CN204521497U - Vibration aircraft cup - Google Patents
Vibration aircraft cup Download PDFInfo
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- CN204521497U CN204521497U CN201520081140.6U CN201520081140U CN204521497U CN 204521497 U CN204521497 U CN 204521497U CN 201520081140 U CN201520081140 U CN 201520081140U CN 204521497 U CN204521497 U CN 204521497U
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- end cap
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Abstract
The utility model discloses a kind of vibration aircraft cup, comprise cup, vibration component, compression assemblies and Control Component, vibration component and compression assemblies are all electrically connected with Control Component; Cup comprises glass body and end cap, and end cap is detachably connected on the first end of glass body; Vibration component is arranged in glass body, comprises flexible glue inner bag, at least one vibrating motor and drive circuit board; Compression assemblies comprises at least one annular air-pocket and air pump, and air pump is arranged in end cap; Control Component comprises control circuit board and battery, and control circuit board and battery are all arranged in end cap; Control circuit board is provided with several probe, several probe stretches out end cap and contacts with drive circuit board and conduct electricity.Vibration aircraft cup of the present utility model, by the setting of annular air-pocket, can extrude flexible glue inner bag periphery entirety, improves Consumer's Experience effect; Further, the Control Component in end cap is electrically connected with the wireless way of contact by the vibration component in probe and cup body, improves aircraft cup service life.
Description
Technical field
This utility model relates to a kind of Mature Audiences, particularly relates to a kind of vibration aircraft cup.
Background technology
Along with the requirement of user to experience effect is more and more higher, Mature Audiences kind, function also get more and more, and vibration aircraft cup is the Mature Audiences of wherein a kind of male.Current vibration aircraft cup is that the motor oscillating by arranging in it drives inner bag vibration mostly, reaches user and wants experience effect.For increasing the squeezing effect of vibration aircraft cup, being also provided with air bag in some vibration aircraft cups, shrinking extruding inner bag by air bag.But those vibration aircraft cups adopt the air bag of strip usually, and the contraction of air bag can only extrude inner bag local side, and Consumer's Experience effect is also bad.
In addition, in vibration aircraft cup, control section and oscillating component are generally arranged in cup and bowl cover respectively, and are connected by wire, and wire easily disconnects at cup and bowl cover disassembly process, causes aircraft cup to damage.
Utility model content
The technical problems to be solved in the utility model is, provides a kind of vibration aircraft cup improving Consumer's Experience effect.
This utility model solves the technical scheme that its technical problem adopts: provide a kind of intelligent vibration aircraft cup, comprise cup, vibration component, compression assemblies and Control Component, described vibration component and compression assemblies are all electrically connected with described Control Component; Described cup comprises the cup body of hollow and the end cap of hollow, and described end cap is detachably connected on the first end of described cup body, and the second end of described cup body is open end;
Described vibration component is arranged in described cup body, and this vibration component comprises middle part and is formed with the flexible glue inner bag of a passage, drive circuit board that at least one is arranged on the vibrating motor on described flexible glue inner bag periphery and is electrically connected with described vibrating motor; One end of described flexible glue inner bag is provided with the opening with described channel connection, and described opening is positioned at the second end of described cup body; Described drive circuit board is positioned at the first end of described cup body near described end cap;
Described compression assemblies comprise at least one to be set on described flexible glue inner bag periphery, by inflation or aerofluxus to extrude the annular air-pocket of described flexible glue inner bag, and the air pump being connected with described air bag, described air bag is inflated or bled; Described air pump is arranged in described end cap;
Described Control Component comprises control circuit board and is electrically connected with described control circuit board and the battery of powering for described vibrating motor, and described control circuit board and battery are all arranged in described end cap; Described control circuit board is provided with several probe, and several described probe stretches out described end cap and contacts with described drive circuit board and conduct electricity, and described drive circuit board is electrically connected with described control circuit board by described probe.
Preferably, described Control Component also comprises and is positioned at described end cap and the power supply circuit board be electrically connected with described control circuit board, is arranged on described power supply circuit board and exposes the switch key of described end cap, described end cap offers the through hole exposed for described switch key.
Preferably, described end cap is also provided with touch control panel, described touch control panel is electrically connected with described control circuit board.
Preferably, described drive circuit board is provided with several corresponding with several described probe respectively and contact of conducting electricity for described probes touch;
Described contact is be arranged on described drive circuit board conductive layer or the jack studding with conductive layer that is opened on described drive circuit board on the surface.
Preferably, described end cap is tapered, and described end cap is connected on the first end of described cup body with one end that internal diameter is larger.
Preferably, the first end of described cup body is open end; Described cup also comprises the connection cover be connected between described end cap and described cup body first end, and described connection cover is provided with the hole portion passed for described probe.
Preferably, described cup also comprises the bowl cover covered on described cup body second end.
Preferably, described control circuit board comprises the first main control unit, for intelligent terminal's wireless telecommunications, receive the control instruction from described intelligent terminal and export described first main control unit to carry out the first radio communication unit processed;
Described first radio communication unit comprise in WIFI unit, bluetooth unit, 3G/4G unit, ZigBee unit, UWB unit and infrared unit one or more.
Preferably, described Control Component also comprise be electrically connected with described first main control unit for gathering the pressure data on described flexible glue inner bag surface and the pressure data collected being exported to described first main control unit, be sent to the pressure transducer of described intelligent terminal by described first radio communication unit.
Preferably, described control circuit board also comprises the charhing unit and power supply unit that are electrically connected with described first main control unit;
Described control circuit board also comprises and being electrically connected with described first main control unit, for detecting the detecting unit of the electricity of described battery.
The beneficial effects of the utility model: by the setting of annular air-pocket, can extrude flexible glue inner bag periphery entirety, improve Consumer's Experience effect; Further, the Control Component in end cap is electrically connected with the wireless way of contact by the vibration component in probe and cup body, improves aircraft cup service life.
In addition, by the setting of radio communication unit on control circuit board, vibration aircraft cup and intelligent terminal can be connected, user controls vibration aircraft cup by intelligent terminal, improves user's sense of participation, substantially increases Consumer's Experience.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is described in further detail, in accompanying drawing:
Fig. 1 is the perspective view of the vibration aircraft cup of this utility model one embodiment;
Fig. 2 is the decomposition texture schematic diagram of cup in the aircraft of vibration shown in Fig. 1 cup;
Fig. 3 is the cross-sectional view of the aircraft of vibration shown in Fig. 1 cup;
Fig. 4 is the explosive view of the aircraft of vibration shown in Fig. 1 cup;
Fig. 5 is the circuit diagram of the first main control unit in this utility model one embodiment;
Fig. 6 is the circuit diagram of the first radio communication unit in this utility model one embodiment;
Fig. 7 is the circuit diagram of drive circuit in this utility model one embodiment;
Fig. 8 is the circuit diagram of charhing unit in this utility model one embodiment;
Fig. 9 is the circuit diagram of power supply unit in this utility model one embodiment;
Figure 10 is the circuit diagram of detecting unit in this utility model one embodiment;
Figure 11 is the circuit diagram of memory element in this utility model one embodiment;
Figure 12 is the circuit diagram of clock unit in this utility model one embodiment;
Figure 13 is the circuit diagram of electrification reset unit in this utility model one embodiment.
Detailed description of the invention
In order to there be understanding clearly to technical characteristic of the present utility model, object and effect, now contrast accompanying drawing and describe detailed description of the invention of the present utility model in detail.
As Figure 1-4, the vibration aircraft cup of this utility model one embodiment, comprises the cup of hollow, the vibration component be arranged in cup, compression assemblies and Control Component, and vibration component and compression assemblies are all electrically connected with Control Component; Vibration component vibrates under control unit controls, and compression assemblies extrudes vibration component under control unit controls, and realizes vibration and the squeezing effect of vibration aircraft cup.
Cup comprises the cup body 10 of hollow and the end cap 20 of hollow, and end cap 20 is detachably connected on the first end of glass body 10.End cap 20 and the connected mode of cup body 10 can be the modes such as buckle is connected, magnet adsorption connection.For convenience of gripping, cup body 10 is cylinder-like structure.Cup body 10 and end cap 20 can adopt rigid plastics to make.
Vibration component is arranged in glass body 10.This vibration component can comprise flexible glue inner bag 31, at least one vibrating motor 32 and drive circuit board 33.Be formed with a passage 310 in the middle part of flexible glue inner bag 31, and one end of flexible glue inner bag 31 is provided with the opening 311 be communicated with passage 310, this opening 311 is positioned at the second end of glass body 10.Second end of cup body 10 is open end, thus this open end is communicated with successively with opening 311, passage 310.Flexible glue inner bag 31 can adopt silica gel to make, and has certain elasticity, can restore after crimp.For location flexible glue inner bag 31, be also provided with ring compression circle 312 between this flexible glue inner bag 31 and cup body 10, this compacting ring 312 is set in flexible glue inner bag 31 periphery and closely cooperates with cup body 10 internal face.
Vibrating motor 32 is arranged on the periphery of flexible glue inner bag 31, thus flexible glue inner bag 31 can be driven when vibrating motor 32 vibrates to vibrate.For making vibrating motor 32 can be fixed on flexible glue inner bag 31, the circumferential lateral surface of this flexible glue inner bag 31 can be provided with groove 313, is embedded wherein for vibrating motor 32.Drive circuit board 33 is electrically connected with vibrating motor 32, vibrates and control its intensity for driving vibrating motor 32.As shown in Figure 3, preferably, drive circuit board 33 is positioned at the first end of glass body 10 near end cap 20.Drive circuit board 33 periphery can sheathed sealing ring 331, to be close-coupled on glass body 10, also plays waterproof effect by sealing ring 331.
The air pump 42 that compression assemblies can comprise at least one annular air-pocket 41 and be connected with air bag 41; Air bag 41 is set on the periphery of flexible glue inner bag 31, and it is by inflation or aerofluxus extruding flexible glue inner bag 31; Air pump 42 is arranged in end cap 20, for inflating air bag 41 or bleeding.When air pump 42 pairs of air bags 41 pass in and out inflation, air bag 41 expands and extrudes flexible glue inner bag 31, can make passage 310 flexural deformation in flexible glue inner bag 31.
Control Component can comprise control circuit board 51 and be electrically connected with control circuit board 51 and the battery 52 of powering for vibrating motor 32, and control circuit board 51 and battery 52 are all arranged in end cap 20.Wherein, control circuit board 51 is provided with several probe 53, several probe 53 stretches out end cap 20 and contacts with drive circuit board 33 and conduct electricity, and drive circuit board 33 is electrically connected with control circuit board 51 by probe 53.Drive circuit board 33 is provided with several corresponding with several probe 53 respectively and contact the contact 332 of conducting electricity for probe 53.Contact 332 can be and is arranged on drive circuit board 33 conductive layer on the surface, and probe 53 is by being electrically connected with drive circuit board 33 with conductive layers make contact; Or contact 332 also can be the jack studding with conductive layer be opened on drive circuit board 33, probe 53 is electrically connected with drive circuit board 33 by being plugged in jack.
When end cap 20 is pulled down on cup body 10, probe 53 departs from drive circuit board 33, thus control circuit board 51 and drive circuit board 33 disconnect; When end cap 20 is installed on glass body 10, probe 53 contacts with drive circuit board 33 and conducts electricity, and realizes the conducting of drive circuit board 33 and control circuit board 51.Drive circuit board 33 drives vibrating motor 32 to vibrate under the control of control circuit board 51; In addition, battery 52 is powered for vibrating motor 32 by control circuit board 51.Battery 52 preferably adopts rechargeable battery, and end cap 20 is provided with the charging inlet (not shown) be electrically connected with control circuit board 51, can be charged by this charging inlet external power supply to battery 52.
In addition, Control Component also comprises power supply circuit board 54 and switch key 55, and power supply circuit board 54 is positioned at end cap 20 and is electrically connected with control circuit board 51, and switch key 55 to be arranged on power supply circuit board 54 and to expose end cap 20.When pressing switch key 55, switch key 55 triggering voltage circuit board 54, opens and closes this vibration aircraft cup by control circuit board 51.Switch key 55 can adopt translucent silica gel material to make, and power supply circuit board 54 can be provided with LED to illuminate this switch key 55.Accordingly, end cap 20 offers the through hole 25 exposed for switch key 55.Can gap be had between through hole 25 and switch key 55, for air circulation, facilitate air pump 42 pairs of air bags 41 inflate or bleed; Or, also can offer QI KOU on end cap 20.
In the present embodiment, end cap 20 is tapered, thus has cone space in end cap 20 with elements such as accommodating control circuit board 51, batteries 52.This end cap 20 is connected on the first end of glass body 10 with one end that internal diameter is larger.One end end face that end cap 20 internal diameter is larger is sealed by a seal cover 21, and control circuit board 51 and battery 52 etc. can be fixed on sealing lid 21 towards on the surface inside end cap 20.Probe 53 one end is connected on control circuit board 51, and the other end passes seal cover 21 to expose end cap 20.
Further, in cup, end cap 20 also can be provided with touch control panel 22, touch control panel 22 is electrically connected with control circuit board 51.User selects the functions such as the oscillation intensity of vibration aircraft cup by touch control panel 22.Touch control panel 22 is arranged on end cap 20 by light guide support 23; Can be provided with inner liner 24 between light guide support 23 and touch control panel 22, inner liner 24 can be EVA foam.
Further, in the present embodiment, the first end of cup body 10 is open end; Cup also comprises the connection cover 30 be connected between end cap 20 and cup body 10 first end, and connection cover 30 is provided with the hole portion 301 passed for probe 53.Probe 53 other end passing seal cover 21 can be worn via portion 301 and contact with the contact 332 on drive circuit board 33 and conduct electricity.Drive circuit board 33 can be fixed in glass body 10 second end by self-tapping screw near connection cover 30, is also fixed on the side of connection cover 30 towards cup body 10 by self-tapping screw.In other embodiments, connection cover 30 also can be integrally formed on the second end of glass body 10, thus cup body 10 second end forms blind end.
In addition, in the present embodiment, cup also comprises the bowl cover 40 covered on cup body 10 second end.When vibrating aircraft cup and not using, the second end of cup body 10 is closed by bowl cover 40, thus is also closed by the opening 311 of flexible glue inner bag 31.For convenience of covering and dismounting of bowl cover 40, the second end of cup body 10 is also provided with ring compression lid 11, and bowl cover 40 is connected by the mode such as buckle, magnetic with this friction top 11.As shown in Figure 3, in the present embodiment, one end that flexible glue inner bag 31 has an opening 311 is exposed glass body 10 second end and is covered by the second end end face, and therefore friction top 11 is set in flexible glue inner bag 31 and has on the periphery, one end of opening 311 on cup body 10 second end.
This vibration aircraft cup also can be connected with intelligent terminal 2 wireless telecommunications, and both can form vibration aircraft cup intelligence control system, can carry out Based Intelligent Control by intelligent terminal 2 to vibration aircraft cup; Intelligent terminal 2 can be the terminal unit of smart mobile phone, computer, Ipad or other types.
In the Control Component of vibration aircraft cup, control circuit board 15 can comprise the first main control unit and the first radio communication unit, first radio communication unit is used for and intelligent terminal's wireless telecommunications, receives the control instruction from intelligent terminal and export the first main control unit to process for the first main control unit.First main control unit controls vibration aircraft cup according to control instruction and performs corresponding function.Intelligent terminal can comprise the second main control unit and the second radio communication unit, second radio communication unit is used for and the wireless telecommunications of vibration aircraft cup, second main control unit is connected with the second radio communication unit, and by the second radio communication unit, control instruction is sent to vibration aircraft cup.
Preferably, the first radio communication unit can comprise one or more in WIFI unit, bluetooth unit, 3G/4G unit, ZigBee unit, UWB unit and infrared unit.Second radio communication unit may correspond to comprise in WIFI unit, bluetooth unit, 3G/4G unit, ZigBee unit, UWB unit and infrared unit one or more.Vibration aircraft cup and intelligent terminal can be operated in online mode, that is, vibration aircraft cup and intelligent terminal are connected by WIFI, bluetooth, ZigBee, UWB, infrared mode.Vibration aircraft cup and intelligent terminal also can be operated in distance control mode, that is, vibration aircraft cup and intelligent terminal are by WIFI, 3G/4G accessing Internet respectively, then both sides log in, and be mutually good friend, invite Long-distance Control and after being accepted by the other side, just can realize Long-distance Control.
Fig. 5 is the circuit diagram of the first main control unit in the present embodiment.First main control unit comprises the first main control chip U1, and the first main control chip U1 is provided with some interfaces for being connected with other unit.
Fig. 6 shows the circuit diagram of the first radio communication unit.Composition graphs 5,6, first radio communication unit comprises WIFI circuit and Bluetooth circuit, WIFI circuit comprises the inductance L 4 and WIFI antenna WIFI_ANT that are connected with the WIFI antenna leads of the first main control chip U1, inductance L 4 two ends respectively by electric capacity C10, C12 ground connection, to reach the object of voltage stabilizing.Bluetooth circuit comprises the electric capacity C7, inductance L 2, inductance L 1, electric capacity C8, inductance L 3 and the Bluetooth antenna BT_ANT that are connected in series, the power output end (VDD-PA) of the first main control chip U1 is connected between electric capacity C7 and inductance L 2, the antennal interface (ANT1, ANT2) of the first main control chip U1 is connected to the two ends of inductance L 1, inductance L 3 two ends respectively by electric capacity C9, C11 ground connection, to reach the object of Antenna Impedance Matching.
In the present embodiment, as shown in Figure 3,4, vibrating motor 32 comprises two, is electrically connected respectively with drive circuit 33.Fig. 7 shows the circuit diagram of drive circuit 33; Composition graphs 5,7, drive circuit 33 comprises the first motor circuit being respectively used to control two vibrating motors 32 and the second motor circuit that are connected with the first main control chip U1.First motor circuit comprises resistance R4, audion Q1, motor JP1 and resistance R1, under the control of the first main control chip U1, controls motor JP1 work; First motor circuit also comprises electric capacity C13, electric capacity C2 and diode D1 for realizing voltage stabilizing; The positive pole of diode D1 connects the colelctor electrode of audion Q1, the negative pole of diode D1 connects supply voltage (VBAT) by resistance R1, the base stage of audion Q1 connects the PWM0 interface of the first main control chip U1 by resistance R4, the grounded emitter of audion Q1, the colelctor electrode of audion Q1 connects supply voltage (VBAT) by motor JP1, resistance R1, between the base stage that electric capacity C13 is connected to audion Q1 and emitter stage, electric capacity C2 is connected to the two ends of motor JP1.Second motor circuit comprises resistance R5, audion Q2, motor JP2 and resistance R2, under the control of the first main control chip U1, controls motor JP2 work; Second motor circuit also comprises electric capacity C14, electric capacity C3 and diode D2 for realizing voltage stabilizing; The base stage of audion Q2 connects the PWM1 pin of the first main control chip U1 by resistance R5, the grounded emitter of audion Q2, the colelctor electrode of audion Q2 connects supply voltage (VBAT) by motor JP2, resistance R2, between the base stage that electric capacity C14 is connected to audion Q2 and emitter stage, electric capacity C3 is connected to the two ends of motor JP2, the positive pole of diode D2 connects the colelctor electrode of audion Q2, and the negative pole of diode D2 connects supply voltage (VBAT) by resistance R2.
In the present embodiment, control circuit board 51 also comprises the charhing unit and power supply unit that are electrically connected with the first main control unit.External power supply is stored in battery 52 by charhing unit, and battery is that the first main control unit and vibrating motor 32 are powered by power supply unit.Fig. 8 shows the circuit diagram of charhing unit in the present embodiment.Composition graphs 5,8, charhing unit comprises charging chip U3, and charging chip U3 is connected with internal battery interface JP4 with external power interface JP3, and charging chip U3 is connected with the GHAGDET interface of the first main control chip U1.Charhing unit also comprises electric capacity C4 for realizing voltage stabilizing and resistance R7; One end of external power interface JP3 is connected with charging chip U3, other end ground connection; Also be provided with the port meeting 5V voltage (VCC5V) between charging chip U3 and external power interface JP3, between charging chip U3 and internal battery interface JP4, be also provided with supply voltage (VBAT) outfan.Fig. 9 shows the circuit diagram of power supply unit in the present embodiment; Composition graphs 5,9, power supply unit comprises power supply chip U4, the input VIN of power supply chip U4 is connected with supply voltage (VBAT) interface of other circuit, outfan VOUT connects 3.3V voltage (VCC3V3), and the voltage transitions for being inputted by VBAT interface becomes 3.3V voltage to export.The Enable Pin EN of power supply chip U4 is connected with the negative pole of diode D4, the positive pole of diode D4 can be accessed by be connected with other circuit resistance R9, ground connection resistance R17 or connect and access interrupteur SW 1, resistance R10.The Enable Pin EN of power supply chip U4 also can be connected with resistance R24, the diode D3 of series connection, and the other end of resistance R24 can connect 5V voltage (VCC5V) interface.The Enable Pin EN of power supply chip U4 also can be connected by diode D5 with other circuit.Understandably, power supply unit also comprises electric capacity C33, C15, C5, C31 for realizing voltage stabilizing object and resistance R20, R33.
Control circuit board 51 also can comprise detecting unit, and it is electrically connected with the first main control unit, for detecting the electricity of battery 52.First main control unit is sent to intelligent terminal by the first radio communication unit after processing detected information about power.Then, second main control unit of intelligent terminal is processed the information about power received by the second radio communication unit, and shows by the display unit of intelligent terminal self.Preferably, this detecting unit, except detecting except the information about power of battery, detects the voltage of external power source, and feeds back to the first main control unit when being also used in charging.The alarm unit of intelligent terminal can produce warning message according to current electric quantity (information about power received).
Figure 10 shows the circuit diagram of detecting unit in the present embodiment.Composition graphs 5,10, detecting unit comprises that one end is connected with the CHAGDET interface of the first main control chip U1, the resistance R23 of another termination 3.3V voltage (VCC3V3), and during for detecting charging, whether battery is full of.Detecting unit also comprises and being connected with the USB_DET interface of the first main control chip U1, the resistance R21 of another termination 5V voltage (VCC5V), the resistance R22 of ground connection is also connected with, for detecting the 5V voltage exported between first main control chip U1 and resistance R21.Detecting unit also comprises and being connected with the BAT_DET interface of the first main control chip U1, the resistance R18 that the other end is connected with supply voltage (VBAT), the resistance R19 of ground connection is also connected with, for detecting the circuit accessed by supply voltage (VBAT) port between first main control chip U1 and resistance R18.
Further, Control Component also can comprise the pressure transducer (not shown) be connected with the first main control unit; Pressure transducer is arranged on flexible glue inner bag 31.This pressure transducer for gathering the pressure data on flexible glue inner bag 31 surface, and exports the pressure data collected to first main control unit, is sent to intelligent terminal by the first radio communication unit.Intelligent terminal then receives this pressure data by the second radio communication unit, and export the second main control unit to, second main control unit can generate pressure regulating control command according to this pressure data, control vibrating motor 32 carries out corresponding vibration or air pump 42 carries out inflating or bleeding, thus regulates oscillation intensity or the crushing strength of vibration aircraft cup.
In addition, control circuit board 15 also can comprise be connected with the first main control unit respectively for store data (comprising the various data such as pressure) memory element, for providing the clock unit and electrification reset unit etc. of clock signal; When charging to vibration aircraft cup, once resetted by this electrification reset unit.
Figure 11 illustrates the circuit diagram of memory element in the present embodiment; Composition graphs 5,11, memory element comprises storage chip U2, and storage chip is connected with the first main control chip U1 with clock cable SCL by data wire SDA, and its power end VCC connects 3.3V voltage (VCC3V3).Figure 12 illustrates the circuit diagram of clock unit in the present embodiment; Composition graphs 5,12, clock unit comprises the crystal oscillator X1 that is connected with the first main control chip U1 and in order to the electric capacity C17 of voltage stabilizing and electric capacity C18; Two clock ends BT_XIN, BT_XO of first main control chip U1 connect the two ends of crystal oscillator X1, and the two ends of crystal oscillator X1 are respectively by electric capacity C17, C18 ground connection.Figure 13 illustrates the circuit diagram of electrification reset unit in the present embodiment; Composition graphs 5,13, electrification reset unit comprises audion Q3, the base stage of audion Q3 connects 5V voltage (VCC5V) by electric capacity C19, the grounded emitter of audion Q3, the colelctor electrode of audion Q3 connects the reset terminal SWDIO of the first main control chip U1, is connected with the resistance R12 of ground connection between base stage and electric capacity C19.
From the above, in this vibration aircraft cup, by settings such as radio communication units on control circuit board, vibration aircraft cup and intelligent terminal can be connected, user controls vibration aircraft cup by intelligent terminal, improves user's sense of participation, substantially increases Consumer's Experience.
The foregoing is only embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every utilize this utility model description and accompanying drawing content to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present utility model.
Claims (10)
1. a vibration aircraft cup, is characterized in that, comprises cup, vibration component, compression assemblies and Control Component, and described vibration component and compression assemblies are all electrically connected with described Control Component; Described cup comprises the cup body (10) of hollow and the end cap (20) of hollow, and described end cap (20) is detachably connected on the first end of described cup body (10), and the second end of described cup body (10) is open end;
Described vibration component is arranged in described cup body (10), and this vibration component comprises middle part and is formed with the flexible glue inner bag (31) of a passage (310), drive circuit board (33) that at least one is arranged on the vibrating motor (32) on described flexible glue inner bag (31) periphery and is electrically connected with described vibrating motor (32); One end of described flexible glue inner bag (31) is provided with the opening (311) be communicated with described passage (310), and described opening (311) is positioned at the second end of described cup body (10); Described drive circuit board (33) is positioned at the first end of described cup body (10) near described end cap (20);
Described compression assemblies comprise at least one to be set on described flexible glue inner bag (31) periphery, by inflation or aerofluxus to extrude the annular air-pocket (41) of described flexible glue inner bag (31), and the air pump (42) being connected with described air bag (41), described air bag (41) being inflated or bleeds; Described air pump (42) is arranged in described end cap (20);
Described Control Component comprises control circuit board (51) and is electrically connected and the battery (52) of powering for described vibrating motor (32) with described control circuit board (51), and described control circuit board (51) and battery (52) are all arranged in described end cap (20); Described control circuit board (51) is provided with several probe (53), several described probe (53) is stretched out described end cap (20) and is contacted with described drive circuit board (33) and conduct electricity, and described drive circuit board (33) is electrically connected with described control circuit board (51) by described probe (53).
2. vibration aircraft cup according to claim 1, it is characterized in that, described Control Component also comprises and is positioned at described end cap (20) and the power supply circuit board (54) be electrically connected with described control circuit board (51), to be arranged on described power supply circuit board (54) upper and expose the switch key (55) of described end cap (20), described end cap (20) offers the through hole (25) exposed for described switch key (55).
3. vibration aircraft cup according to claim 2, is characterized in that, described end cap (20) is also provided with touch control panel (22), and described touch control panel (22) is electrically connected with described control circuit board (51).
4. vibration aircraft cup according to claim 1, is characterized in that, described drive circuit board (33) be provided with several corresponding with several described probe (53) respectively and for described probe (53) contact the contact (332) of conducting electricity;
Described contact (332) is for being arranged on described drive circuit board (33) conductive layer or the jack studding with conductive layer that is opened on described drive circuit board (33) on the surface.
5. vibration aircraft cup according to claim 1, is characterized in that, described end cap (20) is tapered, and described end cap (20) is connected on the first end of described cup body (10) with one end that internal diameter is larger.
6. vibration aircraft cup according to claim 1, is characterized in that, the first end of described cup body (10) is open end; Described cup also comprises the connection cover (30) be connected between described end cap (20) and described cup body (10) first end, and described connection cover (30) is provided with the hole portion (301) passed for described probe (53).
7. vibration aircraft cup according to claim 1, is characterized in that, described cup also comprises the bowl cover (40) covered on described cup body (10) second end.
8. the vibration aircraft cup according to any one of claim 1-7, it is characterized in that, described control circuit board (51) comprises the first main control unit, for intelligent terminal's wireless telecommunications, receive the control instruction from described intelligent terminal and export described first main control unit to carry out the first radio communication unit processed;
Described first radio communication unit comprise in WIFI unit, bluetooth unit, 3G/4G unit, ZigBee unit, UWB unit and infrared unit one or more.
9. vibration aircraft cup according to claim 8, it is characterized in that, described Control Component also comprise be electrically connected with described first main control unit for gathering the pressure data on described flexible glue inner bag surface and the pressure data collected being exported to described first main control unit, be sent to the pressure transducer of described intelligent terminal by described first radio communication unit.
10. vibration aircraft cup according to claim 8, is characterized in that, described control circuit board (51) also comprises the charhing unit and power supply unit that are electrically connected with described first main control unit;
Described control circuit board (51) also comprises and being electrically connected with described first main control unit, for detecting the detecting unit of the electricity of described battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520081140.6U CN204521497U (en) | 2015-02-04 | 2015-02-04 | Vibration aircraft cup |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520081140.6U CN204521497U (en) | 2015-02-04 | 2015-02-04 | Vibration aircraft cup |
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| Publication Number | Publication Date |
|---|---|
| CN204521497U true CN204521497U (en) | 2015-08-05 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520081140.6U Expired - Fee Related CN204521497U (en) | 2015-02-04 | 2015-02-04 | Vibration aircraft cup |
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| CN (1) | CN204521497U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104622677A (en) * | 2015-02-04 | 2015-05-20 | 深圳市无碍互动科技开发有限公司 | Vibrating masturbation cup |
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2015
- 2015-02-04 CN CN201520081140.6U patent/CN204521497U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104622677A (en) * | 2015-02-04 | 2015-05-20 | 深圳市无碍互动科技开发有限公司 | Vibrating masturbation cup |
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