CN213413559U - Electric power inspection unmanned aerial vehicle with electric quantity monitoring function - Google Patents
Electric power inspection unmanned aerial vehicle with electric quantity monitoring function Download PDFInfo
- Publication number
- CN213413559U CN213413559U CN202021901052.3U CN202021901052U CN213413559U CN 213413559 U CN213413559 U CN 213413559U CN 202021901052 U CN202021901052 U CN 202021901052U CN 213413559 U CN213413559 U CN 213413559U
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- Prior art keywords
- aerial vehicle
- unmanned aerial
- inner chamber
- battery
- electric power
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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
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
The utility model discloses an unmanned aerial vehicle is patrolled and examined to electric power that possesses electric quantity monitoring function, including the unmanned aerial vehicle body, the inner chamber swing joint of unmanned aerial vehicle body bottom has battery body, battery body's bottom fixedly connected with bottom plate, the fixed slot has all been seted up to the both sides of bottom plate. The utility model discloses a pulling fixing clip pole, the fixing clip pole drives the sliding sleeve motion, the sliding sleeve extrudees reset spring, fixing clip pole breaks away from the inner chamber of fixed slot when the motion, thereby remove the fixed to battery body and bottom plate, accomplish the dismantlement of battery body, thereby reset spring's the elasticity that resets can drive fixing clip pole and extend to the inner chamber of fixed slot and fix battery body and bottom plate, it is also comparatively common in being used for electric power to patrol and examine to have solved unmanned aerial vehicle, unmanned aerial vehicle's power supply comes from the battery, if the change of battery is convenient can direct influence unmanned aerial vehicle's use inadequately, thereby change for the battery and cause inconvenient problem.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle is patrolled and examined to electric power that possesses electric quantity monitoring function.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, compared with a piloted aircraft, the unmanned aerial vehicle is often more suitable for tasks too foolproof, dirty or dangerous, the unmanned aerial vehicle can be divided into military and civil, and the unmanned aerial vehicle can be widely applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news report, power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like according to the application field, the purposes of the unmanned aerial vehicle are greatly expanded, the unmanned aerial vehicle is common in the power inspection, the power supply of the unmanned aerial vehicle comes from a battery, and the use of the unmanned aerial vehicle can be directly influenced if the battery is not convenient enough, thereby causing inconvenience in battery replacement.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle is patrolled and examined to electric power that possesses electric quantity monitoring function possesses the advantage of being convenient for change the battery, has solved unmanned aerial vehicle and has also comparatively common in being used for electric power to patrol and examine, and unmanned aerial vehicle's power supply comes from the battery, if the change of battery is convenient can direct influence unmanned aerial vehicle's use inadequately to change for the battery and cause inconvenient problem.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle is patrolled and examined to electric power that possesses electric quantity monitoring function, includes the unmanned aerial vehicle body, the inner chamber swing joint of unmanned aerial vehicle body bottom has the battery body, the bottom fixedly connected with bottom plate of battery body, the fixed slot has all been seted up to the both sides of bottom plate, the activity chamber has all been seted up to the both sides of unmanned aerial vehicle body bottom, the inner chamber fixedly connected with slide bar in activity chamber, the sliding surface of slide bar is connected with the sliding sleeve, the bottom fixedly connected with fixing clip pole of sliding sleeve, the one end of fixing clip pole extends to the inner chamber of fixed.
Preferably, the surface of the sliding rod is connected with a return spring in a sliding mode, and two ends of the return spring are fixedly connected with the sliding sleeve and the inner wall of the movable cavity respectively.
Preferably, the both sides of unmanned aerial vehicle body bottom, and the bottom that is located the activity chamber has all seted up spacing slide opening, the fixing clip pole extends to the outside of spacing slide opening, and with the inner chamber sliding connection of spacing slide opening.
Preferably, the top of the inner cavity of the movable cavity is provided with a limiting groove, the inner cavity of the limiting groove is connected with a limiting block in a sliding manner, and one side of the limiting block, which is far away from the inner cavity of the limiting groove, is fixedly connected with the sliding sleeve.
Preferably, equal fixedly connected with undercarriage all around of unmanned aerial vehicle body bottom, the bottom fixedly connected with blotter of undercarriage.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a pulling fixing clip pole, the fixing clip pole drives the sliding sleeve motion, the sliding sleeve extrudees reset spring, fixing clip pole breaks away from the inner chamber of fixed slot when the motion, thereby remove the fixed to battery body and bottom plate, accomplish the dismantlement of battery body, thereby reset spring's the elasticity that resets can drive fixing clip pole and extend to the inner chamber of fixed slot and fix battery body and bottom plate, it is also comparatively common in being used for electric power to patrol and examine to have solved unmanned aerial vehicle, unmanned aerial vehicle's power supply comes from the battery, if the change of battery is convenient can direct influence unmanned aerial vehicle's use inadequately, thereby change for the battery and cause inconvenient problem.
2. The utility model discloses a set up spacing groove and stopper, played the spacing effect of sliding sleeve, through setting up spacing slide opening, played the spacing effect to the fixing clip pole.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic view of the main body of the unmanned aerial vehicle according to the present invention;
fig. 3 is a schematic diagram of a partial enlarged structure shown in fig. 2 according to the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. a battery body; 3. a base plate; 4. fixing grooves; 5. a movable cavity; 6. a slide bar; 7. a sliding sleeve; 8. fixing the clamping rod; 9. a return spring; 10. a limiting slide hole; 11. a limiting groove; 12. a limiting block; 13. a landing gear.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
The utility model discloses an unmanned aerial vehicle body 1, battery body 2, bottom plate 3, fixed slot 4, activity chamber 5, slide bar 6, sliding sleeve 7, fixed kelly 8, reset spring 9, spacing slide opening 10, spacing groove 11, stopper 12 and undercarriage 13 part are the parts that universal standard spare or field technician know, and its structure and principle all are that this technical staff all can learn through the technical manual or learn through conventional experimental method.
Referring to fig. 1-3, an electric power inspection unmanned aerial vehicle with electric quantity monitoring function comprises an unmanned aerial vehicle body 1, landing gears 13 are fixedly connected to the periphery of the bottom of the unmanned aerial vehicle body 1, cushion pads are fixedly connected to the bottoms of the landing gears 13, a battery body 2 is movably connected to the inner cavity of the bottom of the unmanned aerial vehicle body 1, a bottom plate 3 is fixedly connected to the bottom of the battery body 2, fixing grooves 4 are formed in two sides of the bottom plate 3, movable cavities 5 are formed in two sides of the bottom of the unmanned aerial vehicle body 1, slide rods 6 are fixedly connected to the inner cavities of the movable cavities 5, sliding sleeves 7 are slidably connected to the surfaces of the slide rods 6, limiting grooves 11 are formed in the tops of the inner cavities of the movable cavities 5, limiting blocks 12 are slidably connected to the inner cavities of the limiting grooves 11, one sides of the limiting blocks 12, which are far away from the inner cavities of the, the surface of the sliding rod 6 is connected with a reset spring 9 in a sliding way, two ends of the reset spring 9 are respectively fixedly connected with the inner walls of the sliding sleeve 7 and the movable cavity 5, two sides of the bottom of the unmanned aerial vehicle body 1 are respectively provided with a limiting sliding hole 10 at the bottom of the movable cavity 5, the fixed clamping rod 8 extends to the outside of the limiting sliding hole 10 and is connected with the inner cavity of the limiting sliding hole 10 in a sliding way, the fixed clamping rod 8 drives the sliding sleeve 7 to move by pulling the fixed clamping rod 8, the sliding sleeve 7 extrudes the reset spring 9, the fixed clamping rod 8 is separated from the inner cavity of the fixed groove 4 during movement, so that the fixation of the battery body 2 and the bottom plate 3 is released, the disassembly of the battery body 2 is completed, otherwise, the reset elasticity of the reset spring 9 can drive the fixed clamping rod 8 to extend to the inner cavity of the fixed groove 4 to fix the battery body 2 and the bottom plate 3, unmanned aerial vehicle's power supply comes from the battery, if the change of battery is convenient can direct influence unmanned aerial vehicle's use inadequately to change for the battery and cause inconvenient problem.
During the use, through pulling fixing clip pole 8, fixing clip pole 8 drives sliding sleeve 7 motion, sliding sleeve 7 extrudees reset spring 9, fixing clip pole 8 breaks away from the inner chamber of fixed slot 4 when the motion, thereby relieve the fixed to battery body 2 and bottom plate 3, accomplish the dismantlement of battery body 2, thereby reset spring 9's elasticity that resets can drive fixing clip pole 8 and extend to the inner chamber of fixed slot 4 and fix battery body 2 and bottom plate 3, it is also comparatively common in being used for electric power to patrol and examine to have solved unmanned aerial vehicle, unmanned aerial vehicle's power supply comes from the battery, if the change of battery is convenient can direct influence unmanned aerial vehicle's use inadequately, thereby change for the battery and lead to the fact inconvenient problem.
The standard parts used in the present application document can be purchased from the market, and can be customized according to the description of the specification and the accompanying drawings, the specific connection mode of each part adopts the conventional means of mature bolt, rivet, welding and the like in the prior art, the machines, parts and equipment adopt the conventional models in the prior art, the control mode is automatically controlled by a controller, the control circuit of the controller can be realized by simple programming of technicians in the field, the control circuit belongs to the common knowledge in the field, and the present application document is mainly used for protecting mechanical devices, so the control mode and the circuit connection are not explained in detail in the present application.
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 invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides an unmanned aerial vehicle is patrolled and examined to electric power that possesses electric quantity monitoring function, includes unmanned aerial vehicle body (1), its characterized in that: the utility model discloses an unmanned aerial vehicle, including unmanned aerial vehicle body (1), the inner chamber swing joint of unmanned aerial vehicle body (1) bottom has battery body (2), bottom fixedly connected with bottom plate (3) of battery body (2), fixed slot (4) have all been seted up to the both sides of bottom plate (3), movable chamber (5) have all been seted up to the both sides of unmanned aerial vehicle body (1) bottom, the inner chamber fixedly connected with slide bar (6) in activity chamber (5), the sliding surface of slide bar (6) is connected with sliding sleeve (7), the bottom fixedly connected with fixing clip pole (8) of sliding sleeve (7), the one end of fixing clip pole (8) extends to the inner chamber of fixed slot (4.
2. The electric power inspection unmanned aerial vehicle that possesses electric quantity monitoring function of claim 1, its characterized in that: the surface of the sliding rod (6) is connected with a return spring (9) in a sliding mode, and two ends of the return spring (9) are fixedly connected with the inner walls of the sliding sleeve (7) and the movable cavity (5) respectively.
3. The electric power inspection unmanned aerial vehicle that possesses electric quantity monitoring function of claim 1, its characterized in that: the utility model discloses an unmanned aerial vehicle, including unmanned aerial vehicle body (1), fixed clamping bar (8), spacing slide opening (10) are all seted up to the both sides of unmanned aerial vehicle body (1) bottom, and the bottom that is located activity chamber (5), fixed clamping bar (8) extend to the outside of spacing slide opening (10), and with the inner chamber sliding connection of spacing slide opening (10).
4. The electric power inspection unmanned aerial vehicle that possesses electric quantity monitoring function of claim 1, its characterized in that: spacing groove (11) have been seted up at the top of activity chamber (5) inner chamber, the inner chamber sliding connection of spacing groove (11) has stopper (12), one side and sliding sleeve (7) fixed connection that spacing groove (11) inner chamber was kept away from in stopper (12).
5. The electric power inspection unmanned aerial vehicle that possesses electric quantity monitoring function of claim 1, its characterized in that: equal fixedly connected with undercarriage (13) all around of unmanned aerial vehicle body (1) bottom, the bottom fixedly connected with blotter of undercarriage (13).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202021901052.3U CN213413559U (en) | 2020-09-03 | 2020-09-03 | Electric power inspection unmanned aerial vehicle with electric quantity monitoring function |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202021901052.3U CN213413559U (en) | 2020-09-03 | 2020-09-03 | Electric power inspection unmanned aerial vehicle with electric quantity monitoring function |
Publications (1)
Publication Number | Publication Date |
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CN213413559U true CN213413559U (en) | 2021-06-11 |
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CN202021901052.3U Expired - Fee Related CN213413559U (en) | 2020-09-03 | 2020-09-03 | Electric power inspection unmanned aerial vehicle with electric quantity monitoring function |
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CN (1) | CN213413559U (en) |
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2020
- 2020-09-03 CN CN202021901052.3U patent/CN213413559U/en not_active Expired - Fee Related
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210611 Termination date: 20210903 |