Aircraft cup with holder structure

Abstract

Aircraft cup with mounting structure, characterized in that it includes: - a main body comprising a hard shell provided with an interior and a flexible wall arranged in the interior, the flexible wall having a channel for the penetration of male genitalia; - a bracket, wherein the bracket is attached to the wall surface of the hard shell and is designed to clamp the playback device.

Description

Technical area

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

[0002] The airplane cup is one of the portable male masturbation devices. In modern society, where pressure is high, the airplane cup can help relieve male desire.

[0003] When men use the airplane cup, they often watch movies to achieve the intended visual experience and stimulate the male genitals. Current practice is usually to use a special stand or table when using the airplane cup. If the screen is small, this can lead to a decrease in the visual experience and impair the user experience. Contents of the present invention

[0004] The main objective of this invention is to propose an airplane cup with a support structure, combining the support structure with the airplane cup. This allows men to watch movies directly while using the airplane cup, resulting in a dual enjoyment of visual and sexual stimulation and enhancing the user experience.

[0005] To achieve the above object, the present invention proposes an aircraft cup with support structure comprising: a main body, the main body comprising a hard shell provided with an interior space and a flexible wall arranged in the interior space, the flexible wall having a channel for the penetration of male genitalia; a holder, wherein the holder is attached to the wall surface of the hard shell and is designed to clamp the playback device. In the actual design, by arranging the hard shell and the flexible wall, with the hard shell serving as a support structure and for hand holding, the flexible wall is provided with a channel into which the male genitals can be inserted, and by directly attaching the bracket to the hard shell, the player can directly play audio and video, thereby achieving dual stimulation of visual stimuli and genitals, which improves the user experience; At the same time, the combination of hard shell and holder increases the grip surface of the aircraft cup, which improves the grip feel of the aircraft cup.

[0006] The hard shell can also be equipped with a drive device, such as a telescopic structure or a vibration structure, in order to exert a predetermined stimulus source on the flexible wall in the interior. Brief description of the characters Fig. 1 is a schematic diagram of the first embodiment of the present invention; Fig. 2 is a schematic diagram of the second embodiment of the present invention; Fig. 3 is a perspective schematic view of the first embodiment of the present invention; Fig. 4 is a schematic diagram of the second embodiment of the present invention; Fig. 5 is a schematic diagram of the third embodiment of the present invention; Fig. 6 is a schematic diagram of the fourth embodiment of the present invention; Fig. 7 is a schematic diagram of the fifth embodiment of the present invention; Fig. Fig. 8 is a schematic diagram of the sixth embodiment of the present invention; Fig. 9 is a schematic diagram of the seventh embodiment of the present invention. Detailed embodiments

[0007] In the following, the technical solution in the embodiments of the present invention will be described clearly and completely in conjunction with the accompanying drawings. Obviously, the described embodiments represent only a portion of the embodiments of the present invention and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of the present invention.

[0008] It should be noted that when directional terms (such as up, down, left, right, front, back, 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 movement states of the individual components in a specific posture (as shown in the drawings). If this specific posture changes, the directional terms will also change accordingly.

[0009] Furthermore, when descriptions such as "first" or "second," etc., appear in the embodiments of this 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 marked "first" or "second" may explicitly or implicitly include at least one of these features. Furthermore, the technical solutions of the individual embodiments may be combined with each other, but this must be done on the basis that a person skilled in the art can implement them. If the combination of technical solutions leads to contradictions or is not feasible, it should be assumed that such a combination of technical solutions does not exist and is also not within the scope of this invention.

[0010] As in the Fig. 1 to 9, an aircraft cup with support structure comprises: Main body 1, wherein the main body 1 comprises a hard shell 11 provided with an interior space 11a and a flexible wall 12 arranged in the interior space 11a, wherein the flexible wall 12 has a channel 12a for the penetration of the male genitals; a holder 2, wherein the holder 2 is attached to the wall surface of the hard shell 11, wherein the holder 2 is designed to clamp the playback device. In the actual design, by arranging the hard shell 11 and the flexible wall 12, wherein the hard shell 11 is designed as a support structure and for handholding, and the flexible wall 12 has a channel 12a for the penetration of the male genitals, the holder 2 is directly attached to the hard shell 11, whereby the player 100 can directly play audio and video, resulting in dual stimulation of visual and genital stimuli and thus improving the user experience; At the same time, the combination of hard shell 11 and holder 2 also enlarges the gripping surface of the aircraft cup, which in turn improves the gripping feel of the aircraft cup.

[0011] The hard shell 11 can also be equipped with a drive device, such as a telescopic structure or a vibration structure, in order to supply a predetermined stimulus source to the flexible wall 12 in the interior space 11a.

[0012] In particular, the holder 2 comprises a base 21 attached to the hard shell 11, as well as a clamp holder 3 attached to the base 21 and configured for playing audio and video. The hard shell 11 supports the base 21. The outer wall of the hard shell 11 can be coated with an elastic layer to improve the feel of the aircraft cup while also providing a water-repellent function.

[0013] Specifically, the clamp holder 3 is a magnetic seat 33 comprising a plate, the plate being provided with magnets distributed around its perimeter. The arrangement of the magnetic seat 33 allows the existing structure of magnetic mobile phones, magnetic tablets, etc. to be easily adsorbed and fixed. The structure is simple, yet the stability is also quite good. The player can be rotated or the angle adjusted according to actual needs.

[0014] In particular, the base 21 and the magnetic seat 33 are integrally formed or detachably arranged to meet different requirements.

[0015] In particular, the clamp holder 3 comprises a positioning section 31 arranged on the base 21 and an adjustment section 32 slidably mounted on the positioning section 31. The positioning section 31 and the adjustment section 32 are each provided with a first clamping section 31a and a second clamping section 32a arranged opposite one another. The first clamping section 31a and the second clamping section 32a form a clamping distance. The adjustable clamping section is designed for positioning the playback device, wherein a spring can be arranged between the positioning section 31 and the adjustment section 32 to realize the relative movement of the adjustment section 32.

[0016] In particular, the base 21 and the positioning portion 31 are integrally molded, therefore, their structural stability is relatively good, no fixing is required, and the corresponding base 21 and the positioning portion 31 have a fixed angle.

[0017] In particular, the base 21 and the positioning section 31 can be arranged detachably, wherein the corresponding base 21 and the positioning section 31 can have a fixed structure, such as a threaded connection, or the angle between the base 21 and the positioning section 31 can be adjustable by the existing universal joint 5.

[0018] In particular, the base 21 and the positioning section 31 are, for example, in Fig. 9 is fixed by the cardan joint 5.

[0019] In particular, the base 21 can be removably mounted on the hard shell 11.

[0020] In particular, the base 21 is, for example, in Fig. 8 a clamp 35, the clamp 35 is designed to be detachable, the clamp 35 forms a clamp chamber corresponding to the size of the hard shell 11 and is fixed to the outer wall of the hard shell 11 to realize a detachable structure.

[0021] In particular, the clamp 35 comprises a mounting ring 35a and a retaining ring 35b removably mounted on the mounting ring. One end of the mounting ring is pivotally connected to the retaining ring, and the other end is provided with a closure. The wall surface of the mounting ring is provided with a base 21.

[0022] In particular, as in Fig. 3 and Fig. As shown in Figure 4, the hard shell 11 is provided with a positioning hole 41, and the base 21 is provided with a positioning pin 42 that fits the positioning hole 41. Of course, in detail, a rubber plug may be installed in the positioning hole to close it when disassembling the base 21 and to improve aesthetics.

[0023] Specifically, the positioning hole is provided with an internal thread, the positioning pin is provided with an external thread matching the internal thread, and the base 21 can be directly fixed by the external thread and the internal thread.

[0024] In particular, the base 21 is firmly connected to the hard shell 11, for example, the magnetic seat 33 can be mounted directly on the base 21 or installed detachably.

[0025] In particular, the base 21 is firmly riveted to the hard shell 11, integrally molded by injection molding, fixed by snap connection, or bonded with adhesive, which can reduce the damage between the base 21 and the hard shell 11 and increase the service life.

[0026] In particular, as in Fig. As shown in Figure 6, clamping plates 36 are provided on both sides of the hard shell 11, which are relatively movable. The hard shell 11 is provided with guide sliding grooves, the clamping plates 36 are slidably installed in the guide sliding groove, and the distal ends of the two clamping plates 31 are each provided with clamping portions, using a double sliding structure to clamp the device. In one embodiment, the clamping plates 36 can be provided with a locking structure, whereby the clamping plates 36 function as a gripping structure for the hand.

[0027] In particular, the outer wall of the hard shell 11 is covered with a flexible layer to improve the feel of the aircraft cup.

[0028] In particular, as in Fig. As shown in Figure 7, elastic cable bodies 37 are provided on each side of the hard shell 11. When the rear wall of the player rests against the hard shell 11, the elastic cable body exerts a rearward elastic force on the front wall of the player, away from the hard shell 11, thereby locking the player in the hard shell 11.

[0029] In particular, the bracket 2 is attached to the outer wall of the hard shell 11, for example, a clamp; the bracket 2 is attached to the upper wall of the hard shell 11.

[0030] In particular, the base 21, as in Fig. 5, a deformable support strip 34. The support strip 34 can adjust the relative position of the holder 2, for example a universal joint 5, wherein the support strip 34 corresponds to the prior art, for example shape memory metal.

[0031] Fig. 1 to 3 show the first embodiment, which comprises a base 21, a positioning portion 31 and an adjusting portion 32, wherein the base 21 can be either formed integrally with the hard shell 11 or can be detachable.

[0032] Fig. 4 shows the second embodiment: base 21 and magnetic seat 33, wherein the base 21 and the hard shell 11 can be either integrally formed or removable.

[0033] Fig. 5 shows the third embodiment: the combination of base 21 and support strip 34, wherein the support strip 34 is bendable and the base 21 and the hard shell 11 can be either integrally formed or removable.

[0034] Fig. 6 shows the fourth embodiment: relatively sliding clamp, wherein the clamp slides relative to the hard shell 11.

[0035] Fig. 7 shows the fifth embodiment: An elastic rope body is attached to the hard shell 11.

[0036] Fig. 8 shows the sixth embodiment: the combination of clamp, positioning section 31 and adjustment section 32, wherein preferably a groove is provided in the hard shell 11 to fix the clamp.

[0037] Fig. 9 shows the seventh embodiment: The combination of base 21 and cardan 5 enables the adjustment of the relative angle of the clamp holder 3.

[0038] The above are only preferred embodiments of the present invention and do not limit the scope of the 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. Main body, 11. Hard shell, 11a. Interior, 12. Flexible wall, 12a. Channel, 2. Bracket, 21. Base, 3. Clamp holder, 31. Positioning section, 31a. First clamping section, 32. Adjustment section, 32a. Second clamping section, 33. Magnetic seat, 34. Support strips, 35. Clamp, 35a. Mounting ring, 35b. Retaining ring, 36. Terminal boards, 37. Elastic rope body, 41. Positioning hole, 42. Positioning pin, 5. Snowdrop.

Claims

[1] Aircraft cup with support structure, characterized by that it includes: - a main body, the main body comprising a hard shell provided with an interior space and a flexible wall arranged in the interior space, the flexible wall having a channel for the penetration of male genitals; - a holder, wherein the holder is attached to the wall surface of the hard shell and is designed to clamp the playback device. [2] Aircraft cup with support structure according to claim 1, characterized by that the holder comprises a base attached to the hard shell and a clamp holder attached to the base and designed to play audio and video. [3] Aircraft cup with support structure according to claim 2, characterized by that the clamp holder is a magnetic seat comprising a plate provided with magnets distributed around its circumference. [4] Aircraft cup with support structure according to claim 3, characterized by that the base and the magnetic seat are integrally formed or detachably arranged. [5] Aircraft cup with support structure according to claim 2, characterized by in that the clamp holder comprises a positioning section arranged on the base and an adjustment section slidably mounted on the positioning section, wherein the positioning section and the adjustment section are each provided with a first clamping section and a second clamping section which are arranged opposite one another, wherein the first clamping section and the second clamping section form a clamping distance and the adjustable clamping distance is designed for placing the playback device. [6] Aircraft cup with support structure according to claim 5, characterized by that the base and the positioning section are integrally molded. [7] Aircraft cup with support structure according to claim 5, characterized by that the base and the positioning section are arranged removably. [8] Aircraft cup with support structure according to claim 7, characterized by that the base and the positioning section are firmly connected to each other via a cardan joint. [9] Aircraft cup with support structure according to claim 2, characterized by that the base is removable and mounted on the hard shell. [10] Aircraft cup with support structure according to claim 8, characterized by that the base is a clamp, the clamp is designed to be removable, the clamp forms a clamp chamber corresponding to the size of the hard shell, and is attached to the outer wall of the hard shell. [11] Aircraft cup with support structure according to claim 10, characterized bythat the clamp comprises a fastening ring and a locking ring removably mounted on the fastening ring, one end of the fastening ring being pivotally connected to the locking ring and the other end being provided with a closure, the wall surface of the fastening ring being provided with a base. [12] Aircraft cup with support structure according to claim 9, characterized by that the hard shell is provided with a positioning hole and the base is provided with a positioning pin that matches the positioning hole. [13] Aircraft cup with support structure according to claim 11, characterized by that the positioning hole has an internal thread and the positioning pin has an external thread matching the internal thread. [14] Aircraft cup with support structure according to claim 2, characterized by that the base is firmly connected to the hard shell. [15] Aircraft cup with support structure according to claim 14, characterized by that the base is attached to the hard shell by rivets, injection-molded in one piece, fixed by snap connection or glued with adhesive. [16] Aircraft cup with support structure according to claim 1, characterized by that clamping plates which can be moved relative to one another are provided on both sides of the hard shell, wherein the hard shell is provided with guide sliding grooves, the clamping plate is installed so as to be movable in the guide sliding groove and the ends of the two clamping plates which are remote from one another are each provided with clamping sections. [17] Aircraft cup with support structure according to claim 1, characterized by that the outer wall of the hard shell is covered with a flexible layer. [18] Aircraft cup with support structure according to claim 1, characterized bythat elastic rope bodies are provided on both sides of the hard shell, the elastic rope body exerts a rearward-directed elastic force on the front wall of the playback device away from the hard shell when the rear wall of the playback device rests against the hard shell. [19] Aircraft cup with support structure according to claim 1, characterized by that the bracket is attached to the top wall or the outer wall of the hard shell. [20] Aircraft cup with support structure according to claim 2, characterized by that the base is a deformable support strip that can adjust the relative position of the bracket.

Images