CN105958627A - Shipborne unmanned aerial vehicle power supply system - Google Patents
Shipborne unmanned aerial vehicle power supply system Download PDFInfo
- Publication number
- CN105958627A CN105958627A CN201610501901.8A CN201610501901A CN105958627A CN 105958627 A CN105958627 A CN 105958627A CN 201610501901 A CN201610501901 A CN 201610501901A CN 105958627 A CN105958627 A CN 105958627A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- post
- supply system
- energy conversion
- unmanned plane
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000006243 chemical reaction Methods 0.000 claims abstract description 19
- 241000883990 Flabellum Species 0.000 claims description 14
- 238000009413 insulation Methods 0.000 claims description 14
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 239000011701 zinc Substances 0.000 claims description 3
- 229910052725 zinc Inorganic materials 0.000 claims description 3
- 230000002035 prolonged effect Effects 0.000 abstract 1
- 230000005611 electricity Effects 0.000 description 5
- 239000013535 sea water Substances 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 208000035473 Communicable disease Diseases 0.000 description 1
- 102000010029 Homer Scaffolding Proteins Human genes 0.000 description 1
- 108010077223 Homer Scaffolding Proteins Proteins 0.000 description 1
- 241001465754 Metazoa Species 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other DC sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other DC sources, e.g. providing buffering with light sensitive cells
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/14—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle
- H02J7/1415—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle with a generator driven by a prime mover other than the motor of a vehicle
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
- Secondary Cells (AREA)
Abstract
The invention discloses a shipborne unmanned aerial vehicle power supply system, which comprises a machine body, wherein a charging slot is arranged in the bottom part of the machine body; a waterproof base is arranged at the top part of the inner wall of the charging slot; a telescopic motor is arranged in the waterproof base; an output shaft of the telescopic motor is connected with an insulating plate; the insulating plate is arranged below the waterproof base; a positive post and a negative post are arranged at two sides of the bottom part of the insulating plate respectively and are connected with binding posts; a placement cavity is arranged in the machine body; an energy conversion control device and a storage battery pack are arranged in the placement cavity; the energy conversion control device is connected with the storage battery pack; the storage battery pack is connected with the positive post and the negative post through the binding posts; and a solar panel is arranged at the top part of the machine body and is connected with the energy conversion control device. The charging target is achieved by multiple means; the battery life of an unmanned aerial vehicle is prolonged; and the shipborne unmanned aerial vehicle power supply system is simple in structure, convenient to use and low in cost.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, particularly relate to a kind of boat-carrying unmanned plane power-supply system.
Background technology
UAV is called for short " unmanned plane ", is the most manned aircraft of the presetting apparatus manipulation utilizing radio robot with providing for oneself；Unmanned plane presses application, can be divided into military and civilian, military aspect, unmanned plane is divided into reconnaissance plane and target drone, at present taking photo by plane, agricultural, plant protection, auto heterodyne, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, the application in manufacture romance etc. field, greatly having expanded the purposes of unmanned plane itself, developed country is also at actively extension sector application and development unmanned air vehicle technique.
Boat-carrying unmanned plane is that the existing most flying power of boat-carrying unmanned plane is not enough for marine life is searched homer, it is impossible to enough utilizing various ways to be charged accumulation of energy when the task of execution, range is less.
Summary of the invention
The invention aims to solve shortcoming present in prior art, and a kind of boat-carrying unmanned plane power-supply system proposed.
To achieve these goals, present invention employs following technical scheme:
nullA kind of boat-carrying unmanned plane power-supply system，Including fuselage，Described fuselage bottom is provided with charging slot，The inwall top of described charging slot is provided with waterproof seat，It is provided with telescope motor in described waterproof seat，The output shaft of described telescope motor connects insulation board，Described insulation board is positioned at the underface of waterproof seat，And the two bottom sides of insulation board is respectively equipped with positive terminal and negative terminal，Described positive terminal and negative terminal are respectively connected with binding post，It is provided with placed cavity in described fuselage，It is provided with energy conversion in described placed cavity and controls device and accumulator battery，Described energy conversion controls device and is connected with accumulator battery，Described accumulator battery is connected with positive terminal and negative terminal respectively by binding post，The top of described fuselage is provided with solar energy electroplax，Described solar energy electroplax controls device with energy conversion and is connected，The both sides of described fuselage are equipped with connection post，Described connection post is provided with Rotational Cylindrical away from one end of fuselage，Described Rotational Cylindrical is rotationally connected with being connected post，And Rotational Cylindrical is provided with flabellum，Described Rotational Cylindrical is provided with actuating device，It is provided with microgenerator in described fuselage，Described microgenerator is connected with Rotational Cylindrical by actuating device，And microgenerator controls device with energy conversion and is connected.
Preferably, described positive terminal is copper post, and negative terminal is zinc post or aluminum post.
Preferably, the corner, top of described fuselage is all horizontally arranged with support column, described support column is provided with fixing seat away from the top, one end of fuselage, it is provided with micro machine in described fixing seat, the output shaft of described micro machine connects rotation bar, rotating bar and be provided with lifting flabellum, lifting flabellum is positioned at the surface of fixing seat, and micro machine controls device with energy conversion and is connected.
Preferably, the positive pole of described accumulator battery is connected with positive terminal by binding post, and the negative pole of accumulator battery is connected with negative terminal by binding post.
In the present invention, this boat-carrying unmanned plane power-supply system can drive insulation board to move up and down by telescope motor, thus drive positive terminal and negative terminal to move up and down, positive terminal and negative terminal are all connected with sea water, accumulator battery can be charged, electric energy can be converted the solar into by solar energy electroplax, it is stored in accumulator battery, improve the flying power of unmanned plane, Rotational Cylindrical can be driven to rotate when unmanned plane runs by flabellum, Rotational Cylindrical can drive microgenerator to generate electricity by actuating device, accumulator battery is charged, the present invention uses multiple means to reach the purpose of charging, improve the flying power of unmanned plane, simple in construction, easy to use, low cost.
Accompanying drawing explanation
Fig. 1 is the structural representation of a kind of boat-carrying unmanned plane power-supply system that the present invention proposes.
In figure: 1 fuselage, 2 charging slots, 3 waterproof seat, 4 telescope motor, 5 insulation boards, 6 positive terminals, 7 negative terminals, 8 binding posts, 9 placed cavities, 10 solar energy electroplaxs, 11 flabellums, 12 actuating devices.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is clearly and completely described, it is clear that described embodiment is only a part of embodiment of the present invention rather than whole embodiments.
nullWith reference to Fig. 1，A kind of boat-carrying unmanned plane power-supply system，Including fuselage 1，Charging slot 2 it is provided with bottom fuselage 1，The inwall top of charging slot 2 is provided with waterproof seat 3，Telescope motor 4 it is provided with in waterproof seat 3，The output shaft of telescope motor 4 connects insulation board 5，Insulation board 5 is positioned at the underface of waterproof seat 3，And the two bottom sides of insulation board 5 is respectively equipped with positive terminal 6 and negative terminal 7，Positive terminal 6 and negative terminal 7 are respectively connected with binding post 8，Placed cavity 9 it is provided with in fuselage 1，It is provided with energy conversion in placed cavity 9 and controls device and accumulator battery，Energy conversion controls device and is connected with accumulator battery，Accumulator battery is connected with positive terminal 6 and negative terminal 7 respectively by binding post 8，The top of fuselage 1 is provided with solar energy electroplax 10，Solar energy electroplax 10 controls device with energy conversion and is connected，The both sides of fuselage 1 are equipped with connection post，Connection post is provided with Rotational Cylindrical away from one end of fuselage 1，Rotational Cylindrical is rotationally connected with being connected post，And Rotational Cylindrical is provided with flabellum 11，Rotational Cylindrical is provided with actuating device 12，It is provided with microgenerator in fuselage 1，Microgenerator is connected with Rotational Cylindrical by actuating device 12，And microgenerator controls device with energy conversion and is connected，This boat-carrying unmanned plane power-supply system can drive insulation board 5 to move up and down by telescope motor 4，Thus drive positive terminal 6 and negative terminal 7 to move up and down，Positive terminal 6 and negative terminal 7 are all connected with sea water，Accumulator battery can be charged，Electric energy can be converted the solar into by solar energy electroplax 10，It is stored in accumulator battery，Improve the flying power of unmanned plane，Rotational Cylindrical can be driven to rotate when unmanned plane runs by flabellum 11，Rotational Cylindrical can drive microgenerator to generate electricity by actuating device 12，Accumulator battery is charged，The present invention uses multiple means to reach the purpose of charging，Improve the flying power of unmanned plane，Simple in construction，Easy to use，Low cost.
nullIn the present invention，Positive terminal 6 is copper post，And negative terminal 7 is zinc post or aluminum post，The corner, top of fuselage 1 is all horizontally arranged with support column，Support column is provided with fixing seat away from the top, one end of fuselage 1，It is provided with micro machine in fixing seat，The output shaft of micro machine connects rotation bar，Rotate bar and be provided with lifting flabellum，Lifting flabellum is positioned at the surface of fixing seat，And micro machine controls device with energy conversion and is connected，The positive pole of accumulator battery is connected with positive terminal 6 by binding post 8，And the negative pole of accumulator battery is connected with negative terminal 7 by binding post 8，This boat-carrying unmanned plane power-supply system can drive insulation board 5 to move up and down by telescope motor 4，Thus drive positive terminal 6 and negative terminal 7 to move up and down，Positive terminal 6 and negative terminal 7 are all connected with sea water，Accumulator battery can be charged，Electric energy can be converted the solar into by solar energy electroplax 10，It is stored in accumulator battery，Improve the flying power of unmanned plane，Rotational Cylindrical can be driven to rotate when unmanned plane runs by flabellum 11，Rotational Cylindrical can drive microgenerator to generate electricity by actuating device 12，Accumulator battery is charged，The present invention uses multiple means to reach the purpose of charging，Improve the flying power of unmanned plane，Simple in construction，Easy to use，Low cost.
In the present invention, when unmanned plane performs task, solar energy electroplax 10 is continual converts the solar into electric energy, then control device through energy conversion and be stored in accumulator battery, air-flow drives flabellum 11 to rotate simultaneously, thus drive Rotational Cylindrical to rotate, Rotational Cylindrical rotates and drives microgenerator to generate electricity through actuating device 12, the electric power that microgenerator produces is stored in accumulator battery, unmanned plane is when the flight of sea, telescope motor 4 promotes insulation board 5 to move down, so that positive terminal 6 and negative terminal 7 move down, with contact with sea water, produce electricity, it is stored in accumulator battery, improve the flying power of unmanned plane.
The above; it is only the present invention preferably detailed description of the invention; but protection scope of the present invention is not limited thereto; any those familiar with the art is in the technical scope that the invention discloses; according to technical scheme and inventive concept equivalent or change in addition thereof, all should contain within protection scope of the present invention.
Claims (4)
- null1. a boat-carrying unmanned plane power-supply system，Including fuselage (1)，It is characterized in that，Described fuselage (1) bottom is provided with charging slot (2)，The inwall top of described charging slot (2) is provided with waterproof seat (3)，Telescope motor (4) it is provided with in described waterproof seat (3)，The output shaft of described telescope motor (4) connects insulation board (5)，Described insulation board (5) is positioned at the underface of waterproof seat (3)，And the two bottom sides of insulation board (5) is respectively equipped with positive terminal (6) and negative terminal (7)，Described positive terminal (6) and negative terminal (7) are respectively connected with binding post (8)，Placed cavity (9) it is provided with in described fuselage (1)，It is provided with energy conversion in described placed cavity (9) and controls device and accumulator battery，Described energy conversion controls device and is connected with accumulator battery，Described accumulator battery is connected with positive terminal (6) and negative terminal (7) respectively by binding post (8)，The top of described fuselage (1) is provided with solar energy electroplax (10)，Described solar energy electroplax (10) controls device with energy conversion and is connected，The both sides of described fuselage (1) are equipped with connection post，Described connection post is provided with Rotational Cylindrical away from one end of fuselage (1)，Described Rotational Cylindrical is rotationally connected with being connected post，And Rotational Cylindrical is provided with flabellum (11)，Described Rotational Cylindrical is provided with actuating device (12)，Described fuselage is provided with microgenerator in (1)，Described microgenerator is connected with Rotational Cylindrical by actuating device (12)，And microgenerator controls device with energy conversion and is connected.
- A kind of boat-carrying unmanned plane power-supply system the most according to claim 1, it is characterised in that described positive terminal (6) is copper post, and negative terminal (7) is zinc post or aluminum post.
- A kind of boat-carrying unmanned plane power-supply system the most according to claim 1, it is characterized in that, the corner, top of described fuselage (1) is all horizontally arranged with support column, described support column is provided with fixing seat away from the top, one end of fuselage (1), being provided with micro machine in described fixing seat, the output shaft of described micro machine connects rotation bar, rotates bar and is provided with lifting flabellum, lifting flabellum is positioned at the surface of fixing seat, and micro machine controls device with energy conversion and is connected.
- A kind of boat-carrying unmanned plane power-supply system the most according to claim 1, it is characterised in that the positive pole of described accumulator battery is connected with positive terminal (6) by binding post (8), and the negative pole of accumulator battery is connected with negative terminal (7) by binding post (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610501901.8A CN105958627A (en) | 2016-06-30 | 2016-06-30 | Shipborne unmanned aerial vehicle power supply system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610501901.8A CN105958627A (en) | 2016-06-30 | 2016-06-30 | Shipborne unmanned aerial vehicle power supply system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105958627A true CN105958627A (en) | 2016-09-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610501901.8A Pending CN105958627A (en) | 2016-06-30 | 2016-06-30 | Shipborne unmanned aerial vehicle power supply system |
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| Country | Link |
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| CN (1) | CN105958627A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106864699A (en) * | 2017-01-20 | 2017-06-20 | 青岛滨海学院 | A kind of maritime search and rescue device and rescue method |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101435409A (en) * | 2007-11-16 | 2009-05-20 | 唐小岚 | Environment protection type renewable energy source power conversion machine |
| CN101451501A (en) * | 2007-12-05 | 2009-06-10 | 王德恒 | Motor vehicle system driven by wind power |
| CN102185528A (en) * | 2011-05-10 | 2011-09-14 | 北京航空航天大学 | Heat control system and method with complementary solar energy and temperature difference energy applicable to long-endurance aircraft |
| JP2014110719A (en) * | 2012-12-04 | 2014-06-12 | Toyobo Co Ltd | Unmanned work device system |
| CN104290907A (en) * | 2014-10-15 | 2015-01-21 | 西南科技大学 | Novel hybrid vertical/short take-off and landing (V/STOL) unmanned aerial vehicle |
| US20160001883A1 (en) * | 2014-07-02 | 2016-01-07 | Skycatch, Inc. | Unmanned aerial vehicle landing interface |
| US20160011592A1 (en) * | 2013-02-28 | 2016-01-14 | Identified Technologies Corporation | Methods and Apparatus for Persistent Deployment of Aerial Vehicles |
| CN105270627A (en) * | 2015-10-27 | 2016-01-27 | 深圳市飞研智能科技有限公司 | Two-unmanned-aircraft system capable of being charged in air and improving endurance capability |
-
2016
- 2016-06-30 CN CN201610501901.8A patent/CN105958627A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101435409A (en) * | 2007-11-16 | 2009-05-20 | 唐小岚 | Environment protection type renewable energy source power conversion machine |
| CN101451501A (en) * | 2007-12-05 | 2009-06-10 | 王德恒 | Motor vehicle system driven by wind power |
| CN102185528A (en) * | 2011-05-10 | 2011-09-14 | 北京航空航天大学 | Heat control system and method with complementary solar energy and temperature difference energy applicable to long-endurance aircraft |
| JP2014110719A (en) * | 2012-12-04 | 2014-06-12 | Toyobo Co Ltd | Unmanned work device system |
| US20160011592A1 (en) * | 2013-02-28 | 2016-01-14 | Identified Technologies Corporation | Methods and Apparatus for Persistent Deployment of Aerial Vehicles |
| US20160001883A1 (en) * | 2014-07-02 | 2016-01-07 | Skycatch, Inc. | Unmanned aerial vehicle landing interface |
| CN104290907A (en) * | 2014-10-15 | 2015-01-21 | 西南科技大学 | Novel hybrid vertical/short take-off and landing (V/STOL) unmanned aerial vehicle |
| CN105270627A (en) * | 2015-10-27 | 2016-01-27 | 深圳市飞研智能科技有限公司 | Two-unmanned-aircraft system capable of being charged in air and improving endurance capability |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN106864699A (en) * | 2017-01-20 | 2017-06-20 | 青岛滨海学院 | A kind of maritime search and rescue device and rescue method |
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| C06 | Publication | ||
| PB01 | Publication | ||
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Application publication date: 20160921 |