CN105287183A - Masturbation cup - Google Patents
Masturbation cup Download PDFInfo
- Publication number
- CN105287183A CN105287183A CN201510829371.5A CN201510829371A CN105287183A CN 105287183 A CN105287183 A CN 105287183A CN 201510829371 A CN201510829371 A CN 201510829371A CN 105287183 A CN105287183 A CN 105287183A
- Authority
- CN
- China
- Prior art keywords
- cup
- massage
- bowl cover
- swivel becket
- sleeve pipe
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 230000007246 mechanism Effects 0.000 claims abstract description 22
- 239000011324 bead Substances 0.000 claims description 18
- 238000003032 molecular docking Methods 0.000 claims description 6
- 230000005540 biological transmission Effects 0.000 abstract 2
- 239000003921 oil Substances 0.000 description 31
- 239000010687 lubricating oil Substances 0.000 description 8
- 230000000694 effects Effects 0.000 description 7
- 238000000034 method Methods 0.000 description 6
- 230000008569 process Effects 0.000 description 6
- 239000000446 fuel Substances 0.000 description 4
- 230000001276 controlling effect Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000036541 health Effects 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000000741 silica gel Substances 0.000 description 2
- 229910002027 silica gel Inorganic materials 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 210000004392 genitalia Anatomy 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 229920003002 synthetic resin Polymers 0.000 description 1
- 239000000057 synthetic resin Substances 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61H—PHYSICAL THERAPY APPARATUS, e.g. DEVICES FOR LOCATING OR STIMULATING REFLEX POINTS IN THE BODY; ARTIFICIAL RESPIRATION; MASSAGE; BATHING DEVICES FOR SPECIAL THERAPEUTIC OR HYGIENIC PURPOSES OR SPECIFIC PARTS OF THE BODY
- A61H19/00—Massage for the genitals; Devices for improving sexual intercourse
- A61H19/30—Devices for external stimulation of the genitals
- A61H19/32—Devices for external stimulation of the genitals for inserting the genitals therein, e.g. vibrating rings for males or breast stimulating devices
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61H—PHYSICAL THERAPY APPARATUS, e.g. DEVICES FOR LOCATING OR STIMULATING REFLEX POINTS IN THE BODY; ARTIFICIAL RESPIRATION; MASSAGE; BATHING DEVICES FOR SPECIAL THERAPEUTIC OR HYGIENIC PURPOSES OR SPECIFIC PARTS OF THE BODY
- A61H15/00—Massage by means of rollers, balls, e.g. inflatable, chains, or roller chains
- A61H15/0078—Massage by means of rollers, balls, e.g. inflatable, chains, or roller chains power-driven
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61H—PHYSICAL THERAPY APPARATUS, e.g. DEVICES FOR LOCATING OR STIMULATING REFLEX POINTS IN THE BODY; ARTIFICIAL RESPIRATION; MASSAGE; BATHING DEVICES FOR SPECIAL THERAPEUTIC OR HYGIENIC PURPOSES OR SPECIFIC PARTS OF THE BODY
- A61H2205/00—Devices for specific parts of the body
- A61H2205/08—Trunk
- A61H2205/087—Genitals
Landscapes
- Health & Medical Sciences (AREA)
- Epidemiology (AREA)
- Pain & Pain Management (AREA)
- Physical Education & Sports Medicine (AREA)
- Rehabilitation Therapy (AREA)
- Life Sciences & Earth Sciences (AREA)
- Animal Behavior & Ethology (AREA)
- General Health & Medical Sciences (AREA)
- Public Health (AREA)
- Veterinary Medicine (AREA)
- Reproductive Health (AREA)
- Massaging Devices (AREA)
Abstract
The invention provides a masturbation cup. The cup comprises a cup body, an upper cup cover, a lower cup cover, a massaging mechanism, an oil pump, a transmission mechanism and a controller, wherein the upper cup cover and the lower cup cover are respectively arranged at upper and lower ends of the cup body, the upper cup cover is a closed end, while the lower cup cover is an opening end with a port; the massaging mechanism comprises a massaging part arranged in the cup body and a massaging sleeve with a space for accommodating the massaging part; the massaging sleeve is connected with the cup body in a movable connection mode; the massaging part is positioned outside the massaging sleeve, and can move along the outer wall of the massaging sleeve under driving of the transmission mechanism so as to apply pressure to the massaging sleeve; and the oil pump is fixedly arranged in the cup body, is positioned in the region of the upper cup cover or the lower cup cover, and is connected to the massaging sleeve by virtue of an oil pump pipeline. Therefore, the convenience and massaging comfort level when the masturbation cup is used can be improved.
Description
Technical field
The present invention relates to health treatment for adults articles for use, particularly a kind of aircraft cup.
Background technology
Aircraft cup belongs to men's portable class health treatment for adults articles for use, uses its massage functions to make male genitals reach health-care effect, and the psychological need of health.
Aircraft cup is normally made up of soft synthetic resin or silica gel, also exists and uses cheap sponge to make.Aircraft cup can be divided into again breakthrough form and non-penetrating shape according to profile, and main difference is whether tail end is closed exactly.
There are following two aspect shortcomings in the aircraft cup of prior art, on the one hand, owing to adopting large capacity motor to add eccentric drive form, realize vibration massage function, this kind of massaging way dullness is uninteresting, and noise is large, and comfort is poor; On the other hand, usually needing to utilize outside oil pump to add lubricating oil to the massage mechanism of aircraft cup inside for improving comfort level, causing using inconvenient, and the technological deficiency such as massaging way is comparatively single, massage area is limited.
How to provide a kind of built-in oil pump and aircraft cup closer to the massage functions of human body own physiological demand becomes those skilled in the art's technical issues that need to address.
Summary of the invention
The technical problem to be solved in the present invention how to provide a kind of aircraft cup, to solve the problems of the technologies described above.
For solving the problems of the technologies described above, the invention provides a kind of aircraft cup, comprising: cup, upper bowl cover, lower bowl cover, massage mechanism, oil pump, drive mechanism and controller;
Wherein, described upper bowl cover and lower bowl cover are arranged at the upper and lower two ends of described cup respectively, and described upper bowl cover is blind end, and described lower bowl cover is the open end with port;
Described massage mechanism comprises: be arranged at the Massage part in described cup and have the massage sleeve pipe holding Massage Department's bit space, and described massage sleeve pipe adopts the mode connected of living to be connected with cup; Described Massage part is positioned at the outside of described massage sleeve pipe, and under the driving of described drive mechanism, can move, exert pressure to described massage sleeve pipe along the outer wall of described massage sleeve pipe;
Described oil pump sets firmly and is placed in described cup, and is positioned at the region of described upper bowl cover or lower bowl cover, is connected in described massage sleeve pipe by oil pump pipeline.
Preferably, comprising: upper fixed disk and lower fixed disk, be arranged at described upper bowl cover bottom and described lower bowl cover top respectively, described oil pump is arranged between described upper bowl cover and fixed dish.
Preferably, described drive mechanism comprises: upper passive rotating disk, lower passive rotating disk, drivewheel, drive motors, connecting rod and swivel becket;
Described swivel becket is mobilizable to be connected on described connecting rod, and the two ends of described connecting rod connect described passive rotating disk and lower passive rotating disk respectively, and described passive rotating disk is connected with described cup upper end, and described lower passive rotating disk is connected with described cup bottom; Described swivel becket is described between passive rotating disk and lower passive rotating disk; Described drive motors drives described drivewheel to rotate, and described drivewheel drives described passive dial rotation, and described passive rotating disk drives described swivel becket and described lower passive dial rotation by described connecting rod.
Preferably, comprise: limit track and the limited block be arranged at outside described swivel becket, described limit track is arranged between described swivel becket and described cup, described limited block can embed in described limit track, enable described swivel becket described limit track and limited block coordinate spacing under, drive described Massage part along the circular motion outer wall of massage sleeve pipe done up and down reciprocatingly.
Preferably, described limit track comprises: the first spacing pipe box and the second spacing pipe box, described first spacing pipe box and the second spacing pipe box to be sheathed on outside described swivel becket and to be fixed on described cup inwall, and between the two relative end face, form the sine surface rail groove that can hold described limited block, the other end of described first spacing pipe box is connected with described upper bowl cover, and the other end of described second spacing pipe box is connected with described lower bowl cover.
Preferably, described first spacing pipe box and the second spacing pipe box are at least two respectively, form the first limit track at the first half of described cup and form the second limit track in the Lower Half of described cup respectively, described swivel becket is at least two, coordinates respectively with the first limit track and the second limit track.
Preferably, described Massage part is be arranged on the massage bead inside described swivel becket.
Preferably, described massage bead is connected with inside described swivel becket by elastomeric element, according to the deformation of described elastomeric element, regulates the distance between itself and described massage sleeve pipe.
Preferably, described cup is formed along its left cup axially split and the docking of right cup, and described upper bowl cover and/or lower bowl cover are that two parts docking radially split is formed, and match with the upper and lower two ends of described cup.
Preferably, the inwall of described massage sleeve pipe is provided with the guide recess of the flow direction guiding oil in described oil pump pipeline.
Compared with prior art, a kind of aircraft cup provided by the invention, by arranging oil pump in cup, so more convenient in use and improve massage comfort level; In addition, make Massage part realize, to comprehensive massage at massage position, reaching better massage effect, realizing automatic massage simultaneously according to projected path under the restriction of limit track by the limit track arranged, improve the comfort level of user.
Accompanying drawing explanation
In order to be illustrated more clearly in the embodiment of the present invention and technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment and description of the prior art below, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the structural representation of a kind of aircraft cup provided by the invention;
Fig. 2 is the structural profile schematic diagram of the left cup of a kind of aircraft cup provided by the invention;
Fig. 3 is the side view of Fig. 2;
Fig. 4 is the top view of Fig. 2;
Fig. 5 is the structural representation of the swivel becket of a kind of aircraft cup provided by the invention;
Fig. 6 be the swivel becket of a kind of aircraft cup provided by the invention A-A to sectional view;
Fig. 7 is the structural representation of spacing pipe box in the limit track of a kind of aircraft cup provided by the invention
Fig. 8 be a kind of aircraft cup provided by the invention limit track A-A to sectional view;
Fig. 9 is the top view of Fig. 7.
Figure number explanation
Cup 10, upper bowl cover 11, blind end 111, lower bowl cover 12, open end 121, upper fixed disk 13, lower fixed disk 14, fuel reserve tank 15, control button 16, protruding 17, massage mechanism 20, Massage part 21, massage bead 211, massage sleeve pipe 22, guide recess 221, retainer ring 222, oil pump 30, oil pump pipeline 31, drive mechanism 40, upper passive rotating disk 41, lower passive rotating disk 42, drivewheel 43, connecting rod 44, swivel becket 45, limited block 451, limit track 50, first spacing pipe box 51, second spacing pipe box 52, sine surface rail groove 53, draw-in groove 54, drive motors 60, circuit control panel 70, battery 80, bearing 90.
Detailed description of the invention
Below by engaging the accompanying drawing in the embodiment of the present invention, be clearly and completely described the technical scheme in the embodiment of the present invention, obviously, described embodiment is only the present invention's part embodiment, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.
Please refer to shown in Fig. 1, Fig. 1 is the structural representation of a kind of aircraft cup provided by the invention, and described aircraft cup comprises: cup 10, upper bowl cover 11, lower bowl cover 12, massage mechanism 20, oil pump 30, drive mechanism 40 and controller (not shown).Wherein, described upper bowl cover 11 and lower bowl cover 12 are arranged at described cup about 10 two ends respectively, and described upper bowl cover 11 is blind end 111, and described lower bowl cover 12 is for having the open end 121 of opening; Described massage mechanism 20 comprises: be arranged at the Massage part 21 in described cup 10 and have the massage sleeve pipe 22 holding Massage Department's bit space, described Massage part 21 is positioned at the outside of described massage sleeve pipe 22, and under the driving of described drive mechanism 40, outer wall along described massage sleeve pipe 22 moves, and exerts pressure to described massage sleeve pipe 22; Described oil pump 30 sets firmly and is placed in described cup 10, and is positioned at described upper bowl cover 11 region, is connected in described massage sleeve pipe 22 by oil pump pipeline 31.
Composition graphs 1, shown in figure 2-Fig. 4, Fig. 2 is the structural profile schematic diagram of the cup 10 of a kind of aircraft cup provided by the invention; Fig. 3 is the side view of Fig. 2; Fig. 4 is the top view of Fig. 2.In this enforcement, described cup 10 is formed along its left cup axially split and the docking of right cup, and described upper bowl cover 11 and/or lower bowl cover 12 are that two parts docking radially split is formed, and match with described cup about 10 two ends.
As shown in Figure 1, being arranged on described lower bowl cover 12 at oil pump 30 described in embodiment provided by the invention and being positioned at described cup 10, the oil pump pipeline 31 of described oil pump 30 is connected in described massage sleeve pipe 22, in massage sleeve pipe 22, provide lubricating oil.
Massage sleeve pipe 22 can be spread all over inner for ease of lubricating oil, reduce the frictional force between massage sleeve pipe 22 and massage position, the tube wall of described massage sleeve pipe 22 arranges multiple guide recess 221, and oil pump 30 pump evenly can be guided to each position of massage sleeve pipe 22 by described guide recess 221 to the lubricating oil in massage sleeve pipe 22.
For ease of reaching better massage effect, the shape of described massage sleeve pipe 22 can be set to and the more similar close structure of Massage Department's bit architecture.Described massage sleeve pipe can adopt the mode of living and connecting, and is arranged on described passive rotating disk 41 or on lower passive rotating disk 42, thus is convenient to massage the clean of sleeve pipe.In the present embodiment, described massage sleeve pipe is fixed on fixed disk 13 by the retainer ring 222 of massage sleeve pipe.
For enable oil pump 30 and driven unit firm be arranged in cup 10, aircraft cup provided by the invention comprises: go up fixed disk 13 and lower fixed disk 14 and bearing 90 and be arranged at described upper bowl cover 11 bottom and described lower bowl cover 12 top respectively, described oil pump 30 is arranged between described upper bowl cover 11 and fixed dish 13.According to foregoing, in enforcement of the present invention, preferably described oil pump 30 is arranged between described lower bowl cover 12 and lower fixed disk 14.
Fuel reserve tank 15 can be set between described lower bowl cover 12 and lower fixed disk 14 in the invention process, be connected with described oil pump 30, by oil pump 30, lubricating oil is exported in massage sleeve pipe 22, be understandable that, the position of described fuel reserve tank 15 is not limited to above-mentioned, if can meet oil pump 30 lubricating oil in fuel reserve tank 15 can be exported to massage sleeve pipe 22 in any position all can.
In this enforcement, described oil pump 30 can adopt mechanical type pressure mouth form, realizes the startup of oil pump 30 by triggering the control button 16 etc. that cup 10 outer surface is arranged, and then provides lubricating oil in massage sleeve pipe 22; Or adopt automatic control form, set by the fuel-displaced time of controlling organization to oil pump, during arrival Preset Time, oil pump realizes fuel-displaced automatically.
In this enforcement, driven unit and oil pump 30 etc. can realize by the circuit control panel 70 arranged in cup 10 controlling, and can arrange different control buttons 16 at cup 10 outer surface according to different controlling functions.Be understandable that, the circuit control panel 70 in the present invention can realize power supply by arranging battery 80 in cup 10, or can realize power supply by connecting external power source.
It should be noted that, massage sleeve pipe 22 in the present embodiment and can adopt silica gel material, to improve the comfort level at massage position.
The fuel-displaced mode of above-mentioned oil pump 30 and the control mode of driven unit, can adopt various ways, and such as: artificially manual etc., aforesaid way is only and realizes one citing that is fuel-displaced and that control, and mode that the present invention adopts is not limited to foregoing.
Composition graphs 1, shown in figure 5-Fig. 6, Fig. 5 is the structural representation of the swivel becket of a kind of aircraft cup provided by the invention; Fig. 6 be a kind of aircraft cup swivel becket provided by the invention A-A to sectional view.In the invention process, described drive mechanism 40 comprises: upper passive rotating disk 41, lower passive rotating disk 42, drivewheel 43, drive motors 60, connecting rod 44 and swivel becket 45.
Described swivel becket 45 is mobilizable to be connected on described connecting rod 44, the two ends of described connecting rod 44 connect described passive rotating disk 41 and lower passive rotating disk 42 respectively, described passive rotating disk is connected with described cup upper end, described lower passive rotating disk is connected with described cup bottom, in the present embodiment, described upper and lower passive rotating disk is fixed by ball bearing 90 and cup.Described swivel becket 45 is described between passive rotating disk 41 and lower passive rotating disk 42; Described drive motors drives described drivewheel 43 to rotate, described drivewheel 43 drives described passive rotating disk 41 to rotate, described passive rotating disk 41 drives described swivel becket 45 and described lower passive rotating disk 42 to rotate by described connecting rod 44, and described massage sleeve pipe 22 is positioned at described swivel becket 45 internal ring.
In this enforcement, the structure of gears meshing can be adopted to realize rotating between described drivewheel 43 and upper and lower follower, and when not changing motor acquiescence rotating speed, by regulating the size of drivewheel 43 diameter and upper and lower follower diameter, the adjustment to swivel becket speed can be realized.
Described Massage part 21 is arranged at inside institute's swivel becket 45 and towards the direction of described massage sleeve pipe 22 and extends, in swivel becket 45 passes on process, apply massage pressure to described massage sleeve pipe 22, and then reaches the massage effect to Massage part 21 in massage sleeve pipe 22.Described Massage part 21 can adopt the version of massage bead 211, the concrete one end that can adopt is connected to inside described swivel becket 45, the other end is provided with massage bead 211 connecting rod 44 and realizes being connected and fixed of massage bead 211 and swivel becket 45, massage bead 211 on described connecting rod 44 can be multiple, described connecting rod 44 also can be multiple, is distributed in the zones of different inside swivel becket 45.
For reaching better massage effect, at described massage bead 211, connecting rod 44 junction is provided with elastomeric element (not shown), or massage bead 211 is directly connected with inside described swivel becket 45 by described elastomeric element, massage bead 211 makes elastomeric element realize deformation adjustment according to the massage pressure received, thus makes the adjustment that the distance between massage sleeve pipe 22 and massage bead 211 can adapt to according to the massage position of massaging sleeve pipe 22 inside.
In conjunction with above-mentioned, please refer to shown in Fig. 7-9, Fig. 7 is the structural representation of a kind of aircraft cup limit track provided by the invention; Fig. 8 be a kind of aircraft cup provided by the invention limit track A-A to sectional view; Fig. 9 is the top view of Fig. 7.
The present invention makes massage bead 211 can massage according to the path implementation preset, also be provided with limit track 50 and be arranged at the limited block 451 outside described swivel becket 45 between described cup 10 and massage sleeve pipe 22, described limit track 50 is arranged between described swivel becket 45 and described cup 10, described limited block 451 can embed in described limit track 50, makes described swivel becket 45 can do circular motion up and down reciprocatingly at the described massage bead 211 of spacing lower drive that coordinates of described limit track 50 and limited block 451 on the outer wall of massaging sleeve pipe 22.
In this enforcement, described limit track 50 comprises: the first spacing pipe box 51 and the second spacing pipe box 52, described first spacing pipe box 51 and the second spacing pipe box 52 are sheathed on outside described swivel becket 45, and between the two relative end face, form the sine surface rail groove 53 that can hold described limited block 451, the other end of described first spacing pipe box 51 is connected with described upper bowl cover 11, and the other end of described second spacing pipe box 52 is connected with described lower bowl cover 12.
In this enforcement, a pair limit track 50 is set at the first half of described cup 10, that is: the first spacing pipe box 51 and the second spacing pipe box 52; In the Lower Half of described cup 10, a pair limit track 50 is being set, that is: the first spacing pipe box 51 and the second spacing pipe box 52, that is, in enforcement of the present invention, at least two group limit tracks 50 can be set, accordingly, described swivel becket 45 also at least arranges two, the first half being positioned at cup 10, a Lower Half being positioned at cup 10, subregionally respectively realizes massage to the massage position in described massage sleeve pipe 22.
In this enforcement, the outer wall of described first spacing pipe box 51 and the second spacing pipe box 52 arranges draw-in groove 54, described cup 10 inwall arranges protruding 17, by draw-in groove 54 and protruding 17 coordinate and realize fixing of the first spacing pipe box 51 and the second spacing pipe box 52 and cup 10.
It should be noted that, described draw-in groove 54 and protruding 17 positions arranged can exchange, and can fix as long as can meet the spacing pipe box 52 of the first spacing pipe box 51, second with described cup 10.
Above the structure of a kind of aircraft cup provided by the invention is described in detail, below in conjunction with said structure, the work process of aircraft cup provided by the invention has been described in detail.
Massage position is put into massage sleeve pipe 22 by the opening of upper bowl cover 11, by starting the startup button of cup 10 outside, driven unit is driven, drivewheel 43 with under the cooperatively interacting and drive of passive rotating disk 41, the sine surface rail groove 53 formed that swivel becket 45 is limited between the first limit casing and the second limit casing is interior mobile, thus realize massage bead 211 and can do circular motion reciprocal from top to bottom, to realize omnibearing massage to the massage position in massage sleeve pipe 22, closer to the effect of manual massage, and in massage processes, the distance that massage bead 211 can be adjusted massage bead 211 to its applied pressure by elastomeric element and be massaged between position (or massaging sleeve pipe 22) according to massage position, reach better massage effect, meanwhile, in massage processes, user can according to the comfort level of oneself massage, oil pump 30 is started by the button that cup 10 is arranged, and then lubricating oil is imported in massage sleeve pipe 22, the further comfort level improving massage.
The foregoing is only the preferred implementation of a kind of massage machine provided by the invention, do not form limiting the scope of the present invention.Number of components in this embodiment is not limited to the mode adopted in embodiment, and any any amendment done within the spirit and principles in the present invention, equivalent replacement and improvement etc., all should be included within claims of the present invention.
Claims (10)
1. an aircraft cup, is characterized in that, comprising: cup, upper bowl cover, lower bowl cover, massage mechanism, oil pump, drive mechanism and controller;
Wherein, described upper bowl cover and lower bowl cover are arranged at the upper and lower two ends of described cup respectively, and described upper bowl cover is blind end, and described lower bowl cover is the open end with port;
Described massage mechanism comprises: be arranged at the Massage part in described cup and have the massage sleeve pipe holding Massage Department's bit space, and described massage sleeve pipe adopts the mode connected of living to be connected with cup; Described Massage part is positioned at the outside of described massage sleeve pipe, and under the driving of described drive mechanism, can move, exert pressure to described massage sleeve pipe along the outer wall of described massage sleeve pipe;
Described oil pump sets firmly and is placed in described cup, and is positioned at the region of described upper bowl cover or lower bowl cover, is connected in described massage sleeve pipe by oil pump pipeline.
2. aircraft cup according to claim 1, is characterized in that, comprising: upper fixed disk and lower fixed disk, be arranged at described upper bowl cover bottom and described lower bowl cover top respectively, described oil pump is arranged between described upper bowl cover and fixed dish.
3. aircraft cup according to claim 1 and 2, is characterized in that, described drive mechanism comprises: upper passive rotating disk, lower passive rotating disk, drivewheel, drive motors, connecting rod and swivel becket;
Described swivel becket is mobilizable to be connected on described connecting rod, and the two ends of described connecting rod connect described passive rotating disk and lower passive rotating disk respectively, and described passive rotating disk is connected with described cup upper end, and described lower passive rotating disk is connected with described cup bottom; Described swivel becket is described between passive rotating disk and lower passive rotating disk; Described drive motors drives described drivewheel to rotate, and described drivewheel drives described passive dial rotation, and described passive rotating disk drives described swivel becket and described lower passive dial rotation by described connecting rod.
4. aircraft cup according to claim 3, it is characterized in that, comprise: limit track and the limited block be arranged at outside described swivel becket, described limit track is arranged between described swivel becket and described cup, described limited block can embed in described limit track, enable described swivel becket described limit track and limited block coordinate spacing under, drive described Massage part along the circular motion outer wall of massage sleeve pipe done up and down reciprocatingly.
5. aircraft cup according to claim 4, it is characterized in that, described limit track comprises: the first spacing pipe box and the second spacing pipe box, described first spacing pipe box and the second spacing pipe box to be sheathed on outside described swivel becket and to be fixed on described cup inwall, and between the two relative end face, form the sine surface rail groove that can hold described limited block, the other end of described first spacing pipe box is connected with described upper bowl cover, and the other end of described second spacing pipe box is connected with described lower bowl cover.
6. aircraft cup according to claim 5, it is characterized in that, described first spacing pipe box and the second spacing pipe box are at least two respectively, form the first limit track at the first half of described cup and form the second limit track in the Lower Half of described cup respectively, described swivel becket is at least two, coordinates respectively with the first limit track and the second limit track.
7. aircraft cup according to claim 3, is characterized in that: described Massage part is be arranged on the massage bead inside described swivel becket.
8. aircraft cup according to claim 7, is characterized in that, described massage bead is connected with inside described swivel becket by elastomeric element, according to the deformation of described elastomeric element, regulates the distance between itself and described massage sleeve pipe.
9. aircraft cup according to claim 1, it is characterized in that, described cup is formed along its left cup axially split and the docking of right cup, and described upper bowl cover and/or lower bowl cover are that two parts docking radially split is formed, and match with the upper and lower two ends of described cup.
10. aircraft cup according to claim 1, is characterized in that: the guide recess being provided with the flow direction guiding oil in described oil pump pipeline on the inwall of described massage sleeve pipe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510829371.5A CN105287183B (en) | 2015-11-25 | 2015-11-25 | A kind of aircraft cup |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510829371.5A CN105287183B (en) | 2015-11-25 | 2015-11-25 | A kind of aircraft cup |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105287183A true CN105287183A (en) | 2016-02-03 |
| CN105287183B CN105287183B (en) | 2017-12-15 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510829371.5A Active CN105287183B (en) | 2015-11-25 | 2015-11-25 | A kind of aircraft cup |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105287183B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109661219A (en) * | 2016-08-05 | 2019-04-19 | 株式会社典雅 | Ejaculation stimulating device |
| WO2022147822A1 (en) * | 2021-01-11 | 2022-07-14 | 温州琦莎玩具有限公司 | Vibration apparatus and massage device comprising vibration apparatus |
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| CN203954139U (en) * | 2014-06-03 | 2014-11-26 | 深圳市同立创科技有限公司 | A kind of health care facility |
| CN204723371U (en) * | 2015-06-23 | 2015-10-28 | 程香英 | Flexible massaging device |
| CN205885783U (en) * | 2015-11-25 | 2017-01-18 | 刘万坤 | Aircraft cup |
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| CN109661219A (en) * | 2016-08-05 | 2019-04-19 | 株式会社典雅 | Ejaculation stimulating device |
| CN109661219B (en) * | 2016-08-05 | 2021-04-27 | 株式会社典雅 | Ejaculation stimulating device |
| WO2022147822A1 (en) * | 2021-01-11 | 2022-07-14 | 温州琦莎玩具有限公司 | Vibration apparatus and massage device comprising vibration apparatus |
| US12090109B2 (en) | 2021-01-11 | 2024-09-17 | Wenzhou Chisa Toys Co., Ltd. | Vibration apparatus and massage device comprising vibration apparatus |
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