CN205239917U - Unmanned aerial vehicle waters rescue device - Google Patents
Unmanned aerial vehicle waters rescue device Download PDFInfo
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- CN205239917U CN205239917U CN201521023778.0U CN201521023778U CN205239917U CN 205239917 U CN205239917 U CN 205239917U CN 201521023778 U CN201521023778 U CN 201521023778U CN 205239917 U CN205239917 U CN 205239917U
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- lifebuoy
- cantilever
- life buoy
- waters
- unmanned plane
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Abstract
The utility model provides an unmanned aerial vehicle waters rescue device, including ring flange and support, the ring flange is used for connecting unmanned aerial vehicle and life buoy fixing device, the lifesaving snare is put in the life buoy fixing device outside, still include life buoy input device, the life buoy is put in the device and is included the life buoy baffle, the life buoy baffle passes through the guide arm and is connected with the guide rail, return spring set is in the guide arm outside, motor stator fixed mounting is on the bottom plate, electric motor rotor installs in the motor stator below, the last cantilever of installing of electric motor rotor, the guide pulley is installed to the one end of cantilever, cantilever baffle A and cantilever baffle B install the both sides at the guide pulley respectively, life buoy fixing device installs the bottom diaxon that guides unmanned aerial vehicle flight and increases steady camera. A life buoy can accurate single be put in in the design that this unmanned aerial vehicle waters rescue device adopted the radial shrinkage of baffle to put in the life buoy, is carrying out the waters when suing and labouring, and a sortie unmanned aerial vehicle can rescue multiple targets.
Description
Technical field
The utility model belongs to unmanned plane technical field, is specifically related to a kind of unmanned plane waters deliverance apparatus.
Background technology
Along with the development of rotor wing unmanned aerial vehicle technology, unmanned plane is having pure progress aspect voyage and load-carrying, and in actual applications, unmanned plane use cost is low, and flying speed is fast, the advantage that time is short, thereby it can arrive at objective fast.
Along with scientific and technical development, at unmanned plane sciemtifec and technical sphere, the especially needs of the quick reply of applicating technology to water life-saving, because having, unmanned plane is swift in response, the advantages such as maneuverability is strong, apply more and more extensive, therefore also more and more higher to the science and technology of water life-saving requirement itself. Because water life-saving built-in problem is a kind of new requirement and thinking so find this method of unmanned plane lift-launch air life-saving device.
The mode of existing input lifebuoy is artificial input, be difficult to accurately throw, and to have many regions of need to rescuing waterborne is manually to arrive region, can not rescue in time, adopt aircraft to implement rescue cost high, and maneuverability is poor.
Also there is at present the report in the rescue of waters about unmanned plane, the Chinese patent that is CN204078071U as the patent No. discloses " a kind of unmanned plane emergency rescue device waterborne ", this device can accurately be controlled according to camera filmed image the input of lifebuoy, lifebuoy input accuracy rate is high, rescue in time, rescue efficiency is high, but this device fails to solve the problem of lifebuoy supply volume, lifebuoy can only once all be thrown in, after once all throwing in, can only again fly back after reprinting again, just can fly to other regions throws in, can not realize flight and rescue the target in multiple waters.
The patent No. is that the Chinese patent of CN204250326U discloses " a kind of unmanned plane air life-saving device ", also can realize the input of lifebuoy, but fails equally to solve the problem of lifebuoy supply volume, can not realize flight and rescue the target in multiple waters.
Utility model content
For overcoming the deficiencies in the prior art, the utility model has designed a kind of unmanned plane waters deliverance apparatus, this unmanned plane waters deliverance apparatus is a kind of lifebuoy delivery device, adopt the radial contraction of baffle plate to throw in the design of lifebuoy, accurately single is thrown in a lifebuoy, carrying out waters while suing and labouring, a sortie unmanned plane can be rescued multiple targets.
For realizing technique scheme, the utility model provides a kind of unmanned plane waters deliverance apparatus, comprise ring flange and support, described support is fixed on ring flange, ring flange is used for connecting unmanned plane and lifebuoy fixture, lifebuoy is mounted on lifebuoy fixture outside, also comprise the lifebuoy delivery device that is arranged on lifebuoy fixture lower end, described lifebuoy delivery device comprises lifebuoy baffle plate, described lifebuoy baffle plate is connected with guide rail by guide rod, back-moving spring is enclosed within guide rod outside, one end of back-moving spring is connected with fixed dam, one end is connected with guide rail in addition, motor stator is fixedly mounted on base plate, rotor is arranged on motor stator below, on described rotor, cantilever is installed, one end of described cantilever is provided with guide wheel, cantilever baffle plate A and cantilever baffle plate B are arranged on respectively the both sides of guide wheel, described lifebuoy fixture bottom is provided with guides the diaxon of unmanned plane during flying to increase steady camera.
In technique scheme, can realize being connected of this unmanned plane waters deliverance apparatus and unmanned plane by ring flange, when support can ensure that unmanned plane lands, bottom diaxon increases steady camera can not encounter ground, diaxon increases steady camera and photographic images can be passed back, operator can, according to the picture of passing back, throw in lifebuoy accurately. under normal condition, cantilever guide wheel is positioned at cantilever baffle plate B place, lifebuoy baffle plate is protruding blocks lifebuoy, in the time that needs are thrown in lifebuoy, send remote control by controller and throw in instruction, rotor rotation, cantilever guide wheel movement is to cantilever baffle plate A place, back-moving spring is upheld, guide rail is promoted to inside, guide rail inwardly pulls lifebuoy baffle plate by guide rod, lifebuoy falls, rotor rotates again afterwards, drive cantilever guide wheel movement to cantilever baffle plate B place, promoting guide rail outwards moves, thereby make the extrapolation of lifebuoy baffle plate, again stop the whereabouts of lifebuoy, rotate the time once by controlling rotor, can accurately control the time that lifebuoy baffle plate resets, and then control each rotation and just throw in a lifebuoy.
Preferably, described cantilever baffle plate B is fixedly connected with guide rail, cantilever baffle plate A and cantilever baffle plate B form two cover loops and are connected with controller with guide wheel, judge the signal of motor cantilever position as controller, when guide wheel movement is during to cantilever baffle plate A, motor stop motion, receive while again rotating task, when motor reverse rotation moves to cantilever baffle plate B, again stop the rotation, after again starting, reverse rotation again, according to this rotation repeatedly.
Preferably, described fixed dam is fixedly mounted on base plate, and the object that fixed dam is set is that a stress point is provided while stretching promotion guide rail for back-moving spring.
Preferably, have two through holes on described fixed dam, one end of guide rod is connected with guide rail through through hole.
Preferably, the picture that when described diaxon increases inner two the steady motors of increasing installing of steady camera for the medium dip of stabilized flight process, camera is taken.
Compared with prior art, the technical solution adopted in the utility model has following beneficial effect:
1) this unmanned plane waters deliverance apparatus adopts the radial contraction of baffle plate to throw in the design of lifebuoy, an accurately lifebuoy of single input, and carrying out waters while suing and labouring, a sortie unmanned plane during flying can be rescued multiple targets;
2) this unmanned plane increases steady camera by the diaxon that is arranged on its bottom, can realize the accurate delivery of lifebuoy.
Brief description of the drawings
Fig. 1 is perspective view of the present utility model.
Fig. 2 is stereochemical structure upward view of the present utility model.
Fig. 3 is the structural representation of lifebuoy delivery device in the utility model.
In figure: 1-ring flange, 2-support, 3-lifebuoy fixture, 4-lifebuoy, 5-diaxon increases steady camera, 6-lifebuoy baffle plate, 7-cantilever baffle plate A, 8-motor stator, 9-electronics rotor, 10-cantilever, 11-guide wheel, 12-cantilever baffle plate B, 13-guide rail, 14-fixed dam, 15-back-moving spring, 16-guide rod, 17-base plate.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out to clear, complete description, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiment. This area ordinary person, not making the every other embodiment obtaining under creative work prerequisite, all belongs to protection domain of the present utility model.
Embodiment: a kind of unmanned plane waters deliverance apparatus.
Shown in Fig. 3, a kind of unmanned plane waters deliverance apparatus, comprise ring flange 1 and support 2, described support 2 is fixed on ring flange 1, ring flange 1 is for connecting unmanned plane and lifebuoy fixture 3, lifebuoy 4 is mounted on lifebuoy fixture 3 outsides, also comprise the lifebuoy delivery device that is arranged on lifebuoy fixture 3 lower ends, described lifebuoy delivery device comprises lifebuoy baffle plate 6, described lifebuoy baffle plate 6 is connected with guide rail 13 by guide rod 16, back-moving spring 15 is enclosed within guide rod 16 outsides, one end of back-moving spring 15 is connected with fixed dam 14, one end is connected with guide rail 13 in addition, motor stator 8 is fixedly mounted on base plate 17, rotor 9 is arranged on motor stator 8 belows, on described rotor 9, cantilever 10 is installed, one end of described cantilever 10 is provided with guide wheel 11, cantilever baffle plate A7 and cantilever baffle plate B12 are arranged on respectively the both sides of guide wheel 11, described lifebuoy fixture 3 bottoms are provided with guides the diaxon of unmanned plane during flying to increase steady camera 5.
In the present embodiment, can realize being connected of this unmanned plane waters deliverance apparatus and unmanned plane by ring flange 1, when support 2 can ensure that unmanned plane lands, bottom diaxon increases steady camera 5 can not encounter ground, diaxon increases steady camera 5 and photographic images can be passed back, operator can, according to the picture of passing back, throw in lifebuoy 4 accurately. under normal condition, cantilever guide wheel 11 is positioned at cantilever baffle plate B12 place, lifebuoy baffle plate 6 is protruding blocks lifebuoy 4, in the time that needs are thrown in lifebuoy 4, send remote control by controller and throw in instruction, rotor 9 rotates, cantilever guide wheel 11 moves to cantilever baffle plate A7 place, back-moving spring 15 is upheld, guide rail 13 is promoted to inside, guide rail 13 inwardly pulls lifebuoy baffle plate 6 by guide rod 16, lifebuoy 4 falls, rotor 9 rotates again afterwards, drive cantilever guide wheel 11 to move to cantilever baffle plate B12 place, promoting guide rail 13 outwards moves, thereby lifebuoy baffle plate 6 is extrapolated, again stop the whereabouts of lifebuoy 4, come and go the time of rotation by controlling rotor 9, can accurately control the time that lifebuoy baffle plate 6 resets, and then control and just throw in a lifebuoy at every turn.
In the present embodiment, described cantilever baffle plate B12 is fixedly connected with guide rail 13, cantilever baffle plate A7 forms two cover loops and is connected with controller with guide wheel 11 with cantilever baffle plate B12, judge the signal of motor cantilever 10 positions as controller, in the time that guide wheel 11 moves to cantilever baffle plate A7, rotor 9 stop motions, lifebuoy baffle plate 6 shrinks, after lifebuoy 4 falls, rotor 9 rotates again, and motor reverse rotation moves to cantilever baffle plate B12 place and again stops the rotation, and lifebuoy baffle plate 6 is overhanging, next lifebuoy 4 is blocked, until again receive the next signal of throwing in.
In the present embodiment, described fixed dam 14 is fixedly mounted on base plate 7, and the object that fixed dam 14 is set is that a stress point is provided while stretching promotion guide rail 13 for back-moving spring 15.
In the present embodiment, have two through holes on described fixed dam 14, one end of guide rod 16 is connected with guide rail 13 through through hole.
In the present embodiment, the picture that when described diaxon increases inner two the steady motors of increasing installing of steady camera 5 for the medium dip of stabilized flight process, camera is taken.
The above is preferred embodiment of the present utility model; but the utility model should not be limited to this embodiment and the disclosed content of accompanying drawing; do not depart from the equivalence or the amendment that under spirit disclosed in the utility model, complete so every, all fall into the scope of the utility model protection.
Claims (5)
1. a unmanned plane waters deliverance apparatus, comprise ring flange and support, described support is fixed on ring flange, ring flange is used for connecting unmanned plane and lifebuoy fixture, lifebuoy is mounted on lifebuoy fixture outside, it is characterized in that: also comprise the lifebuoy delivery device that is arranged on lifebuoy fixture lower end, described lifebuoy delivery device comprises lifebuoy baffle plate, described lifebuoy baffle plate is connected with guide rail by guide rod, back-moving spring is enclosed within guide rod outside, one end of back-moving spring is connected with fixed dam, one end is connected with guide rail in addition, motor stator is fixedly mounted on base plate, rotor is arranged on motor stator below, on described rotor, cantilever is installed, one end of described cantilever is provided with guide wheel, cantilever baffle plate A and cantilever baffle plate B are arranged on respectively the both sides of guide wheel.
2. unmanned plane as claimed in claim 1 waters deliverance apparatus, is characterized in that: described cantilever baffle plate B is fixedly connected with guide rail.
3. unmanned plane as claimed in claim 1 waters deliverance apparatus, is characterized in that: described fixed dam is fixedly mounted on base plate.
4. unmanned plane as claimed in claim 3 waters deliverance apparatus, is characterized in that: on described fixed dam, have two through holes, one end of guide rod is connected with guide rail through through hole.
5. unmanned plane as claimed in claim 1 waters deliverance apparatus, is characterized in that: described lifebuoy fixture bottom is provided with guides the diaxon of unmanned plane during flying to increase steady camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521023778.0U CN205239917U (en) | 2015-12-11 | 2015-12-11 | Unmanned aerial vehicle waters rescue device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521023778.0U CN205239917U (en) | 2015-12-11 | 2015-12-11 | Unmanned aerial vehicle waters rescue device |
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| CN205239917U true CN205239917U (en) | 2016-05-18 |
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| CN201521023778.0U Active CN205239917U (en) | 2015-12-11 | 2015-12-11 | Unmanned aerial vehicle waters rescue device |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105416526A (en) * | 2015-12-11 | 2016-03-23 | 佛山市南海区广工大数控装备协同创新研究院 | Unmanned aerial vehicle rescue device for water area |
| CN106094857A (en) * | 2016-08-22 | 2016-11-09 | 京东方科技集团股份有限公司 | The flight control method of unmanned plane, wearable device and unmanned plane, device |
| CN106585990A (en) * | 2016-11-30 | 2017-04-26 | 湖北大秀天域科技发展有限公司 | Release device applicable to unmanned aerial vehicle |
| CN106741745A (en) * | 2016-12-31 | 2017-05-31 | 詹榆菲 | A kind of life saving system |
| CN110576971A (en) * | 2018-06-07 | 2019-12-17 | 成都天府新区光启未来技术研究院 | Throwing device applied to water rescue unmanned aerial vehicle system |
| CN113511337A (en) * | 2021-05-20 | 2021-10-19 | 华南理工大学 | Multi-material transportation aircraft and control method thereof |
| CN118419229A (en) * | 2024-07-05 | 2024-08-02 | 西安麦莎科技有限公司 | Marine unmanned aerial vehicle for throwing rescue equipment |
-
2015
- 2015-12-11 CN CN201521023778.0U patent/CN205239917U/en active Active
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105416526A (en) * | 2015-12-11 | 2016-03-23 | 佛山市南海区广工大数控装备协同创新研究院 | Unmanned aerial vehicle rescue device for water area |
| CN105416526B (en) * | 2015-12-11 | 2017-08-18 | 佛山市南海区广工大数控装备协同创新研究院 | Water area unmanned machine deliverance apparatus |
| CN106094857A (en) * | 2016-08-22 | 2016-11-09 | 京东方科技集团股份有限公司 | The flight control method of unmanned plane, wearable device and unmanned plane, device |
| CN106585990A (en) * | 2016-11-30 | 2017-04-26 | 湖北大秀天域科技发展有限公司 | Release device applicable to unmanned aerial vehicle |
| CN106585990B (en) * | 2016-11-30 | 2019-02-26 | 湖北大秀天域科技发展有限公司 | A kind of delivery device on unmanned plane |
| CN106741745A (en) * | 2016-12-31 | 2017-05-31 | 詹榆菲 | A kind of life saving system |
| CN106741745B (en) * | 2016-12-31 | 2018-06-22 | 詹榆菲 | A kind of life saving system |
| CN110576971A (en) * | 2018-06-07 | 2019-12-17 | 成都天府新区光启未来技术研究院 | Throwing device applied to water rescue unmanned aerial vehicle system |
| CN113511337A (en) * | 2021-05-20 | 2021-10-19 | 华南理工大学 | Multi-material transportation aircraft and control method thereof |
| CN118419229A (en) * | 2024-07-05 | 2024-08-02 | 西安麦莎科技有限公司 | Marine unmanned aerial vehicle for throwing rescue equipment |
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