CN108945465B - Battery throwing and recycling positioning device for electric multi-rotor aircraft - Google Patents
Battery throwing and recycling positioning device for electric multi-rotor aircraft Download PDFInfo
- Publication number
- CN108945465B CN108945465B CN201810958881.6A CN201810958881A CN108945465B CN 108945465 B CN108945465 B CN 108945465B CN 201810958881 A CN201810958881 A CN 201810958881A CN 108945465 B CN108945465 B CN 108945465B
- Authority
- CN
- China
- Prior art keywords
- battery
- battery pack
- positioning device
- opening
- box
- 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.)
- Active
Links
- 238000004064 recycling Methods 0.000 title claims abstract description 15
- 238000001514 detection method Methods 0.000 claims abstract description 12
- 230000001681 protective effect Effects 0.000 claims description 10
- 238000000926 separation method Methods 0.000 claims description 4
- 230000005484 gravity Effects 0.000 claims description 2
- 238000011084 recovery Methods 0.000 claims description 2
- 239000000463 material Substances 0.000 abstract description 7
- 230000002035 prolonged effect Effects 0.000 abstract description 5
- 238000000034 method Methods 0.000 description 9
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
The invention discloses a battery throwing, feeding, recycling and positioning device for an electric multi-rotor aircraft, which comprises the following components: the battery box is of a hollow structure and is made of light materials; the battery packs are arranged in the battery box at intervals along the length direction of the battery box, and the size of each battery pack is smaller than that of the battery box; the fixing pieces are in one-to-one correspondence with the battery packs, each fixing piece comprises an even number of brackets, the even number of brackets are symmetrically arranged on the inner wall of the battery box, and the brackets are arranged at two ends of the bottom of the battery pack; the positioning device can be used for positioning the battery pack to the position of the battery pack for recycling after the battery pack is thrown; the battery box is internally provided with a detection unit, when the capacity of the battery pack at the bottom is insufficient, the battery is thrown, so that the load of the aircraft is lightened, the endurance time of the aircraft is prolonged, and the flexibility is higher.
Description
Technical Field
The invention relates to a battery throwing, feeding and recycling positioning device, in particular to a battery throwing, feeding and recycling positioning device for an electric multi-rotor aircraft.
Background
The multi-rotor aircraft selects the batteries as energy sources, the battery loading multiple groups can improve the endurance time of the aircraft, but after the battery electric quantity is exhausted, the battery becomes useless weight, which is equivalent to the condition that the aircraft needs to bear useless weight to continue flying and consume a great amount of electric quantity, if the battery with the exhausted electric quantity is discarded, the useless load of the aircraft can be directly reduced, the endurance time is prolonged, and the battery throwing, recovering and positioning device disclosed by the invention can realize the automatic discarding function of the battery, integrates the anti-falling and position returning functions on the battery, and provides a reference idea for prolonging the endurance time of the aircraft.
The traditional battery is thrown and is retrieved positioner and do not have parachute and protective sheath, causes the battery to break easily in the battery throwing in-process, and some do not set up the emitter that can launch 3G or 4G signal, can not accurate location to retrieve after the battery is thrown, causes the group battery after throwing easily to lose, waste resource, and some do not have the spring between door and the battery box that opens and shuts, can not reset the door that opens and shuts after will opening through the tension of spring and close, and the practicality is not strong.
Disclosure of Invention
The invention overcomes the defects of the prior art and provides a battery throwing, feeding, recovering and positioning device for an electric multi-rotor aircraft.
In order to achieve the above purpose, the invention adopts the following technical scheme: a battery cast-in-place recovery positioning device for an electric multi-rotor aircraft, comprising: the battery box is of a hollow structure and is made of light materials; the battery packs are arranged in the battery box at intervals along the length direction of the battery box, and the size of each battery pack is smaller than that of the battery box; the fixing pieces are in one-to-one correspondence with the battery packs, each fixing piece comprises an even number of brackets, the even number of brackets are symmetrically arranged on the inner wall of the battery box, and the brackets are arranged at two ends of the bottom of the battery pack; and the battery pack can be positioned to the battery pack position for recycling through the positioning device after being thrown.
In a preferred embodiment of the present invention, the battery box further includes a plurality of power connectors and at least one detection unit, where the power connectors are in a one-to-one correspondence with the positions of the battery pack, and the detection unit is capable of detecting the electric quantity of the battery pack.
In a preferred embodiment of the invention, when the detection unit detects that the capacity of the battery pack at the bottom is less than 5% -10% of the total amount of the batteries, the battery is thrown by retracting the support after the power connector is connected with the battery pack at the upper layer.
In a preferred embodiment of the invention, the battery box further comprises an opening and closing door, wherein the opening and closing door is arranged at the bottom of the battery box, and the opening and closing door is connected with the battery box through a hinge.
In a preferred embodiment of the present invention, the opening and closing door is provided with a switch, and the opening and closing door is controlled to rotate and unlock through the switch.
In a preferred embodiment of the invention, the opening and closing door is connected with the battery box through a spring, and the opened opening and closing door can be reset through the tension of the spring.
In a preferred embodiment of the invention, a plurality of grooves are formed in the inner wall of the battery box, the grooves correspond to the supports, and when the supports are retracted, the supports enter the grooves to prevent the supports from protruding to influence the detachment of the battery.
In a preferred embodiment of the invention, the battery pack positioning device further comprises a transmitting device, wherein the transmitting device can transmit 3G or/and 4G signals, and the battery pack positioning device is matched with the positioning device to accurately position the battery pack.
In a preferred embodiment of the invention, the battery pack is provided with the parachute and the protective sleeve, the parachute is arranged at the top of the battery pack, the protective sleeve is arranged at the outer side of the battery pack, and the thrown battery pack can be prevented from being broken through the parachute and the protective sleeve.
In a preferred embodiment of the present invention, 5% -10% of the remaining electric quantity in the battery pack after casting can charge the transmitting device and the positioning device.
In a preferred embodiment of the present invention, the power connector is rotatable about its axis to complete the disconnection of the battery electrodes.
In a preferred embodiment of the present invention, the bracket and the door opening and closing switch can rotate around the shaft to realize the functions.
In a preferred embodiment of the present invention, the battery pack is thrown from bottom to top in sequence along the length direction of the battery box.
In a preferred embodiment of the invention, the battery box further comprises a side door, and the side door is opened to facilitate the layering of the battery components inside the battery box.
The invention solves the defects existing in the background technology, and has the following beneficial effects:
(1) The battery throwing and recycling positioning device can realize the automatic discarding function of the battery, integrates the anti-falling and position returning functions on the battery, does not have a parachute and a protective sleeve for prolonging the endurance time of the aircraft, does not cause the battery to break in the battery throwing process, and prolongs the service life of the battery pack.
(2) The 3G or/and 4G signals can be transmitted through the transmitting device and then matched with the positioning device, the battery can be accurately positioned and recycled after being thrown, the battery pack after being thrown cannot be lost, the safety is high, and the positioning information is very accurate.
(3) A spring is arranged between the opening and closing door and the battery box, and the opening and closing door after being opened is reset and closed through the tension of the spring, so that the battery pack is prevented from being thrown by mistake.
(4) The battery box inner wall is equipped with the recess, and the recess corresponds with the support position, and the size is the same, and the support has the self-locking function, prevents support maloperation, causes the group battery to throw by mistake, and after the support was packed up, the support got into in the recess, prevents that the support from protruding, influences the battery and breaks away from.
(5) When the detection unit detects that the battery capacity of the battery pack at the bottom is less than 5% -10% of the total amount of the batteries, the power connector is connected with the battery pack at the upper layer, then the control unit controls the support to retract to throw the batteries, so that the sudden power failure of the aircraft can be avoided, and the safety is high.
(6) The positioning device and the transmitting device of the 3G or/and 4G signals are arranged under the parachute and are powered by the residual electric quantity of the thrown battery, so that ground personnel can retrieve and recover the battery pack after the throwing of the exhausted battery is completed, the situation that the positioning device and the transmitting device are not powered by a power supply does not occur, the battery pack is lost, and the safety is high.
(7) When the battery pack is thrown, in order to ensure that the parachute can be opened, a tension rope is hung at the bottom of the battery pack on the upper layer, a hanging ring is connected with the tension rope and hung on the parachute at the top of the battery pack on the lower layer, the hanging ring is of a snap-on structure, and the parachute is pulled out by an elastic rope on the hanging ring in the separation process of the battery pack, so that the parachute in the descent process can be completely opened, and the throwing safety is improved.
(8) The switch can lock the opening and closing door, prevent misoperation of the opening and closing door, prevent the battery box from throwing the battery pack at improper time or place, and improve safety.
Drawings
FIG. 1 is a schematic partial construction of a preferred embodiment of the present invention;
FIG. 2 is a schematic side door construction view of a preferred embodiment of the present invention;
FIG. 3 is a schematic view of the power connector structure of the preferred embodiment of the present invention;
FIG. 4 is a schematic view of the stent structure of the preferred embodiment of the present invention;
FIG. 5 is a schematic view of the hinge connection location of the preferred embodiment of the present invention;
FIG. 6 is a schematic diagram of the switch position of a preferred embodiment of the present invention;
reference numerals:
1. parachute 2, group battery, 3, switch, 4, open and shut the door, 5, power connection, 6, support, 7, power cord, 8, hinge, 9, spring, 10, link, 11, side door.
Detailed Description
The invention will now be described in further detail with reference to the drawings and examples, which are simplified schematic illustrations of the basic structure of the invention, which are presented only by way of illustration, and thus show only the structures that are relevant to the invention.
As shown in fig. 1, 2, 3, 4, 5 and 6, a battery throwing, recycling and positioning device for an electric multi-rotor aircraft comprises a battery box, a plurality of battery packs 2, a plurality of fixing pieces, a control unit and at least one positioning device.
Specifically, the battery box is hollow structure, the battery box adopts light material to make, light material includes but is not limited to than iron, aluminum alloy or combined material that copper material is lighter, in order to lighten battery box self weight, group battery 2 sets up in the battery box inside along battery box length direction interval, group battery 2 size is less than the battery box size, the mounting is in one-to-one correspondence with group battery 2, the mounting includes even a plurality of support 6, even a plurality of support 6 symmetry are installed at the battery box inner wall, support 6 sets up in group battery 2 bottom both ends, control unit can control support 6 to pack up, group battery 2 on the support 6 drops this moment, group battery 2 throws the back and can fix a position group battery 2 position through positioner and retrieve.
In other words, the battery throwing and recycling positioning device for the electric multi-rotor aircraft comprises, but is not limited to, a battery box, a battery pack 2, a fixing piece, a control unit and a positioning device, wherein the battery box is made of a light material, so that the whole mass of the battery box is smaller, the flying efficiency of the aircraft is avoided, the device can be arranged at the bottom of the electric multi-rotor aircraft and is mainly used for discarding batteries with depleted electric quantity, so that the air time of the aircraft is prolonged, the battery pack 2 is sequentially arranged and arranged in the battery box from top to bottom, the number of the battery packs 2 can be freely increased and decreased according to test requirements, the electric multi-rotor aircraft uses the batteries in the battery box from bottom to top, the battery throwing and recycling positioning device can realize the automatic discarding function of the batteries, the anti-falling and position returning functions are integrated on the batteries, the battery throwing and recycling positioning device does not have parachute 1 and protective sleeves, the battery is not damaged in the battery throwing process, and the service life of the battery pack 2 is prolonged.
According to a preferred embodiment of the present invention, a battery throwing, recovering and positioning device for an electric multi-rotor aircraft further comprises an opening and closing door 4, a hanging ring 10, a positioning device and a launching device.
Specifically, when the battery pack 2 is thrown, in order to ensure that the parachute 1 can be opened, a tension rope is hung at the bottom of the upper layer of battery pack 2, the tension rope is connected with a hanging ring 10, the hanging ring 10 is hung on the parachute 1 at the top of the lower layer of battery pack 2, the hanging ring 10 is divided into two parts, one end of the hanging ring is connected with the bottom of the upper layer of battery pack 2, the other end of the hanging ring is connected with the top of the parachute 1, the hanging ring 10 is of a snap button structure, when the lower layer of battery pack 2 is thrown, the hanging ring 10 is opened through the gravity of the battery pack 2, and meanwhile, the parachute 1 is pulled by an elastic rope on the hanging ring 10 in the separation process of the battery pack 2, so that the parachute 1 in the falling process can be completely opened, and the throwing safety is improved.
The positioning device is a GPS positioning device, the opening and closing door 4 is arranged at the bottom of the battery box, the opening and closing door 4 is connected with the battery box through a hinge 8, the hinge 8 has the function of enabling the opening and closing door 4 to smoothly rotate, the hinge 8 is connected in a mode that two parts of the hinge 8 are respectively close to the outer wall of the battery box and the side face of the opening and closing door 4 when the opening and closing door 4 is closed, a switch 3 is arranged on the opening and closing door 4, the switch 3 is controlled by a control unit to further control the opening and closing door 4 to rotate and unlock, the opening and closing door 4 is connected with the battery box through a spring 9, the opened opening and closing door 4 can be reset through tension or/and tension of the spring 9, and the spring 9 needs to ensure that the opening and closing door returns to a tightly closed state after the opening and closing door is controlled by the control unit to rotate to an upper locking state after 30s of throwing.
The switch 3 can be controlled to be turned on or off by the control unit, the opening and closing door 4 is closed by the spring force of the spring 9, the action of the switch 3 can be a safety function, the control unit is prevented from accidentally falling off the battery pack 2 at an improper place when the control unit fails, the retraction of the switch is completed before 3s of the battery pack 2 is about to be thrown, and a specific working mode can be small motor control.
A spring 9 is connected between the opening and closing door 4 and the wall of the battery box, so that the opening and closing door 4 can be restored to the closed state from the opened state, the tension between the spring 9 and the opening and closing door 4 cannot be too large, the opening and closing door 4 can be opened and thrown smoothly in the battery descending process, meanwhile, the tension cannot be too small, the opening and closing door 4 can be restored to the closed state after being opened, the opening and closing door 4 can be closed by being embedded into the door by the switch 3, and the opening and closing door 4 is locked, so that accidents are prevented.
The hinge 8 is arranged between the opening and closing door 4 and the battery box, the opening and closing door 4 is divided into a left part and a right part, the opening and closing of the opening and closing door 4 is controlled by the switch 3, the transmitting device can transmit 3G or/and 4G signals, and the transmitting device is matched with the positioning device to accurately position the battery pack 2.
According to a preferred embodiment of the present invention, the battery box further includes a plurality of power connectors 5 and at least one detection unit, the positions of the power connectors 5 and the battery pack 2 are in one-to-one correspondence, the plurality of power connectors 5 are connected to a power line 7, the detection unit can detect the electric quantity of the battery pack 2, when the detection unit detects that the battery capacity of the bottom battery pack 2 is less than 5% -10% of the total amount of batteries, the power connectors 5 are connected to the upper layer of battery pack 2, and then the control unit controls the support 6 to retract for battery throwing.
Specifically, when the detection unit detects that the battery capacity of the bottom battery pack 2 is less than 5% -10% of the total amount of batteries, after the power connector 5 is connected with the upper layer of battery pack 2, the control unit controls the support 6 to retract and throw the batteries, so that sudden power failure of an aircraft can not be caused, safety is high, then the opening and closing rotation of the opening and closing door 4 is controlled to unlock the door, further the power connector 5 and the support 6 of the batteries needing to be thrown are controlled to retract, the batteries which consume electric quantity descend by self weight to open the opening and closing door 4, then the opening and closing door 4 is locked, the throwing of the batteries is completed, the support 6 uses a small amount of electric energy corresponding to the battery pack 2 to complete a self-locking function, after the control unit sends a throwing signal, the power connector 5 of the corresponding battery pack 2 is disconnected, and the support 6 drops due to the fact that no electric energy supports falling due to self weight.
The parachute 1 can be opened in the descending process of the battery pack, the residual electric quantity is used for supplying power for the GPS positioning device and the 3G or/and 4G device so that ground personnel can recover batteries, the other batteries are thrown and recovered, the process is similar to the steps, the uppermost battery does not need to be thrown, a 3G or/and 4G signal can be transmitted through the transmitting device and then matched with the positioning device, the battery can be accurately positioned and recovered after being thrown, the battery pack 2 after being thrown cannot be lost, the safety is higher, the positioning information is very accurate, the size of the battery pack 2 is slightly smaller than the internal size of the storage box of the battery pack 2, and the battery pack 2 can be smoothly separated from the storage box.
According to a preferred embodiment of the invention, the inner wall of the battery box is provided with grooves and side doors 11.
Specifically, the recess corresponds with support 6 position, and the size is the same, and after support 6 was packed up, support 6 got into in the recess, prevents that support 6 is protruding, when group battery 2 is thrown down in proper order along battery box length direction, can not cause support 6 to block group battery 2, influences the battery and breaks away from, throws the effect better, and side door 11 is opened and can be conveniently put into the battery box inside with group battery 2 layering.
In sum, the battery throwing and recycling positioning device can realize the automatic discarding function of the battery, the anti-falling and position feedback functions are integrated on the battery, the device for prolonging the endurance time of the aircraft to lighten the load of the aircraft and prolong the endurance time of the aircraft can realize the automatic discarding function of the battery, the anti-falling and position feedback functions are integrated on the battery, the battery throwing and recycling positioning device does not have a parachute 1 and a protective sleeve for prolonging the endurance time of the aircraft, the battery is not broken in the battery throwing process, the service life of the battery pack 2 is prolonged, the 3G or/and 4G signals can be transmitted through the transmitting device, then the battery throwing device is matched with the positioning device, the battery can be accurately positioned and recycled after being thrown, the thrown battery pack 2 is not lost, the safety is high, and the positioning information is very accurate.
The above-described preferred embodiments according to the present invention are intended to suggest that, from the above description, various changes and modifications can be made by the person skilled in the art without departing from the scope of the technical idea of the present invention. The technical scope of the present invention is not limited to the description, but must be determined according to the scope of claims.
Claims (4)
1. A battery cast-in-place recovery positioning device for an electric multi-rotor aircraft, comprising:
the battery box is of a hollow structure;
the battery packs are arranged in the battery box at intervals along the length direction of the battery box, and the size of each battery pack is smaller than that of the battery box;
the fixing pieces are in one-to-one correspondence with the battery packs, each fixing piece comprises an even number of brackets, the even number of brackets are symmetrically arranged on the inner wall of the battery box, and the brackets are arranged at two ends of the bottom of the battery pack;
the battery pack can be positioned to the position of the battery pack for recycling through the positioning device after being thrown;
the battery box is internally provided with a plurality of power connectors and at least one detection unit, the power connectors are in one-to-one correspondence with the positions of the battery pack, and the detection units can detect the electric quantity of the battery pack;
when the detection unit detects that the capacity of the battery pack at the bottom is less than 5% -10% of the total amount of the batteries, the battery is thrown by retracting the bracket after the power connector is connected with the battery pack at the upper layer;
the opening and closing door is also connected with the battery box through a spring, and the opened opening and closing door can be reset through the tension of the spring;
the battery pack positioning device comprises a positioning device, a transmitting device and a battery pack positioning device, wherein the battery pack positioning device is used for positioning a battery pack, and the transmitting device can transmit 3G or/and 4G signals;
the battery pack is provided with a parachute and a protective sleeve, the parachute is arranged at the top of the battery pack, the protective sleeve is arranged at the outer side of the battery pack, and the thrown battery pack can be prevented from being broken through the parachute and the protective sleeve;
the rest 5% -10% of electric quantity in the battery pack after throwing can charge the transmitting device and the positioning device;
the battery pack is sequentially arranged and installed in the battery box body from top to bottom, in order to ensure that the parachute can be opened, a tension rope is hung at the bottom of the upper layer of battery pack, a hanging ring is connected to the tension rope and hung on the parachute at the top of the lower layer of battery pack, the hanging ring is divided into two parts, one end of the hanging ring is connected to the bottom of the upper layer of battery pack, the other end of the hanging ring is connected to the top of the parachute, the hanging ring is of a snap structure, and when the lower layer of battery pack is thrown, the hanging ring is opened by the gravity of the battery pack, and meanwhile, the parachute is pulled by an elastic rope on the hanging ring in the separation process of the battery pack.
2. A battery cast and retrieve positioning device for an electric multi-rotor aircraft according to claim 1, wherein:
the battery box is characterized by further comprising an opening and closing door, wherein the opening and closing door is arranged at the bottom of the battery box, and the opening and closing door is connected with the battery box through a hinge.
3. A battery cast and retrieve positioning device for an electric multi-rotor aircraft according to claim 2, wherein:
the opening and closing door is provided with a switch, and the opening and closing door is controlled to rotate and unlock through the switch.
4. A battery cast and retrieve positioning device for an electric multi-rotor aircraft according to claim 1, wherein:
the inner wall of the battery box is provided with a plurality of grooves, the grooves correspond to the supports, and when the supports are retracted, the supports enter the grooves to prevent the supports from protruding to influence the separation of the battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810958881.6A CN108945465B (en) | 2018-08-22 | 2018-08-22 | Battery throwing and recycling positioning device for electric multi-rotor aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810958881.6A CN108945465B (en) | 2018-08-22 | 2018-08-22 | Battery throwing and recycling positioning device for electric multi-rotor aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108945465A CN108945465A (en) | 2018-12-07 |
| CN108945465B true CN108945465B (en) | 2024-02-23 |
Family
ID=64473524
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810958881.6A Active CN108945465B (en) | 2018-08-22 | 2018-08-22 | Battery throwing and recycling positioning device for electric multi-rotor aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108945465B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110667863A (en) * | 2019-11-11 | 2020-01-10 | 北京中科利丰科技有限公司 | Unmanned aerial vehicle driving system capable of being separated step by step |
| CN113911371A (en) * | 2021-10-14 | 2022-01-11 | 贵州电网有限责任公司 | Unmanned aerial vehicle battery increase-volume anti-falling system |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1137503A (en) * | 1965-01-29 | 1968-12-27 | Gq Parachute Comp Ltd | Improvements in or relating to containers |
| CN106143918A (en) * | 2016-08-21 | 2016-11-23 | 张玉华 | Unmanned plane delivered by a kind of lifebuoy |
| CN106660619A (en) * | 2015-04-01 | 2017-05-10 | 嵩比有限公司 | Drone-type lifesaving equipment dropping device |
| KR101812487B1 (en) * | 2016-07-20 | 2017-12-27 | 주식회사 숨비 | Offshore lifesaving system using drone |
| CN206841719U (en) * | 2017-05-11 | 2018-01-05 | 防灾科技学院 | A kind of more rotor Intelligent flight devices with function of taking photo by plane and jettisoning |
| CN107600439A (en) * | 2017-09-26 | 2018-01-19 | 上海重塑能源科技有限公司 | A kind of long endurance unmanned aircraft electrical source of power device and unmanned plane |
| CN208882115U (en) * | 2018-08-22 | 2019-05-21 | 江苏心源航空科技有限公司 | A kind of battery for electronic multi-rotor aerocraft is jettisoninged and recycling positioning device |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8480034B2 (en) * | 2009-05-29 | 2013-07-09 | Caylym Technologies International, Llc | Aerial delivery devices, systems and methods |
| WO2014011255A2 (en) * | 2012-03-30 | 2014-01-16 | W. Morrison Consulting Group, Inc. | Long range electric aircraft and method of operating same |
-
2018
- 2018-08-22 CN CN201810958881.6A patent/CN108945465B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1137503A (en) * | 1965-01-29 | 1968-12-27 | Gq Parachute Comp Ltd | Improvements in or relating to containers |
| CN106660619A (en) * | 2015-04-01 | 2017-05-10 | 嵩比有限公司 | Drone-type lifesaving equipment dropping device |
| KR101812487B1 (en) * | 2016-07-20 | 2017-12-27 | 주식회사 숨비 | Offshore lifesaving system using drone |
| CN106143918A (en) * | 2016-08-21 | 2016-11-23 | 张玉华 | Unmanned plane delivered by a kind of lifebuoy |
| CN206841719U (en) * | 2017-05-11 | 2018-01-05 | 防灾科技学院 | A kind of more rotor Intelligent flight devices with function of taking photo by plane and jettisoning |
| CN107600439A (en) * | 2017-09-26 | 2018-01-19 | 上海重塑能源科技有限公司 | A kind of long endurance unmanned aircraft electrical source of power device and unmanned plane |
| CN208882115U (en) * | 2018-08-22 | 2019-05-21 | 江苏心源航空科技有限公司 | A kind of battery for electronic multi-rotor aerocraft is jettisoninged and recycling positioning device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108945465A (en) | 2018-12-07 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108891601B (en) | Material pod release control system and release control method | |
| CN108945465B (en) | Battery throwing and recycling positioning device for electric multi-rotor aircraft | |
| CN109120055B (en) | Emergency traction and auxiliary storage battery system for rail transit | |
| CN210041109U (en) | Transmission line inspection device | |
| CN108438226A (en) | Goods and materials with parachute launch gondola | |
| AU2006222162A1 (en) | Accumulator and method for the operation thereof | |
| JP7178743B2 (en) | unmanned aerial vehicle | |
| CN107069538A (en) | Wire walking type line data-logging device based on multi-rotor unmanned aerial vehicle technology | |
| CN206511133U (en) | A kind of parachute of unmanned plane | |
| CN107612115A (en) | Airborne lithium battery group is thrown and moves back power grid control method and control device | |
| KR102163447B1 (en) | Unmanned aerial vehicle with improved battery efficiency | |
| CN105947191B (en) | A kind of novel multi-rotor unmanned aerial vehicle | |
| CN209795841U (en) | unmanned aerial vehicle parachute control system | |
| CN208882115U (en) | A kind of battery for electronic multi-rotor aerocraft is jettisoninged and recycling positioning device | |
| CN109131848B (en) | Safe forced landing system for unmanned aerial vehicle and auxiliary device thereof | |
| CN111470049A (en) | Multi-rotor unmanned aerial vehicle inspection safety protection device and protection method | |
| WO2019172061A1 (en) | Unmanned aerial vehicle and moving body | |
| WO2022157245A1 (en) | Aircraft propulsion module and aircraft | |
| CN209795831U (en) | Carrying aircraft | |
| CN213205020U (en) | Building engineering construction special type operation auxiliary device | |
| CN211293267U (en) | Unmanned aerial vehicle positioner based on solar energy | |
| CN210468843U (en) | Mobile power supply with standby lithium battery | |
| CN208506597U (en) | A kind of cover control device in UAV Formation Flight | |
| CN109956046B (en) | Unmanned aerial vehicle protection device | |
| CN109502031B (en) | Electronic emergency separating device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |