CN216186140U - Conversion interface arranged in ground power supply system for solving power supply problem of fixed-wing unmanned aerial vehicle - Google Patents
Conversion interface arranged in ground power supply system for solving power supply problem of fixed-wing unmanned aerial vehicle Download PDFInfo
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- CN216186140U CN216186140U CN202122745301.5U CN202122745301U CN216186140U CN 216186140 U CN216186140 U CN 216186140U CN 202122745301 U CN202122745301 U CN 202122745301U CN 216186140 U CN216186140 U CN 216186140U
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- power supply
- interface
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- support arm
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/12—Electric charging stations
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
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- Electric Propulsion And Braking For Vehicles (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model discloses a conversion interface which is arranged in a ground power supply system and solves the problem of power supply of a fixed wing unmanned aerial vehicle, and relates to the technical field of power supply of unmanned aerial vehicles. When the charging box needs to be charged for use, the switching interface part can enable the flip plate to be lifted together when the switching interface part extends out of the power supply box, so that the process of manually lifting the flip plate is omitted, and the purposes of saving time and improving efficiency are achieved.
Description
Technical Field
The utility model relates to the technical field of power supply of unmanned aerial vehicles, in particular to a conversion interface which is arranged in a ground power supply system and solves the problem of power supply of a fixed-wing unmanned aerial vehicle.
Background
Fixed wing unmanned aerial vehicle compares in traditional small-size unmanned aerial vehicle, and its size further grow makes its can wide application in trades such as survey and drawing, geology, oil, agriculture and forestry, and its good function, modularization are integrated. At present, in a field specially used for charging a fixed-wing unmanned aerial vehicle, a conversion interface part is mostly directly used indoors for charging, the application range of the conversion interface part is limited, the conversion interface part cannot be carried, and the conversion interface part cannot be used flexibly according to the field layout.
In view of the above, the present invention provides a conversion interface disposed in a ground power supply system to solve the problem of power supply for a fixed wing drone.
Disclosure of Invention
The utility model aims to provide a conversion interface which is arranged in a ground power supply system and solves the problem of the prior art by solving the power supply problem of a fixed wing unmanned aerial vehicle.
In order to achieve the purpose, the utility model provides the following technical scheme:
arrange the conversion interface of solving the power supply of fixed wing unmanned aerial vehicle in ground power supply system, including the conversion interface part, bury underground in the ground power supply bus of subsurface, the last parallel connection of ground power supply bus has a plurality of ground power supply branch lines, and every ground power supply branch line connects electrical end electric connection with the conversion interface part, its characterized in that: the belly battery on the fixed wing unmanned aerial vehicle connects the electricity with the conversion interface part through the plug of charging wire tip, conversion interface part fixed mounting is in the one end of interface mount pad, the other end of interface mount pad rotates through the pivot and connects on the interior upper portion lateral wall of power supply box, be provided with in the power supply box and be used for keeping the horizontal gesture of interface mount pad and be used for promoting the actuating mechanism to vertical gesture with the interface mount pad.
As a further improvement of the utility model, the top of the power supply box is of an open structure, and a flip plate for covering the top of the power supply box is rotatably arranged on one side of the open structure through a hinge;
when the interface mounting seat is changed from a horizontal state to a vertical state, the turnover cover plate can be synchronously changed into a lifting state from a state of covering the top of the power supply box.
As a further improvement of the utility model, a wire clamping ring is fixedly arranged on one side of the inner surface of the flip plate, which is far away from the rotating end, and the wire clamping ring is used for limiting the charging wire.
As a further improvement of the utility model, a cover supporting block is fixedly connected to the upper edge of the inner side wall of the power supply box and is used for supporting the flip plate when the flip plate is covered.
As a further improvement of the utility model, one end of the interface mounting seat close to the conversion interface part is rotatably provided with a guide wheel through a rotating shaft, and the guide wheel is used for being in rolling contact with the corresponding side surface of the flip cover plate.
As a further improvement of the present invention, the driving mechanism includes a power device, the power device is rotatably connected to the inner lower portion of the power box through a rotating shaft, the output end of the power device is rotatably connected to one end of a second support arm through a rotating shaft, the end of the second support arm is rotatably connected to one end of a first support arm through a rotating shaft, the other end of the second support arm is hinged to the power box, the other end of the first support arm is rotatably connected to an interface mounting base through a rotating shaft, the interface mounting base is rotatably connected to one end of a linkage arm through a rotating shaft, and the other end of the linkage arm is rotatably connected to the upper edge of the inner wall of the power box through a rotating shaft.
As a further improvement of the utility model, one end of the second support arm, which is far away from the first support arm, is provided with a circular ring part for sleeving a rotating shaft, and the rotating shaft is fixedly connected to the inner wall of the power supply box.
As a further improvement of the utility model, the circular ring part is fixedly connected with one end of a third support arm, and the other end of the third support arm is fixedly connected with the end part of the second support arm through a fixed arm.
As a further improvement of the utility model, the power device is an electric push rod.
Compared with the prior art, the utility model has the following beneficial effects:
1. according to the utility model, the fixed wing unmanned aerial vehicle is firstly controlled to move to the charger position where the power supply box is located, then the driving mechanism is controlled to push the interface mounting seat out of the top of the power supply box, so that the conversion interface part is vertically upward, and then a tap of a charging wire is inserted into the conversion interface part, so that the purpose of charging a belly storage battery is realized.
2. When the charging box is not charged, the flip plate covers the power supply box, so that the effects of isolating the inside and the outside of the power supply box are achieved, the effects of rain prevention, light prevention, dust prevention and the like are achieved, the effect of protecting the conversion interface part is achieved, when the charging box is required to be charged and used, the flip plate can be lifted together when the conversion interface part extends out of the power supply box, the process of manually lifting the flip plate is omitted, and the purposes of saving time and improving efficiency are achieved.
3. The utility model can ensure that the interface mounting seat has the effect of pushing up the turnover cover plate in the process of extending out of the power supply box, and the rotation of the interface mounting seat can not be hindered in the process of pushing up the turnover cover plate, so that the in-place process of the interface part is flexible and quick.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of the flip plate of the present invention when it is closed;
FIG. 3 is a schematic structural view of the flip cover of the present invention when opened;
FIG. 4 is a layout diagram of the power box according to the present invention.
In the figure: 1. a fixed wing drone; 2. a belly storage battery; 3. a charging wire; 4. a ground power supply bus; 5. a power supply box; 6. a conversion interface part; 7. an interface mounting base; 8. turning over a cover plate; 9. a ground power supply branch line; 10. a wire clamping ring; 11. an electric push rod; 12. a fixed arm; 13. a linkage arm; 14. a cover supporting block; 15. a guide wheel; 16. a first support arm; 17. a second support arm; 18. and a third support arm.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-4, a switching interface disposed in a ground power supply system for solving the problem of power supply of a fixed-wing drone includes a switching interface 6 and a ground power supply bus 4 buried under the ground, the ground power supply bus 4 is connected in parallel with a plurality of ground power supply branches 9, each ground power supply branch 9 is electrically connected with a power connection terminal of the switching interface 6, and the switching interface is characterized in that: the plug that fixed wing unmanned aerial vehicle 1 was last ventral battery 2 passes through the 3 tip of charging wire connects the electricity with conversion interface part 6, conversion interface part 6 fixed mounting is in the one end of interface mount pad 7, the other end of interface mount pad 7 rotates through the pivot to be connected on the interior upper portion lateral wall of power box 5, be provided with in the power box 5 and be used for keeping 7 horizontal gestures of interface mount pad and be used for promoting the actuating mechanism to vertical gesture with interface mount pad 7.
In the utility model, the top of the power supply box 5 is of an open structure, and a flip plate 8 for covering the top of the power supply box 5 is rotatably arranged on one side of the open structure through a hinge;
when the interface mounting base 7 is changed from a horizontal state to a vertical state, the flip plate 8 can be synchronously changed from a state of covering the top of the power supply box 5 to a lifted state.
Specifically, when the fixed-wing unmanned aerial vehicle 1 needs to be charged, the fixed-wing unmanned aerial vehicle 1 is firstly controlled to travel to a charging station where the power supply box 5 is located, then the driving mechanism is controlled to push the interface mounting seat 7 out of the top of the power supply box 5, so that the conversion interface part 6 is vertically upward, and then a tap of the charging wire 3 is inserted into the conversion interface part 6, so that the charging purpose of the belly storage battery 2 is achieved, and the conversion interface part 6 is located at a certain height by means of the interface mounting seat 7, so that the charging action can be completed by the short charging wire 3; when the charging is not performed, the flip plate 8 covers the power supply box 5, so that the effects of isolating the inside and the outside of the power supply box 5 are achieved, and the effects of rain prevention, light prevention, dust prevention and the like are achieved, and therefore the effect of protecting the conversion interface part 6 can be achieved, when the charging and using are needed, the conversion interface part 6 can enable the flip plate 8 to be lifted together when the power supply box 5 is extended out, the process of manually lifting the flip plate 8 is omitted, and the purposes of saving time and improving efficiency are achieved.
Referring to fig. 2 and 3, in the present invention, a wire clamping ring 10 is fixedly installed on one side of the inner surface of the flip plate 8, which is far away from the rotation end, and the wire clamping ring 10 is used for limiting the charging wire 3, so as to achieve the purpose of wire arrangement of the charging wire 3, so that the charging wire 3 can extend along the length direction of the flip plate 8, and the practicability is improved.
Referring to fig. 2 and 3, a cover supporting block 14 is fixedly connected to an upper edge of an inner side wall of the power box 5, and the cover supporting block 14 is used for supporting the flip cover 8 when the flip cover 8 is closed, so that a sealing state of the flip cover 8 can be maintained.
The guide wheel 15 is rotatably mounted at one end, close to the conversion interface part 6, of the interface mounting seat 7 through a rotating shaft, and the guide wheel 15 is used for being in rolling contact with the corresponding side face of the flip cover plate 8, so that the interface mounting seat 7 can achieve the effect of pushing up the flip cover plate 8 in the process of extending out of the power supply box 5, the interface mounting seat 7 cannot be prevented from rotating in the process of pushing up the flip cover plate 8, and the in-place process of the conversion interface part 6 is flexible and rapid.
Actuating mechanism includes power device, power device rotates the interior lower part of connecting power box 5 through the pivot, power device's output rotates the one end of connecting second support arm 17 through the pivot, just second support arm 17 this end rotates the one end of connecting first support arm 16 through the pivot, the other end of second support arm 17 articulates on power box 5, the other end of first support arm 16 rotates through the pivot and connects on interface mount pad 7, rotate the one end of connecting interlock arm 13 through the pivot on interface mount pad 7, the other end of interlock arm 13 rotates through the pivot and connects on the inner wall of power box 5 along.
The end of the second support arm 17, which is far away from the first support arm 16, is provided with a circular ring part for sleeving a rotating shaft, and the rotating shaft is fixedly connected to the inner wall of the power supply box 5.
The circular part is fixedly connected with one end of a third support arm 18, and the other end of the third support arm 18 is fixedly connected with the end part of a second support arm 17 through a fixed arm 12.
In the present invention, by starting the power device, the fixed arm 12, the second arm 17 and the third arm 18 rotate upward around the rotation axis as a pivot, and at the same time, the first arm 16 gradually supports the interface mounting base 7 vertically, so that the conversion interface 6 reaches a position where charging is convenient.
Preferably, the power device is an electric push rod 11.
Referring to fig. 4, in the scheme, the power boxes 5 can be flexibly arranged according to the ground power supply branch line 9, especially, the power boxes 5 can be arranged in the only range as many as possible by adopting a stepped layout, so as to meet the charging requirements of a plurality of fixed-wing unmanned aerial vehicles 1; as long as the ground power supply branch line 9 is provided on the field, the power supply box 5 can be carried and laid out and then used.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (9)
1. Arrange the conversion interface of solving the power supply of fixed wing unmanned aerial vehicle in ground power supply system, including conversion interface part (6), bury underground in subaerial ground power supply bus (4), it has a plurality of ground power supply branch lines (9) to go up the parallel connection on ground power supply bus (4), and every ground power supply branch line (9) connects electrical end electric connection with conversion interface part (6), its characterized in that: belly battery (2) on fixed wing unmanned aerial vehicle (1) connect the electricity through the plug and conversion interface part (6) of charging wire (3) tip, conversion interface part (6) fixed mounting is in the one end of interface mount pad (7), the other end of interface mount pad (7) rotates through the pivot and connects on the interior upper portion lateral wall of power supply box (5), be provided with in power supply box (5) and be used for keeping interface mount pad (7) horizontal gesture and be used for promoting interface mount pad (7) to the actuating mechanism of vertical gesture.
2. The transition interface arranged to address fixed wing drone powering in a ground powered system of claim 1, characterized by: the top of the power supply box (5) is of an open structure, and a flip plate (8) for covering the top of the power supply box (5) is rotatably mounted on one side of the open structure through a hinge;
when the interface mounting seat (7) is changed from a horizontal state to a vertical state, the turnover cover plate (8) can be synchronously changed into a lifted state from a state of covering the top of the power supply box (5).
3. The transition interface arranged to address fixed wing drone powering in a ground powered system of claim 2, characterized by: one side fixed mounting that the internal surface of flip board (8) kept away from the rotation end has card wire loop (10), and card wire loop (10) are used for spacing charging wire (3).
4. The transition interface arranged to address fixed wing drone powering in a ground powered system of claim 2, characterized by: the power supply box (5) inside wall is gone up along fixedly connected with support apron piece (14), support apron piece (14) are used for holding flip board (8) when flip board (8) lid closes.
5. A conversion interface arranged in a ground power supply system to address fixed wing drone powering according to any one of claims 2 to 4, characterized by: one end of the interface mounting seat (7) close to the conversion interface part (6) is rotatably provided with a guide wheel (15) through a rotating shaft, and the guide wheel (15) is used for rolling and contacting with the corresponding side surface of the flip plate (8).
6. The transition interface arranged to address fixed wing drone powering in a ground powered system of claim 5, characterized by: actuating mechanism includes power device, power device rotates the interior lower part of connecting power box (5) through the pivot, power device's output rotates the one end of connecting second support arm (17) through the pivot, just this end of second support arm (17) rotates the one end of connecting first support arm (16) through the pivot, the other end of second support arm (17) articulates on power box (5), the other end of first support arm (16) rotates through the pivot and connects on interface mount pad (7), rotate the one end of connecting interlock arm (13) through the pivot on interface mount pad (7), the other end of interlock arm (13) rotates through the pivot and connects on the inner wall of power box (5) along.
7. The transition interface arranged to address fixed wing drone powering in a ground powered system of claim 6, characterized by: one end, away from first support arm (16), of second support arm (17) is equipped with a ring portion that is used for the cover to establish the rotation axis, rotation axis fixed connection is on the inner wall of power box (5).
8. The transition interface arranged to address fixed wing drone powering in a ground powered system of claim 7, characterized by: the circular part is fixedly connected with one end of a third support arm (18), and the other end of the third support arm (18) is fixedly connected with the end part of a second support arm (17) through a fixed arm (12).
9. The transition interface arranged to address fixed wing drone powering in a ground powered system of claim 6, characterized by: the power device is an electric push rod (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122745301.5U CN216186140U (en) | 2021-11-10 | 2021-11-10 | Conversion interface arranged in ground power supply system for solving power supply problem of fixed-wing unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122745301.5U CN216186140U (en) | 2021-11-10 | 2021-11-10 | Conversion interface arranged in ground power supply system for solving power supply problem of fixed-wing unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216186140U true CN216186140U (en) | 2022-04-05 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122745301.5U Active CN216186140U (en) | 2021-11-10 | 2021-11-10 | Conversion interface arranged in ground power supply system for solving power supply problem of fixed-wing unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216186140U (en) |
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2021
- 2021-11-10 CN CN202122745301.5U patent/CN216186140U/en active Active
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