit is accurately thrown in rescuing region by sighting system, mobility strong, be swift in response, buoyant apparatus adopts from air inflator system, reliably safe and efficient, and it is low to rescue region environmental requirement, implement rescue cost low, rescue distance more than 125 times can be increased, 2.5 km are promoted to by traditional 20 meters, throw in accuracy rate and improve more than 5 times, accurate radius is brought up within 1 meter by 5 meters, and can disposable carry 4 life saving appliance from inflatable life preserver because use, so rescue efficiency also improves 4 times.
By reference to the accompanying drawings detailed description of the invention of the present utility model is described although above-mentioned; but the restriction not to the utility model protection domain; one of ordinary skill in the art should be understood that; on the basis of the technical solution of the utility model, those skilled in the art do not need to pay various amendment or distortion that performing creative labour can make still within protection domain of the present utility model.
Claims (2)
1. a unmanned plane air life-saving device, it is characterized in that, by module, slotting hanger, ejector, excitor, drag-line, pulley, carbon dioxide canister, buoy quoit form described unmanned plane air life-saving device soon, described ejector, excitor, drag-line, pulley are arranged on the fast inserting or hanging member of module, excitor is connected with pulley by drag-line, and carbon dioxide canister and buoy quoit are arranged on below unmanned plane air life-saving device.
2. unmanned plane air life-saving device as claimed in claim 1, it is characterized in that, excitor is actuator.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420509051.2U CN204250326U (en) | 2014-09-05 | 2014-09-05 | A kind of unmanned plane air life-saving device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420509051.2U CN204250326U (en) | 2014-09-05 | 2014-09-05 | A kind of unmanned plane air life-saving device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204250326U true CN204250326U (en) | 2015-04-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420509051.2U Expired - Fee Related CN204250326U (en) | 2014-09-05 | 2014-09-05 | A kind of unmanned plane air life-saving device |
Country Status (1)
| Country | Link |
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| CN (1) | CN204250326U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106864698A (en) * | 2017-03-08 | 2017-06-20 | 深圳市雷凌广通技术研发有限公司 | A kind of intelligent unmanned machine for succouring drowning person |
| CN107907889A (en) * | 2017-12-25 | 2018-04-13 | 成都壹橙科技有限公司 | A kind of deliverance apparatus based on unmanned plane |
| CN107902056A (en) * | 2017-11-24 | 2018-04-13 | 陆汉明 | A kind of Intelligent lifesaving circle release device |
| CN109850095A (en) * | 2017-07-16 | 2019-06-07 | 郑州国知网络技术有限公司 | Rescue mode and its system under a kind of intelligent water based on unmanned plane |
| CN110001889A (en) * | 2019-04-26 | 2019-07-12 | 大庆九州维安科技有限公司 | A kind of more crowd's body rescue systems waterborne based on unmanned plane |
| WO2022037043A1 (en) * | 2020-08-21 | 2022-02-24 | 南京灵雀智能制造有限公司 | Long-distance throw device applicable to aquatic robot, robot, and operation method |
| WO2022037042A1 (en) * | 2020-08-21 | 2022-02-24 | 南京灵雀智能制造有限公司 | Buoyancy constraint device suitable for water first-aid robot, first-aid robot, and working method |
-
2014
- 2014-09-05 CN CN201420509051.2U patent/CN204250326U/en not_active Expired - Fee Related
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106864698A (en) * | 2017-03-08 | 2017-06-20 | 深圳市雷凌广通技术研发有限公司 | A kind of intelligent unmanned machine for succouring drowning person |
| CN109850095A (en) * | 2017-07-16 | 2019-06-07 | 郑州国知网络技术有限公司 | Rescue mode and its system under a kind of intelligent water based on unmanned plane |
| CN109850095B (en) * | 2017-07-16 | 2020-11-17 | 广东德九新能源有限公司 | Intelligent underwater rescue method and system based on unmanned aerial vehicle |
| CN107902056A (en) * | 2017-11-24 | 2018-04-13 | 陆汉明 | A kind of Intelligent lifesaving circle release device |
| CN107902056B (en) * | 2017-11-24 | 2021-01-22 | 陆汉明 | Intelligent life buoy releasing device |
| CN107907889A (en) * | 2017-12-25 | 2018-04-13 | 成都壹橙科技有限公司 | A kind of deliverance apparatus based on unmanned plane |
| CN110001889A (en) * | 2019-04-26 | 2019-07-12 | 大庆九州维安科技有限公司 | A kind of more crowd's body rescue systems waterborne based on unmanned plane |
| CN110001889B (en) * | 2019-04-26 | 2023-09-22 | 大庆九州维安科技有限公司 | Unmanned aerial vehicle-based water multi-crowd rescue system |
| WO2022037043A1 (en) * | 2020-08-21 | 2022-02-24 | 南京灵雀智能制造有限公司 | Long-distance throw device applicable to aquatic robot, robot, and operation method |
| WO2022037042A1 (en) * | 2020-08-21 | 2022-02-24 | 南京灵雀智能制造有限公司 | Buoyancy constraint device suitable for water first-aid robot, first-aid robot, and working method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| DD01 | Delivery of document by public notice |
Addressee: Xu Weijia Document name: Notification of Passing Examination on Formalities |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160627 Address after: 067000 Hebei city of Chengde province high tech Zone Yudu Phoenix sixth unit 2 Building No. 303 Patentee after: Chengde Eagle Shield Trading Co.,Ltd. Address before: Songzhangzi village Songzhangzi town 122524 Liaoning city in Lingyuan Province, a group of 9591 Patentee before: Xu Weijia |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160816 Address after: 067000 Chengde Development Zone, Hebei science and technology building, annex floor, floor 12 Patentee after: Chengde Eagle Electronic Technology Co.,Ltd. Address before: 067000 Hebei city of Chengde province high tech Zone Yudu Phoenix sixth unit 2 Building No. 303 Patentee before: Chengde Eagle Shield Trading Co.,Ltd. |
|
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 067000 Chengde Development Zone, Hebei science and technology building, annex floor, floor 12 Patentee after: HAWK EYE TECHNOLOGY CO.,LTD. Address before: 067000 Chengde Development Zone, Hebei science and technology building, annex floor, floor 12 Patentee before: Chengde Eagle Electronic Technology Co.,Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150408 Termination date: 20210905 |