Aircraft cup with opening structure

Abstract

Aircraft cup with an opening structure, characterized in that it comprises: - a soft main body, wherein the soft main body is elongated, with two arcuate flexible side wings extending towards each other on both sides of the soft main body, - wherein the two flexible side wings are the first side wing and the second side wing respectively, and the soft main body, the inner wall of the first side wing and the inner wall of the second side wing form a massage channel; the first side wing comprises a first end wall, the second side wing comprises a second end wall corresponding to the first end wall; - a deformation position enclosed between the first end wall and the second end wall, wherein the first side wing can deform the first end wall and the second side wing can deform the second end wall to change the relative position of the first end wall and the second end wall; - a first stimulation source located in the cavity of the soft main body, wherein the first stimulation source can provide a predetermined physical stimulation at at least one position of the soft main body, the first lateral wing and the second lateral wing.

Description

Technical area

[0001] The present invention relates to the field of sex toys, in particular to an airplane cup with an opening structure. State of the art

[0002] The existing airplane cup is primarily used to stimulate the male genitals by creating pleasurable sensations through the application of predetermined stimulation to sensitive points. The structure of the existing airplane cup generally consists of a cavity with a channel, one end of which has an opening into which the male genitals can be inserted.

[0003] Therefore, the corresponding structure restricts their internal dimensions, thus limiting the applicable penis size. Of course, there are also some cavities with elastic structures that are suitable for a specific range of penis sizes, but their adaptability is correspondingly lower. At the same time, airplane cups with hollow structures generally have the problem of being large in volume and the storage box is not easy to carry. Contents of this utility model

[0004] The objective of this invention is to propose an aircraft cup with an opening structure, which aims to improve the existing aircraft cup structure. The opening structure allows it to accommodate a wider range of penis sizes, while maintaining a small volume, providing a predetermined clamping force, improving the degree of adaptability, effectively increasing the stimulation of sensitive points, and thus enhancing market competitiveness.

[0005] To achieve the above object, the present invention proposes an aircraft cup having an opening structure comprising: - a soft main body, the soft main body being elongated in shape, with two curved flexible side wings extending towards each other on the two sides of the soft main body, - wherein the two flexible side wings are the first side wing and the second side wing, respectively, and the soft main body, the inner wall of the first side wing and the inner wall of the second side wing form a massage channel; the first side wing comprises a first end wall, the second side wing comprises a second end wall corresponding to the first end wall. The first side wing comprises the first end wall, the second side wing comprises the second end wall corresponding to the first end wall; - a deformation position enclosed between the first end wall and the second end wall, wherein the first side wing can deform the first end wall and the second side wing can deform the second end wall to change the relative position of the first end wall and the second end wall; - a first stimulation source arranged in the cavity of the soft main body, wherein the first stimulation source can provide a predetermined physical stimulation at at least one position of the soft main body, the first side wing and the second side wing.

[0006] In the actual design, by changing the shape of the aircraft cup, the conventional sleeve structure is converted into a tubular structure, with the first side wing and the second side wing on the two sides of the soft main body being flexible, which allows the first end wall and the second end wall to approach or move away from each other, ensuring that it is suitable for a wider range of male genital sizes.

[0007] During use, when the male genital organ is inserted into the massage channel, the width of the deformation position expands, bringing the inner wall of the massage channel into contact with the outer wall of the male genital organ. This can provide a larger contact area for the penis, which in turn provides a larger friction surface and increases the stimulation effect.

[0008] At the same time, various first stimulation sources can be installed in the soft main body to increase the stimulation effect of the aircraft cup, such as mechanical stimulation, electrical stimulation and heat stimulation. Brief description of the characters Fig. 1 is a schematic diagram of the first embodiment of the first embodiment of the present invention; Fig. 2 is a schematic diagram of the second embodiment of the first embodiment of the present invention; Fig. 3 is a schematic diagram of the third embodiment of the first embodiment of the present invention; Fig. 4 is a schematic diagram of the first embodiment of the second embodiment of the present invention; Fig. 5 is a schematic diagram of the second embodiment of the second second embodiment of the present invention; Fig. 6 is a schematic diagram of the first embodiment of the third embodiment of the present invention; Fig. 7 is a schematic diagram of the second embodiment of the third embodiment of the present invention; Fig. 8 is a schematic diagram of the first embodiment of the fourth embodiment of the present invention; Fig. 9 is a schematic diagram of the second embodiment of the fourth embodiment of the present invention; Fig. 10 is a schematic diagram when the first stimulation source is a tapping device; Fig. Figure 11 is a schematic representation when the first stimulation source is a tongue. Detailed embodiments

[0009] In the following, the technical solutions of the embodiments of the present invention are described clearly and completely in conjunction with the figures. Obviously, the described embodiments are only a part of the embodiments of the present invention and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by general technicians in this field without creative work are within the scope of the present invention.

[0010] It should be noted that when directional terms (such as up, down, left, right, front, back, upper, lower, inward, outward, vertical, horizontal, longitudinal, counterclockwise, clockwise, circumferential, radial, axial, etc.) are included in the embodiments of the present invention, these directional terms are used only to explain the relative positional relationships and movements of the individual components in a specific posture (as shown in the figures). If this specific posture changes, the directional terms will also change accordingly.

[0011] Furthermore, when descriptions such as "first" or "second," etc. are included in the embodiments of the present invention, these descriptions are for descriptive purposes only and should not be understood as indicating or suggesting their relative importance or as implicitly indicating the number of technical features specified. Therefore, a feature referred to as "first" or "second" may explicitly or implicitly include at least one of these features. Furthermore, the technical solutions of the various embodiments may be combined with each other, but this must be done on the basis that a general technician in this field can implement it. If the combination of the technical solutions leads to contradictions or impossibility, it should be assumed that such a combination of technical solutions does not exist and does not fall within the scope of this invention.

[0012] As in the Fig. 1 to 11, an aircraft cup having an opening structure comprises: - a soft main body 1, wherein the soft main body 1 is elongated, a cavity 13 is formed inside the soft main body, and two curved flexible side wings extend towards each other on the two sides of the soft main body 1, - wherein the two flexible side wings are the first side wing 11 and the second side wing 12, respectively, and the soft main body 1, the inner wall of the first side wing 11 and the inner wall of the second side wing 12 form a massage channel 5; - a deformation position 3: the deformation position 3 is located between the first end wall 21 of the first side wing 11 and the second end wall 22 of the second side wing 12. The two flexible side wings can change the relative position of the first end wall 21 and the second end wall 22, ie the first side wing 11 can deform the first end wall 21 and the second side wing 12 can deform the second end wall 22, so that the first end wall 21 and the second end wall 22 can approach each other or move away from each other; - the first stimulation source, the first stimulation source is arranged in the cavity 13 of the soft main body 1, the first stimulation source can provide a predetermined physical stimulation at at least one position of the soft main body 1, the first side wing 11 and the second side wing 12.

[0013] In the actual design, by changing the shape of the aircraft cup, the conventional sleeve structure is converted into a tubular structure. The flexible first side wings 11 and second side wings 12 on both sides of the soft main body 1 allow the first end wall 21 and the second end wall 22 to deform toward or away from each other, ensuring that they are suitable for male genitalia of various sizes.

[0014] During use, when the male genital organ is inserted into the massage channel 5, the width of the deformation position 3 expands, bringing the inner wall of the massage channel 5 into contact with the outer wall of the male genital organ. This can provide a larger contact area for the penis, resulting in a larger friction surface and increasing the stimulation effect.

[0015] At the same time, various first stimulation sources can be installed in the soft main body 1 to enhance the stimulation effect of the aircraft cup, such as mechanical stimulation, electrical stimulation and heat stimulation.

[0016] In the first embodiment, both ends of the massage channel 5 are continuous, wherein the deformation position 3 is S-shaped.

[0017] In the second embodiment, both ends of the massage channel 5 are formed continuously, and the soft main body 1 is provided with an annular object, wherein the deformation position 3 has a curved shape.

[0018] In the third embodiment, one end of the massage channel 5 is provided with a blocking seat 100, and the blocking seat 100 is equipped with a tongue 101 extending in the direction of the massage channel 5.

[0019] In the fourth embodiment, one end of the massage channel 5 is provided with a locking seat 100, and the locking seat 100 extends integrally with a handle portion, while the locking seat 100 also has a swinging tongue 101.

[0020] In particular, the upper wall 5a (which of course can also be the lower wall) of the soft main body 1, the inner wall 5b of the first side wing 11 and the inner wall 5c of the second side wing 12 form the massage channel 5.

[0021] Specifically, deformation position 3 has an arcuate, curved, S-shaped, straight, oblique, or open shape. Depending on the shape, it can exert different elastic constraints on the penis while simultaneously providing different friction surfaces and friction stimuli, thus enhancing the user experience.

[0022] In particular, the shape of the first end wall 21 and the shape of the second end wall 22 are symmetrical.

[0023] In particular, when the deformation position 3 has an open or straight shape, the shape of the first end wall 21 and the shape of the second end wall 22 are formed symmetrically, which makes the shape and design of the aircraft cup more symmetrical, the lines smoother and more beautiful, and the overall design is improved.

[0024] In particular, when the shape of the first end wall 21 and the shape of the second end wall 22 are irregular, the shapes of the first end wall 21 and the second end wall 22 are formed in an offset symmetrical manner, for example, in a curved shape or an S-shape; As a result, the deformation position 3 has different restricting forces and thus offers different degrees of adaptation for different experiences; In the offset symmetry, the symmetry line can be curved, S-shaped, longitudinal or transverse.

[0025] In particular, a first side portion 41 extends from the lower part of the side wall of the first end wall 21 toward the second end wall 22, and a second side portion 42 extends from the upper part of the side wall of the second end wall 22 toward the first end wall 21, whereby the deformation position 3 assumes a curved structure.

[0026] In particular, the massage channel 5 is provided with massage lines 50, wherein the massage lines 50 are arranged on the wall of the soft main body 1 and / or on the inner side wall of the flexible side wings; the massage lines 50 are designed as protruding or groove-like structures.

[0027] In particular, the 50 massage lines are designed as ridges, bumps, nubs, or humps, which can provide different stimulation sensations depending on their shape, thereby increasing the contact area. This can provide a realistic vagina or a simulated tactile sensation, thus enhancing the product experience.

[0028] In particular, the massage lines 50 are designed as strip-shaped grooves, dot-shaped grooves or block-shaped grooves, which can provide a realistic vagina or a simulated tactile feeling and thus enhance the product experience.

[0029] The massage lines 50 are arranged in a spiral or pattern, for example in the form of a collar as in Fig. 6.

[0030] The deformation position 3 is the distance between the first end wall 21 and the second end wall 22 or the groove formed by the contact between the first end wall 21 and the second end wall 22.

[0031] Specifically, the physical stimulation of the first stimulation source includes mechanical stimulation, electrical stimulation, and thermal stimulation. Mechanical stimulation includes at least one of the following: vibration, oscillation, torsion, tapping, telescopic, and suction. The actual design can be customized to meet actual needs.

[0032] Specifically, the first stimulation source includes a hard shell 6 disposed within the soft main body 1, and a first drive device disposed inside the hard shell 6. Also disposed within the hard shell 6 are a PCB 62 and a lithium battery 61 connected to the PCB 62. The vibration motor 7 is connected to the PCB, and the soft main body 1 encloses the hard shell 6.

[0033] The front wall, the rear wall, or the back of the hard shell 6, which is remote from the massage channel 5, is equipped with a control button 63. The control button 63 is used to turn the first stimulation source on or off. When switched on, parameters such as the vibration frequency of the vibration motor 7 can also be controlled.

[0034] The control button 63 is preferably located on the back of the hard shell 6, which allows for easy operation. Pressing the control button exerts pressure on the soft main body 1, allowing the control button inside the hard shell 6 to be actuated.

[0035] Specifically, the first driving device is a vibration motor 7. When the vibration motor 7 is turned on, it moves the soft main body 1 at a predetermined frequency, thereby causing the massage lines 50 to come into frictional contact with the penis and improving the usage experience.

[0036] In particular, the first drive device is a tapping device 8. The tapping device 8 includes a guide slot 84 arranged in the hard shell 6, and a diaphragm 85 that slides vertically in the guide slot 84. The eccentric bearing 82 projects into the side wall of the lower diaphragm 85 of the tapping seat 83 and bears against the soft main body 1.

[0037] The knocking device 8 also includes the first rotary motor 81, the eccentric bearing 82 attached to the drive of the first rotary motor 81 and the vertically extending knocking seat 83, the upper end of which is connected to the diaphragm 85.

[0038] By fitting the soft main body 1 to the diaphragm 85 and establishing the guide slot 84, the rotation stroke is converted into a vertical stroke, so that the diaphragm 85 can repeatedly tap the wall surface of the soft main body 1 to achieve the tap effect.

[0039] In particular, both ends of the massage channel 5 are formed continuously. Therefore, the overall volume is small, and during use, any portion can be inserted into the massage channel 5 according to actual needs.

[0040] During use, the palm of the hand can come into contact with the back wall of the soft main body 1, and the thumb and other fingers can grip the first side wing 11 and the second side wing 12 respectively to control the aircraft cup forward or in other directions, thus providing the desired stimulation.

[0041] Specifically, the soft main body 1, the first side panel 11, and the second side panel 12 are injection-molded in one piece, using silicone. The preferred material is silicone, which is injection-molded in one piece. Silicone provides a good tactile feel, and one-piece injection molding can provide a good grip while ensuring the waterproofness of the electronic components and facilitating cleaning.

[0042] Specifically, the soft main body 1 extends over an elastic cord 9, and the end of the elastic cord 9, which is remote from the soft main body 1, is provided with a ring-shaped object. The ring-shaped object is an ejaculation ring, which serves to exert a predetermined restrictive force on the testicles or the base of the penis. This can prolong the erection time and the ejaculation time of the penis while simultaneously achieving a stimulating effect, thus enhancing the user experience and simultaneously providing a training effect.

[0043] Specifically, the ejaculation ring includes a first collar 91 connected to the elastic cord 9, and a second collar 92 connected to the first collar 91 via a connecting cable 93. The first collar 91 serves to insert the penis, while the second collar 92 serves to insert the testicles. This results in a double ejaculation delay effect that prolongs the duration of penile erection and delays the ejaculation time.

[0044] In particular, a blocking seat 100 extends from one end of the soft main body 1, which can block the massage channel 5. The blocking seat 100 is equipped with a second stimulation source comprising a second drive device and a tongue 101 swingably mounted on the wall of the blocking seat 100.

[0045] The tongue 101 extends from the locking seat 100 toward the massage channel 5, and the second drive device serves to swing the tongue 101 back and forth. The arrangement of the second stimulation source and the tongue 101 allows the penis head to be stimulated, mimicking the tongue movement and enhancing the overall experience of the airplane cup.

[0046] Of course, in actual use, lubricant can be applied to the main body and tongue 101 to enhance the effect.

[0047] Specifically, the second drive device includes a second rotary motor 200 and an eccentric cam 201 connected to the second rotary motor 200 (the structure may refer to the eccentric bearing 82). The middle part of the tongue 101 is rotatably mounted through the first pivot point 102, the rear part of the tongue 101 is equipped with a drive unit 202, the drive unit 202 is provided with an elongated slot 203, the eccentric cam 201 is equipped with an eccentric part 204 projecting into the elongated slot 203, and the tongue 101 is covered with an elastic layer 103, thereby converting the rotational path of the second rotary motor 200 into a rectangular path, enabling the reciprocating movement of the tongue 101.

[0048] In particular, the soft main body 1 is located on one side of the blocking seat 100 and extends horizontally with a handle portion 300, the handle portion 300 being used for holding by the hand.

[0049] In particular, the handle portion 300 is provided with a through-hole 301 extending through the side wall of the handle portion 300. The arrangement of the handle portion 300 allows the aircraft cup to be held comfortably, improving the user experience.

[0050] The above is only a preferred embodiment of the present invention and does not limit the scope of the present invention. All equivalent structural changes made within the spirit of the present invention or direct / indirect application in other related technical fields are included within the scope of the present invention. List of reference symbols 1. Soft main body, 11. First lateral wing, 12. Second lateral wing, 13. Cavity, 21. First end wall, 22. Second end wall, 3. Deformation position, 41. First page section, 42. Second page section, 5. Massage channel, 50. Massage lines, 5a. Upper wall of the soft main body, 5b. Inner wall of the first lateral wing, 5c. Inner wall of the second lateral wing, 6. Hard shell, 61. Lithium battery, 62. PCB board, 63. Control button, 7. Vibration motor, 8. Knocking device, 8. First rotary motor, 82. Eccentric bearing, 83. Knocking seat, 84. Guide slot, 85. Diaphragm, 9. Elastic rope, 91. First collar, 92. Second collar, 93. Connecting rope, 100. Locking seat, 101. Tongue, 102. First pivot point, 103. Elastic layer, 200. Second rotary motor, 201. Eccentric cam, 202. Drive part, 203. Elongated slot, 204. Eccentric part, 300. Handle section, 301. Through hole.

Claims

[1] Aircraft cup with an opening structure, characterized by that it includes: - a soft main body, the soft main body being elongated in shape, with two curved flexible side wings extending towards each other on the two sides of the soft main body, - wherein the two flexible side wings are the first side wing and the second side wing, respectively, and the soft main body, the inner wall of the first side wing, and the inner wall of the second side wing form a massage channel; the first side wing comprises a first end wall, the second side wing comprises a second end wall corresponding to the first end wall; - a deformation position enclosed between the first end wall and the second end wall, wherein the first side wing can deform the first end wall and the second side wing can deform the second end wall to change the relative position of the first end wall and the second end wall; - a first stimulation source arranged in the cavity of the soft main body, wherein the first stimulation source can provide a predetermined physical stimulation at at least one position of the soft main body, the first side wing and the second side wing. [2] An aircraft cup having an opening structure according to claim 1, characterized by that the deformation position has an arc shape, a curved shape, an S-shape, a linear shape, a diagonal shape or an opening shape. [3] An aircraft cup having an opening structure according to claim 1, characterized bythat the shape of the first end wall and the shape of the second end wall are symmetrical. [4] An aircraft cup having an opening structure according to claim 1, characterized by that the shape of the first end wall and the shape of the second end wall are offset symmetrically formed when the shape of the first end wall and the shape of the second end wall are irregular. [5] Aircraft cup with opening structure according to claim 4, characterized by that a first side section extends from the lower part of the side wall of the first end wall towards the second end wall, and a second side section extends from the upper part of the side wall of the second end wall towards the first end wall. [6] Aircraft cup with opening structure according to claim 1, characterized bythat the massage channel is provided with massage lines, wherein the massage lines are arranged on the wall of the soft main body and / or on the inner side wall of the flexible side wings; wherein the massage lines are designed as protruding or groove-like structures. [7] Aircraft cup with opening structure according to claim 6, characterized by that the massage lines include ribs, elevations, knobs or bumps. [8] Aircraft cup with opening structure according to claim 6, characterized by that the deformation position is the distance between the first end wall and the second end wall or the groove formed by the contact between the first end wall and the second end wall. [9] Aircraft cup with opening structure according to claim 1, characterized bythat the physical stimulation of the first stimulation source comprises mechanical stimulation, electrical stimulation and thermal stimulation; wherein the mechanical stimulation comprises at least one of the following: vibration, oscillation, torsion, tapping, telescoping and suction. [10] Aircraft cup with opening structure according to claim 1, characterized by that the first stimulation source comprises a hard shell arranged in the soft main body and a first drive device arranged inside the hard shell, wherein a PCB board and a lithium battery connected to the PCB board are also arranged in the hard shell, - the soft main body envelops the hard shell; - the front wall, the rear wall or the back of the hard shell remote from the massage channel is provided with a control button for switching the first stimulation source on or off. [11] Aircraft cup with opening structure according to claim 10, characterized by that the first drive device is a vibration motor connected to the PCB. [12] Aircraft cup with opening structure according to claim 10, characterized by that the first drive device is a knocking device, the knocking device comprising a guide slot arranged in the hard shell and a membrane slidably mounted vertically in the guide slot, the membrane resting against the soft main body, - wherein the knocking device further comprises a first rotary motor, an eccentric bearing arranged at the drive end of the first rotary motor and a vertically extending knocking seat, wherein the eccentric bearing projects into the side wall of the lower part of the knocking seat and the upper end of the knocking seat is connected to the diaphragm. [13] Aircraft cup with opening structure according to claim 1, characterized by that the two ends of the massage channel are continuous. [14] Aircraft cup with opening structure according to claim 1, characterized by that the soft main body, the first side wing and the second side wing are integrally molded by injection molding, the injection molding material being silicone. [15] Aircraft cup with opening structure according to claim 1, characterized by that the soft main body extends an elastic rope, wherein an end of the elastic rope remote from the soft main body is provided with a ring-shaped object, wherein the ring-shaped object is an ejaculation ring which serves to exert a predetermined binding force on the testicles or the base of the penis. [16] Aircraft cup with opening structure according to claim 15, characterized bythat two ejaculation rings are provided, wherein the ejaculation ring comprises a first collar and a second collar, wherein the first collar is connected to the elastic rope, and the second collar is connected to the first collar by a connecting rope, wherein the first collar serves for inserting the penis, while the second collar serves for inserting the testicles. [17] Aircraft cup with opening structure according to claim 1, characterized by in that one end of the soft main body has a blocking seat which can block the massage channel, the blocking seat is equipped with a second stimulation source which comprises a second driving device and a tongue which is swingably mounted on the wall of the blocking seat, the tongue extending from the blocking seat towards the massage channel, the second driving device serving to swing the tongue back and forth. [18] Aircraft cup with opening structure according to claim 17, characterized by that the second drive device comprises a second rotary motor and an eccentric cam connected to the second rotary motor, wherein the middle part of the tongue is pivotally arranged about a first pivot point, the rear part of the tongue is provided with a drive part, the drive part has an elongated slot, the eccentric cam has an eccentric part projecting into the elongated slot and the tongue is covered with an elastic layer. [19] Aircraft cup with opening structure according to claim 18, characterized by that a handle portion extends horizontally from the side of the soft main body located at the blocking seat. [20] Aircraft cup with opening structure according to claim 19, characterized by that the handle portion is provided with a through hole penetrating the side wall of the handle portion.

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