CN209626991U - For the element of the wireless charging device of Internet of Things cloud platform - Google Patents

For the element of the wireless charging device of Internet of Things cloud platform Download PDF

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Publication number
CN209626991U
CN209626991U CN201822202966.XU CN201822202966U CN209626991U CN 209626991 U CN209626991 U CN 209626991U CN 201822202966 U CN201822202966 U CN 201822202966U CN 209626991 U CN209626991 U CN 209626991U
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China
Prior art keywords
fuselage
pillar
shells
internet
plate
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CN201822202966.XU
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Chinese (zh)
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不公告发明人
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Shaanxi hailsen Electronic Technology Co.,Ltd.
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Xi'an Yu Bin Mdt Infotech Ltd
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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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/50—Photovoltaic [PV] energy

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  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

A kind of element of the wireless charging device for Internet of Things cloud platform, pillar is fixedly connected on the structure of the upside of the fuselage are as follows: the pillar is rectangular-shape and is molded of plastic material, the pillar is connected via the interlocking part with the upside of the fuselage, the interlocking part includes the connected scarfing plate in the bottom of same pillar, and there are also what the upside with fuselage was connected to prop up platform.The scarfing plate is molded of plastic material, and in addition the scarfing plate is connected with pillar integration.The platform that props up includes propping up piece to be also connected in the set of shells for propping up on piece, and cavity is constituted in set of shells, extruding item is arranged in set of shells.It effectively prevents riveting in the prior art, the framework of interlocking is not easy the defect for usually separating the firm stabilization in the bottom of pillar from the top of fuselage in the top of the fuselage, the bottom of pillar.

Description

For the element of the wireless charging device of Internet of Things cloud platform
Technical field
The utility model relates to the technical fields of Internet of Things cloud platform, and in particular to a kind of nothing for Internet of Things cloud platform The element of line charge electric equipment.
Background technique
In Internet of Things cloud platform, original network communication case and external power supply are electrically connected, and during use, are needed A large amount of electric wire is added, not only waste of resource, but also also more troublesome when maintenance circuit, electric wire is longer, needs to be segmented inspection The problem of looking into, wasting plenty of time
It has just obtained being such as " 2018.05.30 " and patent application No. is " 201820825016.X ", the applying date by research and development A kind of electronic communication equipment wireless charging device described in entitled " electronic communication equipment wireless charging device " comprising body Component and charging assembly, the cylinder block set include fuselage, foot prop, chamber door and door lock, and the fuselage and the foot prop, which are fixed, to be connected It connects, the fuselage is in the upside of the foot prop, and chamber door is arranged on the fuselage, and ventilation opening, institute are arranged on the chamber door The outside that door lock is fixedly connected on the chamber door is stated, the door lock is in the inside of the ventilation opening, and the charging assembly includes Battery, solar energy electroplax, pillar, connecting plate, shield, fan, shaft and fixed plate, the battery are detachably connected on institute The inside of fuselage is stated, the solar energy electroplax is spirally connected with the pillar, and the solar energy electroplax is in the upside of the pillar, The solar energy electroplax and the battery are electrically connected, and the pillar is fixedly connected on the upside of the fuselage, the pillar On link block is set, the link block is fixedly connected on the upside of the pillar, the connecting plate be fixedly connected on it is described too The downside of positive energy battery plate, the connecting plate are the outside with the link block, nut and bolt are arranged on the connecting plate, institute Bolt-through to be stated in the connecting plate and the link block, and is spirally connected with the nut, the shield is spirally connected with the fuselage, and The shield is in the outside of the fuselage, and the fan is rotatably connected on the inside of the shield, the fan and the storage Battery is electrically connected, and the shaft is rotatably connected on the inside of the fan, and the fixed plate is fixedly connected with the shield, and The fixed plate is in the outside of the shield, is arranged screw in the fixed plate, the screw through the fixed plate, And it is spirally connected with the fuselage.
The length of the solar energy electroplax is less than the length of the fuselage, and the width of the solar energy electroplax is less than the machine The width of body.
The quantity of the connecting plate and the link block is a pair, and the connecting plate is made of two pieces of iron plates, the company There is link slot, the width of the link slot is identical as the thickness of the link block on fishplate bar.
It is opened up on the connecting plate and the link block and sets connecting hole, the connecting hole is greater than the straight of the bolt Diameter.
The pillar is in cuboid column, and the width of the pillar is of same size with the link block, the pillar Thickness is less than the thickness of the link block.
The quantity of the fixed plate is four, and the quantity of the screw is four.
It is opened up in the fixed plate and sets circular hole, the diameter of the fixed plate is less than the diameter of the circular hole.
The shield is in rectangular box shape, and the width of the shield is less than the width of the fuselage, and the length of the shield is small In the height of the fuselage.
The length of the fan is less than the width of the shield.
Battery has been added on the inside of fuselage, is made it have the use of Power supply belt motivation body, is added on the upside of fuselage Solar energy electroplax, makes solar energy be converted to electric energy, is stored in battery, add link block, connecting plate and bolt, make it too Positive energy battery plate and fuselage have connectivity, are easy for installation and removal, fan, wind power generation, electric power have been added on the outside of fuselage It is stored in internal storage battery, can ensure that body there can be enough electric power, body operation is driven, not only reduces the utilization of resources, It is also convenient for overhauling and use.
The mode for the upside that the current pillar is fixedly connected on the fuselage commonly uses riveting, interlocking comes the bottom pillar Portion stablizes at the top of the fuselage, due to the rectangular-shape structure of the pillar, rivets, the framework of interlocking is not easy pillar The firm stabilization in bottom at the top of the fuselage, in addition the bottom of pillar is usually separated from the top of fuselage.
Summary of the invention
To solve the above problems, the utility model provides a kind of member of wireless charging device for Internet of Things cloud platform Part effectively reduces riveting in the prior art, the framework of interlocking is not easy the firm stabilization in the bottom of pillar in the fuselage Top, pillar bottom usually from the top of fuselage separate defect.
In order to overcome the shortcomings in the prior art, the utility model provides a kind of wireless charging for Internet of Things cloud platform The solution of the element of electric equipment, specific as follows:
A kind of element of the wireless charging device for Internet of Things cloud platform, including electronic communication equipment wireless charging are set It is standby comprising fuselage, pillar are fixedly connected on the upside of the fuselage；
The pillar is fixedly connected on the structure of the upside of the fuselage are as follows: the pillar is for rectangular-shape and by plastics material Material is constituted, and the pillar is connected via the interlocking part with the upside of the fuselage, and the interlocking part includes the bottom of same pillar C2 The connected scarfing plate CA1 in portion, there are also what the upside with fuselage was connected to prop up platform.
The scarfing plate CA1 is molded of plastic material, and in addition the scarfing plate CA1 is connected with pillar C2 integration.
The platform that props up includes propping up piece CC1 to be also connected in the set of shells CC2 propped up on piece CC1, structure in set of shells CC2 At cavity C CB3, it is arranged on set of shells CC2 and squeezes a CCB1.
The scarfing plate CA1 rabbets into set of shells CC2, squeezes a CCB1 and is used to prevent scarfing plate CA1 from isolating cavity, institute Connection CCC1 is respectively set in the both sides for stating set of shells CC2, and a connection CCC1, which is connected in, to be propped up on piece CC1, couples a CCC1 On positioning plate CCC2 is set, positioning plate CCC2 is used to push down set of shells CC2.
The scarfing plate CA1 further includes stretch section CA2, and stretch section CA2 is stretched according to the both sides of pillar C2.
The scarfing plate CA1 includes that the bottom wall CAA1 of scarfing plate and a pair of skew wall CAA3, a pair of of skew wall CAA3 are in pillar The both sides of C2, in addition skew wall CAA3 is to be less than pi/2 greater than zero with the size of the radian constituted between stretch section CA2.
The skew wall CAA3 between the bottom wall CAA1 of scarfing plate include arcuation wall CAA2.
The set of shells CC2 includes combining wall CCB2, is connected in conjunction with wall CCB2 with the bottom wall CAA1 of scarfing plate.
The pair of extruding CCB1 is towards cavity C CB3 extending obliquely.
The number of the set of shells CC2 is a pair, and a pair of of set of shells CC2 rabbets with scarfing plate CA1；
Fuselage positioning port CC4 is arranged in described prop up on piece CC1；The piece CC1 that props up is via the same machine of fuselage positioning port CC4 Body is connected；
The fuselage positioning port CC4 is arranged in the both sides of scarfing plate CA1.
The utility model has the following beneficial effects:
Having introduced positioning plate CCC2 avoids set of shells CC2 from occurring no small strain after compressing, so that scarfing plate CA1 is separated And go out；Positioning plate CCC2 the both sides set of shells CC2 constraint set of shells CC2 dependent variable, in this way via can allow the office of set of shells CC2 There is not small strain in portion, not only ensures that scarfing plate CA1 is put in without hindrance, scarfing plate after also preventing set of shells CC2 to oppress The separation of CA1 and go out.
Detailed description of the invention
Fig. 1 is the edge schematic diagram of the scarfer with pillar of the utility model.
Fig. 2 is the schematic three dimensional views of the scarfer with pillar of the utility model.
Fig. 3 is the Facad structure figure for propping up platform of the utility model.
Fig. 4 is the downward perspective view for propping up platform of the utility model.
Fig. 5 is that the scarfer of the utility model is combined figure with the front for propping up platform.
Fig. 6 is the scarfer of the utility model and the combination figure projected downwards for propping up platform.
Specific embodiment
The utility model is described further below in conjunction with embodiment.
As shown in figs 1 to 6, for the element of the wireless charging device of Internet of Things cloud platform, including such as application No. is " 201820825016.X ", the applying date are " 2018.05.30 " and patent name is that " a kind of electronic communication equipment wireless charging is set It is standby " described in electronic communication equipment wireless charging device comprising cylinder block set and charging assembly, the cylinder block set include machine Body, foot prop, chamber door and door lock, the fuselage are fixedly connected with the foot prop, and the fuselage is in the upside of the foot prop, described Chamber door is set on fuselage, ventilation opening is set on the chamber door, and the door lock is fixedly connected on the outside of the chamber door, described Door lock is in the inside of the ventilation opening, the charging assembly include battery, solar energy electroplax, pillar, connecting plate, shield, Fan, shaft and fixed plate, the battery are detachably connected on the inside of the fuselage, the solar energy electroplax and the branch Column is spirally connected, and the solar energy electroplax is in the upside of the pillar, and the solar energy electroplax and the battery are electrically connected, The pillar is fixedly connected on the upside of the fuselage；Link block is set on the pillar, and the link block is fixedly connected on The upside of the pillar, the connecting plate are fixedly connected on the downside of the solar energy electroplax, and the connecting plate is and the company Connect the outside of block, nut and bolt be set on the connecting plate, the bolt-through in the connecting plate and the link block, And be spirally connected with the nut, the shield is spirally connected with the fuselage, and the shield is in the outside of the fuselage, the fan It is rotatably connected on the inside of the shield, the fan and the battery are electrically connected, and the shaft is rotatably connected on described The inside of fan, the fixed plate are fixedly connected with the shield, and the fixed plate is in the outside of the shield, described solid Screw is set on fixed board, and the screw is spirally connected through the fixed plate, and with the fuselage.
The length of the solar energy electroplax is less than the length of the fuselage, and the width of the solar energy electroplax is less than the machine The width of body.
The quantity of the connecting plate and the link block is a pair, and the connecting plate is made of two pieces of iron plates, the company There is link slot, the width of the link slot is identical as the thickness of the link block on fishplate bar.
It is opened up on the connecting plate and the link block and sets connecting hole, the connecting hole is greater than the straight of the bolt Diameter.
The pillar is in cuboid column, and the width of the pillar is of same size with the link block, the pillar Thickness is less than the thickness of the link block.
The quantity of the fixed plate is four, and the quantity of the screw is four.
It is opened up in the fixed plate and sets circular hole, the diameter of the fixed plate is less than the diameter of the circular hole.
The shield is in rectangular box shape, and the width of the shield is less than the width of the fuselage, and the length of the shield is small In the height of the fuselage.
The length of the fan is less than the width of the shield.
The pillar is fixedly connected on the structure of the upside of the fuselage are as follows: the pillar is for rectangular-shape and by plastics material Material is constituted, and the pillar is connected via the interlocking part with the upside of the fuselage, and the interlocking part includes the bottom of same pillar C2 The connected scarfing plate CA1 in portion, there are also what the upside with fuselage was connected to prop up platform.
Here, the scarfing plate CA1 is molded of plastic material, and in addition the scarfing plate CA1 is connected with pillar C2 integration.
Described to prop up platform also and be plastic material and constitute, the platform that props up includes the length that integration is connected on the upside of fuselage Cube shape is propped up piece CC1 and is also connected in outer arcuation and the open-topped set of shells CC2, set of shells CC2 propped up on piece CC1 The cavity C CB3 communicated with the top opening is constituted, strip is set on set of shells CC2 and squeezes a CCB1.
The scarfing plate CA1 rabbets into set of shells CC2, squeezes a CCB1 and is used to prevent scarfing plate CA1 from isolating cavity, institute Rod-shaped connection CCC1 is respectively set in the both sides for stating set of shells CC2, and a connection CCC1, which is connected in, to be propped up on piece CC1, couples item Plate positioning plate CCC2 is set on CCC1, and positioning plate CCC2 is used to push down set of shells CC2.
Scarfing plate CA1 is molded of plastic material, and can be put in and covered with pillar C2 together punch forming, scarfing plate CA1 with this When in shell CC2, squeezes a CCB1 and no small strain occurs for set of shells CC2, allow scarfing plate CA1 to put in this；It puts in A CCB1 is squeezed because having afterwards, with this prevents scarfing plate CA1 from separating and goes out；In addition, set of shells CC2 to be avoided to occur after compressing No small strain has introduced positioning plate CCC2 so that scarfing plate CA1 is separated and gone out.Positioning plate CCC2 the both sides set of shells CC2 about The beam strain of set of shells CC2, therefore via can allow the local train of set of shells CC2 not only to ensure that scarfing plate CA1 is put in It is without hindrance, also prevent set of shells CC2 oppress after scarfing plate CA1 separation and go out.
The scarfing plate CA1 further includes stretch section CA2, and stretch section CA2 is stretched according to the both sides of pillar C2.Via stretch section The introducing of CA2 increases connected regions range of the connection-peg with pillar C2, increases the connected stability of pillar C2.
The scarfing plate CA1 includes that the bottom wall CAA1 of scarfing plate and a pair of skew wall CAA3, a pair of of skew wall CAA3 are in pillar The both sides of C2, in addition skew wall CAA3 is to be less than pi/2 greater than zero with the size of the radian constituted between stretch section CA2.In this way, tiltedly Wall CAA3 allows scarfing plate CA1 to constitute go back to hook part on both sides, and what combination extruding CCB1 can be more firm in this way ensures scarfing plate The stabilization of CA1 is connected.
The skew wall CAA3 between the bottom wall CAA1 of scarfing plate include arcuation wall CAA2.Arcuation wall CAA2 can increase interlocking Plate CA1 put in set of shells CC2 when without hindrance performance, and avoid damage set of shells CC2.
The set of shells CC2 includes combining wall CCB2, is connected in conjunction with wall CCB2 with the bottom wall CAA1 of scarfing plate.In conjunction with wall After CCB2 connects with the bottom wall CAA1 of scarfing plate, the performance for securely living in scarfing plate CA1 can be improved.
The pair of extruding CCB1 is towards cavity C CB3 extending obliquely.It squeezes a CCB1 to stretch towards cavity C CB3, constitute Hook part is gone back to, it is possible thereby to more stable guarantee scarfing plate CA1's is bonded.
The number of the set of shells CC2 is a pair, and a pair of of set of shells CC2 rabbets with scarfing plate CA1；Via a pair of of sheath body Body CC2 can more preferably position scarfing plate.
Fuselage positioning port CC4 is arranged in described prop up on piece CC1；The piece CC1 that props up is via the same machine of fuselage positioning port CC4 Body is connected；
The fuselage positioning port CC4 is arranged in the both sides of scarfing plate CA1.Fuselage positioning port CC4 may get around interlocking in this way Plate CA1 is conducive to decompose and repair.
Having introduced positioning plate CCC2 avoids set of shells CC2 from occurring no small strain after compressing, so that scarfing plate CA1 is separated And go out；Positioning plate CCC2 the both sides set of shells CC2 constraint set of shells CC2 dependent variable, in this way via can allow the office of set of shells CC2 There is not small strain in portion, not only ensures that scarfing plate CA1 is put in without hindrance, scarfing plate after also preventing set of shells CC2 to oppress The separation of CA1 and go out.
The utility model is described by way of examples above, it will be understood by those of skill in the art that this public affairs It opens and is not limited to embodiments described above, without departing from the scope of the utility model, can make a variety of changes, change Become and replaces.

Claims (10)

1. a kind of element of the wireless charging device for Internet of Things cloud platform, which is characterized in that including electronic communication equipment without Line charge electric equipment comprising fuselage, pillar are fixedly connected on the upside of the fuselage；
The pillar is fixedly connected on the structure of the upside of the fuselage are as follows: the pillar is for rectangular-shape and by plastic material structure Connected via interlocking part with the upside of the fuselage at, the pillar, the interlocking part include the bottom of same pillar be connected it is embedding Fishplate bar, there are also what the upside with fuselage was connected to prop up platform.
2. the element of the wireless charging device according to claim 1 for Internet of Things cloud platform, which is characterized in that described Scarfing plate is molded of plastic material, and in addition the scarfing plate is connected with pillar integration.
3. the element of the wireless charging device according to claim 1 for Internet of Things cloud platform, which is characterized in that described Propping up platform includes propping up piece to be also connected in the set of shells for propping up on piece, and cavity is constituted in set of shells, is arranged in set of shells Squeeze item.
4. the element of the wireless charging device according to claim 3 for Internet of Things cloud platform, which is characterized in that described Scarfing plate is rabbeted into set of shells, squeezes item and is used to prevent scarfing plate from isolating cavity, the both sides of the set of shells are respectively set Couple item, connection item, which is connected in, props up on piece, couples and positioning plate is arranged on item, and positioning plate is used to push down set of shells.
5. the element of the wireless charging device according to claim 3 for Internet of Things cloud platform, which is characterized in that described Scarfing plate further includes stretch section, and stretch section is stretched according to the both sides of pillar.
6. the element of the wireless charging device according to claim 3 for Internet of Things cloud platform, which is characterized in that described Scarfing plate includes that the bottom wall of scarfing plate and a pair of of skew wall, a pair of of skew wall are in the both sides of pillar, and in addition skew wall is the same as between stretch section The size of the radian of composition is to be less than pi/2 greater than zero.
7. the element of the wireless charging device according to claim 6 for Internet of Things cloud platform, which is characterized in that described Skew wall between the bottom wall of scarfing plate include arcuation wall.
8. the element of the wireless charging device according to claim 6 for Internet of Things cloud platform, which is characterized in that described Set of shells includes combining wall, is connected in conjunction with wall with the bottom wall of scarfing plate.
9. the element of the wireless charging device according to claim 6 for Internet of Things cloud platform, which is characterized in that described A pair squeezes item all towards cavity extending obliquely.
10. the element of the wireless charging device according to claim 3 for Internet of Things cloud platform, which is characterized in that institute The number for stating set of shells is a pair, and a pair of of set of shells is all rabbeted with scarfing plate；
Fuselage positioning port is arranged in the on piece of propping up；It is described prop up piece via fuselage positioning port with fuselage be connected；
The fuselage positioning port is arranged in the both sides of scarfing plate.
CN201822202966.XU 2018-12-26 2018-12-26 For the element of the wireless charging device of Internet of Things cloud platform Active CN209626991U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201822202966.XU CN209626991U (en) 2018-12-26 2018-12-26 For the element of the wireless charging device of Internet of Things cloud platform

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201822202966.XU CN209626991U (en) 2018-12-26 2018-12-26 For the element of the wireless charging device of Internet of Things cloud platform

Publications (1)

Publication Number Publication Date
CN209626991U true CN209626991U (en) 2019-11-12

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Application Number Title Priority Date Filing Date
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Country Status (1)

Country Link
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Effective date of registration: 20221110

Address after: 710000 Room 417, Jiabei Building, Keji Second Road, Xi'an Hi tech Zone, Shaanxi Province

Patentee after: Shaanxi hailsen Electronic Technology Co.,Ltd.

Address before: 710,065 Room 32,106, Building 2, No. 86, Gaoxin Road, High tech Zone, Xi'an, Shaanxi

Patentee before: XI'AN YUBIN INFORMATION TECHNOLOGY Co.,Ltd.