WO2018176209A1 - 一种飞机杯 - Google Patents

一种飞机杯 Download PDF

Info

Publication number
WO2018176209A1
WO2018176209A1 PCT/CN2017/078379 CN2017078379W WO2018176209A1 WO 2018176209 A1 WO2018176209 A1 WO 2018176209A1 CN 2017078379 W CN2017078379 W CN 2017078379W WO 2018176209 A1 WO2018176209 A1 WO 2018176209A1
Authority
WO
WIPO (PCT)
Prior art keywords
card
protrusion
casing
retaining
slot
Prior art date
Application number
PCT/CN2017/078379
Other languages
English (en)
French (fr)
Inventor
李欣
Original Assignee
深圳市为乐科技有限公司
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 深圳市为乐科技有限公司 filed Critical 深圳市为乐科技有限公司
Priority to PCT/CN2017/078379 priority Critical patent/WO2018176209A1/zh
Publication of WO2018176209A1 publication Critical patent/WO2018176209A1/zh

Links

Images

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits

Definitions

  • the present invention relates to the field of sex toys and, more particularly, to an aircraft cup.
  • common aircraft cups generally include a cup body, a core control component, and a housing.
  • the cup body and the core control component are disposed in the housing for protection by the housing.
  • the housing In order to facilitate the cleaning of the cup body and the loading and unloading of the battery, the housing generally includes an upper housing and a lower housing, and the upper housing and the lower housing are detachably connected.
  • a snap-fit is generally adopted.
  • the general clamping force requires a large disassembly force, and the card protrusion of the engaging portion is required to be deformed to cause the card portion to be easily damaged, thereby causing the upper and lower casings to be closed, and reducing the aircraft. The life of the cup.
  • an object of the present invention is to provide an aircraft cup which can effectively solve the problem of inconvenient disassembly of the aircraft cup.
  • the present invention provides the following technical solutions:
  • An aircraft cup comprising an upper casing and a lower casing, comprising a card protrusion and a card member, wherein the card protrusion is composed of an upper card protrusion and a lower card protrusion which are disposed apart from each other up and down, the card slot and the card protrusion of the card member Slidingly engaging in a longitudinal direction to prevent the upper card protrusion from being disengaged from the lower card protrusion in an up-and-down direction, the upper card protrusion being relatively fixed to the upper case, the lower card protrusion being relatively fixed to the lower case .
  • one side of the upper case and one side of the lower case are hinged by a hinge; the other side of the upper case is provided with the upper card protrusion, and the other side of the lower case Set the card Convex.
  • the card has a dovetail cross section, and the card slot is a dovetail slot.
  • the upper side of the upper casing, the lower casing and the card member are all located on the same cylindrical side.
  • the outer side of the outer side of the card member is adjacent to the upper case and the lower case, respectively.
  • the hinge is disposed inside the upper casing and disposed inside the lower casing.
  • one end of the card member is provided with a card slot, and the other end is provided with a pulling protrusion.
  • the invention provides an aircraft cup comprising an upper casing, a lower casing, a card protrusion and a card member.
  • the card protrusion is composed of an upper card protrusion and a lower card protrusion which are separated by upper and lower sides, that is, the card protrusion includes an upper card protrusion and a lower card protrusion.
  • the upper card protrusion and the upper case are relatively fixed, and may be integrally formed or fixedly connected; wherein the lower card protrusion and the lower case are relatively fixed, and may be integrally formed or fixedly connected.
  • the card member is provided with a card slot, and the card slot and the card protrusion are slidably engaged in the longitudinal direction to prevent the upper card protrusion and the lower card protrusion from being separated in the up and down direction.
  • the aircraft cup when the aircraft cup is applied, when the upper casing and the lower casing are closed, it is necessary to prevent the two from moving in the up and down direction, and the card convex can be slid in the longitudinal direction.
  • the card slot of the card member is inserted into the card slot of the card member to prevent relative movement of the upper case and the lower case through the card slot of the card member.
  • the upper and lower groove walls of the card slot are respectively opposed to the upper and lower card protrusions, thereby effectively preventing the upper case and the lower case from moving relative to each other in the up and down direction, thereby effectively securing the upper case and the lower case.
  • the shells are relatively fixed between each other, and the sliding between the card slot and the card protrusion is convenient, the sliding fit is convenient to install, the detaching is also very convenient, and the card slot or the card convexity does not appear to be damaged during the disassembly process. And in the process of frequent disassembly and assembly, the disassembly and assembly will become smoother and smoother.
  • the aircraft cup can effectively solve the problem of inconvenient assembly and disassembly of the aircraft cup.
  • FIG. 1 is a schematic cross-sectional structural view of an aircraft cup according to an embodiment of the present invention.
  • FIG. 2 is a schematic structural diagram of a card provided by an embodiment of the present invention.
  • FIG. 3 is a schematic structural view of a housing in an unfolded state according to an embodiment of the present invention.
  • the embodiment of the invention discloses an aircraft cup to effectively solve the problem that the aircraft cup is inconvenient to be disassembled.
  • FIG. 1 is a schematic cross-sectional view of an aircraft cup according to an embodiment of the present invention
  • FIG. 2 is a schematic structural view of a card member according to an embodiment of the present invention
  • the present embodiment provides an aircraft cup comprising an upper casing 1, a lower casing 2, a card projection and a card member 5, and of course other necessary components, such as Cup and drive parts, etc.
  • a storage chamber is formed between the upper casing 1 and the lower casing 2, and is generally used for placing components such as batteries or driving components in the storage chamber.
  • the outer side of the upper casing 1 and the outer side of the lower casing 2 are generally on a cylindrical side, or on the outer side of a rotating body, to facilitate the holding of the upper casing 1 and the lower casing 2 .
  • the card protrusion is composed of an upper card protrusion 3 and a lower card protrusion 4 which are separated from each other, that is, the card protrusion includes the upper card protrusion 3 and the lower card protrusion 4.
  • the upper card protrusion 3 is fixed to the upper casing 1 , and may be integrally formed or fixedly connected.
  • the lower card protrusion 4 is fixed to the lower casing 2 , and may be integrally formed or fixedly connected.
  • the upper card convex 3 and the lower card convex 4 are separated from each other in the up and down direction, and the upper card convex 3 and the lower card convex 4 are relatively moved in the up and down direction, so that the upper card convex 3 and the lower card convex 4 can be separated to be independent. Two parts.
  • the card member 5 is provided with a card slot 6, and the card slot 6 is slidably engaged with the card protrusion in the longitudinal direction to prevent the upper card protrusion 3 and the lower card protrusion 4 from being disengaged in the up and down direction. That is, the notch of the card slot 6 faces in the lateral direction, so that the upper and lower groove walls of the card slot 6 respectively abut against the upper side of the upper tab 3 and the lower side of the lower tab 4 to prevent the upper tab 3 from moving upward, preventing The lower tab 4 moves downward, which in turn prevents the upper tab 3 and the lower tab 4 from separating in the up and down direction.
  • the relative movement of the upper card protrusion 3 and the lower card protrusion 4 in the lateral direction can be fixed by a pin, for example, on the upper card protrusion 3 and the lower card protrusion 4, one is provided with a pin, and the other is provided with a jack, which can be Fixed by other directions, no specific difference is made here. It should be noted that the longitudinal direction mentioned here and below refers to the extending direction of the entire aircraft cup.
  • the upper casing 1 and the lower casing 2 are closed, it is necessary to prevent the two from moving relative to each other in the up and down direction, and the card protrusion can be slid into the longitudinal direction at this time.
  • the card slot 6 of the card member 5 the upper case 1 and the lower case 2 are prevented from moving relative to each other by the card slot 6 of the card member 5.
  • the upper and lower groove walls of the card slot 6 are respectively opposed to the upper card protrusion 3 and the lower card protrusion 4, so that the upper case 1 and the lower case 2 can be effectively prevented from moving relative to each other in the up and down direction, thereby effectively ensuring
  • the relative fixing between the upper casing 1 and the lower casing 2 is a sliding fit between the card slot 6 and the card protrusion, the sliding fit is convenient to install, the detaching is also very convenient, and no strong force occurs during the disassembly process. Destroy the card slot 6 or the card protrusion, and in the process of frequent disassembly and assembly, the disassembly and assembly will become smoother and smoother.
  • the aircraft cup can effectively solve the problem of inconvenient assembly and disassembly of the aircraft cup.
  • one side of the upper case 1 and one side of the lower case 2 are hinged by a hinge; the other side of the upper case 1 is provided with an upper tab 3, and the other side of the lower case 2 is provided with a lower card Convex 4.
  • the upper casing 1 and the lower casing 2 can only move up and down between the upper casing 1 and the lower casing 2 on the side where the cam is provided. It is of course possible to provide the card housing and the card member 5 on both sides of the upper case 1 and the lower case 2, but the installation is very inconvenient, and the one side hinge is used to effectively avoid the upper case 1 and the lower case. 2 completely separated, and fully restrains the degree of freedom of the upper casing 1 relative to the other direction of the lower casing 2, which is extremely convenient for operation, Moreover, the inner chambers of the upper casing 1 and the lower casing 2 can also be sufficiently opened.
  • the cross section of the convex portion is a dovetail type
  • the card slot 6 is a dovetail groove.
  • the swallow-tail type card slot 6 is slidably engaged with the dovetail type card to prevent the card protrusion from being disengaged from the card slot 6 in the groove depth direction of the card slot 6 by its structural shape characteristics.
  • the restraining member or the card member 5 can also be used, but the card convex portion and the card member 5 can be disassembled and assembled inconveniently, and the overall cost is greatly increased.
  • the outer side surfaces of the upper casing 1, the lower casing 2 and the card member 5 are all located on the same cylindrical side surface so that the outer contour of the entire aircraft cup is cylindrical to improve the comfort of the hand grip.
  • the outer side surface of the card member 5 may be further adjacent to the upper casing 1 and the lower casing 2, respectively, to avoid the card member 5 and the upper casing 1 and the lower casing.
  • the above-mentioned hinge is disposed inside the upper casing 1 and is provided inside the lower casing 2 to avoid the pin projection of the hinge.
  • the front end of the card member 5 is provided with a card slot 6, and the rear end is provided with a pulling protrusion.
  • the tab 5 can be pulled by hand to slide the card member 5 away from the card protrusion.

Landscapes

  • Health & Medical Sciences (AREA)
  • Physical Education & Sports Medicine (AREA)
  • Mechanical Engineering (AREA)
  • Reproductive Health (AREA)
  • Epidemiology (AREA)
  • Pain & Pain Management (AREA)
  • Engineering & Computer Science (AREA)
  • Rehabilitation Therapy (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Animal Behavior & Ethology (AREA)
  • General Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Veterinary Medicine (AREA)
  • Toys (AREA)

Abstract

一种飞机杯，包括上壳体（1）和下壳体（2），还包括卡凸（3，4）和卡件（5），该卡凸（3，4）由沿上下分离设置的上卡凸（3）和下卡凸（4）组成，该卡件（5）的卡槽（6）与卡凸（3，4）沿纵向方向滑动配合以阻止该上卡凸（3）与该下卡凸（4）沿上下方向脱离，该上卡凸（3）与该上壳体（1）相对固定，该下卡凸（4）与该下壳体（2）相对固定。在该飞机杯中，通过卡槽（6）的上下槽壁分别与上卡凸（3）和下卡凸（4）相抵，可以有效地阻止上壳体（1）和下壳体（2）沿上下方向相对移动，继而有效地保证上壳体（1）和下壳体（2）之间的相对固定，同时卡槽（6）与卡凸（3，4）之间为滑动配合，拆装方便，且拆装会越来越顺畅。综上，该飞机杯可以有效地解决飞机杯拆装不方便的问题。

Description

一种飞机杯 技术领域
本发明涉及情趣用品领域，更具体地说，涉及一种飞机杯。
背景技术
随着各种生活关系，目前服务于男性和女性的各种情趣用品，需求越来越大。如前男性使用的情趣用品一般具有仿阴腔，如飞机杯。
目前常见的飞机杯，一般包括杯体、核心控制部件和壳体。其中杯体以及核心控制部件均设置在壳体内，以通过壳体进行保护。为了方便清洗杯体以及装卸电池等原因，壳体一般包括上壳体和下壳体，且使上壳体和下壳体可拆卸连接，为了拆卸方便，一般采用卡扣卡接。但是经过发明人长期研究发现，一般的卡接，需要的拆卸力比较大，而且需要卡接部的卡凸强制变形，以导致卡接部容易损坏，进而导致上下壳体无法合上，降低飞机杯的使用寿命。
综上所述，如何有效地解决飞机杯拆开不方便的问题，是目前本领域技术人员急需解决的问题。
发明内容
有鉴于此，本发明的目的在于提供一种飞机杯，该飞机杯可以有效地解决飞机杯拆开不方便的问题。
为了达到上述目的，本发明提供如下技术方案：
一种飞机杯，包括上壳体和下壳体，包括卡凸和卡件，所述卡凸由沿上下分离设置的上卡凸和下卡凸组成，所述卡件的卡槽与卡凸沿纵向方向滑动配合以阻止所述上卡凸与所述下卡凸沿上下方向脱离，所述上卡凸与所述上壳体相对固定，所述下卡凸与所述下壳体相对固定。
优选地，所述上壳体的一侧和所述下壳体的一侧通过铰链铰接；所述上壳体的另一侧设置有所述上卡凸，所述下壳体的另一侧设置有所述下卡 凸。
优选地，所述卡凸的横截面呈燕尾型，所述卡槽为燕尾型槽。
优选地，所述上壳体、所述下壳体和所述卡件的外侧面均位于同一圆柱侧面上。
优选地，所述卡件的外侧面上下两侧分别与所述上壳体和所述下壳体毗邻。
优选地，所述铰链设置在所述上壳体的内侧，且设置在所述下壳体的内侧。
优选地，沿纵向方向上，所述卡件的一端设置有卡槽，另一端设置有拉动凸起。
本发明提供的一种飞机杯，该飞机杯包括上壳体、下壳体、卡凸和卡件。其中卡凸由上下分离设置的上卡凸和下卡凸组成，即卡凸包括上卡凸和下卡凸。其中上卡凸与上壳体相对固定，具体可以是一体成型，也可以是固定连接；其中下卡凸与下壳体相对固定，具体可以是一体成型，也可以是固定连接。而其中的卡件上设置有卡槽，卡槽与卡凸沿纵向方向滑动配合，以阻止上卡凸和下卡凸沿上下方向脱离。
根据是上述的技术方案，可以知道，在应用该飞机杯时，当上壳体和下壳体合上时，需要阻止两者沿上下方向相对移动时，此时可以将卡凸沿纵向方向滑入至卡件的卡槽内，以通过卡件的卡槽阻止上壳体和下壳体相对移动。在该飞机杯中，通过卡槽的上下槽壁分别与上卡凸和下卡凸相抵，可以有效地阻止上壳体和下壳体沿上下方向相对移动，进而有效地保证上壳体和下壳体之间的相对固定，同时卡槽与卡凸之间为滑动配合，滑动配合安装方便，拆离也非常方便，且在拆装的过程中不会出现强力破坏卡槽或卡凸的情况，且在频繁拆装过程中，会使拆装越来越顺畅。综上所述，该飞机杯可以有效地解决飞机杯拆装不方便的问题。
附图说明
为了更清楚地说明本发明实施例或现有技术中的技术方案，下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍，显而易见地， 下面描述中的附图仅仅是本发明的一些实施例，对于本领域普通技术人员来讲，在不付出创造性劳动的前提下，还可以根据这些附图获得其他的附图。
图1为本发明实施例提供的飞机杯的横截面结构示意图；
图2为本发明实施例提供的卡件的结构示意图；
图3为本发明实施例提供的壳体展开状态下的结构示意图。
附图中标记如下：
上壳体1、下壳体2、上卡凸3、下卡凸4、卡件5、卡槽6。
具体实施方式
本发明实施例公开了一种飞机杯，以有效地解决飞机杯拆开不方便的问题。
下面将结合本发明实施例中的附图，对本发明实施例中的技术方案进行清楚、完整地描述，显然，所描述的实施例仅仅是本发明一部分实施例，而不是全部的实施例。基于本发明中的实施例，本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例，都属于本发明保护的范围。
请参阅图1-图3，图1为本发明实施例提供的飞机杯的横截面结构示意图；图2为本发明实施例提供的卡件的结构示意图；图3为本发明实施例提供的壳体展开状态下的结构示意图。
在一种具体实施例中，本实施例提供了一种飞机杯，该飞机杯包括上壳体1、下壳体2、卡凸和卡件5，当然还会包括其他一些必要的部件，如杯体和驱动部件等。
其中上壳体1和下壳体2之间会形成一个置物腔，在置物腔内一般用于放置电池或驱动部件等部件。为了使用方便，上壳体1的外侧面和下壳体2的外侧面一般会在一个圆柱侧面上，或在一个回转体的外侧面上，以方便手握上壳体1和下壳体2。
其中卡凸由上下分离设置的上卡凸3和下卡凸4组成，即卡凸包括上卡凸3和下卡凸4。其中上卡凸3与上壳体1相对固定，具体可以是一体成型，也可以是固定连接；其中下卡凸4与下壳体2相对固定，具体可以是一体成型，也可以是固定连接。其中上卡凸3和下卡凸4上下方向分离设置，指的是上卡凸3和下卡凸4沿上下方向相对移动后，可以使上卡凸3和下卡凸4分离开来成独立的两个部件。
而其中的卡件5上设置有卡槽6，卡槽6与卡凸沿纵向方向滑动配合，以阻止上卡凸3和下卡凸4沿上下方向脱离。即卡槽6的槽口朝向为横向方向，以使卡槽6的上下槽壁分别与上卡凸3的上侧面和下卡凸4的下侧面相抵，以阻止上卡凸3向上移动，阻止下卡凸4向下移动，继而阻止上卡凸3和下卡凸4沿上下方向分离。而上卡凸3和下卡凸4横向方向的相对移动，可以通过插销固定，具体的如，在上卡凸3和下卡凸4上，一个设置有插销，另一个设置有插孔，可以通过其它方向固定，在此处不做具体相抵。需要说明的是，此处以及下文中所提到的纵向方向，指的是整个飞机杯的延伸方向。
在本实施例中，在应用该飞机杯时，当上壳体1和下壳体2合上时，需要阻止两者沿上下方向相对移动时，此时可以将卡凸沿纵向方向滑入至卡件5的卡槽6内，以通过卡件5的卡槽6阻止上壳体1和下壳体2相对移动。在该飞机杯中，通过卡槽6的上下槽壁分别与上卡凸3和下卡凸4相抵，可以有效地阻止上壳体1和下壳体2沿上下方向相对移动，进而有效地保证上壳体1和下壳体2之间的相对固定，同时卡槽6与卡凸之间为滑动配合，滑动配合安装方便，拆离也非常方便，且在拆装的过程中不会出现强力破坏卡槽6或卡凸的情况，且在频繁拆装过程中，会使拆装越来越顺畅。综上所述，该飞机杯可以有效地解决飞机杯拆装不方便的问题。
进一步的，优选上壳体1的一侧和下壳体2的一侧通过铰链铰接；上壳体1的另一侧设置有上卡凸3，下壳体2的另一侧设置有下卡凸4。以在设置有卡凸的一侧，上壳体1和下壳体2之间只能够上下移动。当然可以使上壳体1和下壳体2的两侧均设置有卡凸和卡件5，但是这样安装非常不方便，而采用一侧铰接，能够有效地避免上壳体1和下壳体2完全分离，并充分约束上壳体1相对下壳体2其它方向的自由度，极大的方便操作， 而且同样能够使上壳体1和下壳体2内腔充分打开。
进一步的，优选卡凸的横截面呈燕尾型，且卡槽6为燕尾型槽。以通过燕尾型卡槽6与燕尾型的卡凸相配合滑动，以通过自身的结构形状特性，能够有效地阻止卡凸沿卡槽6的槽深方向脱离卡槽6。当然还可以在卡凸上设置有限位滑孔，但是闭合性不好，且增加的结构设置不方便。当然还可以采用约束件或卡件5，但是会导致卡凸和卡件5拆装不方便，且大大增大整体成本。
进一步地，优选上壳体1、下壳体2和卡件5的外侧面均位于同一圆柱侧面上，以使得整个飞机杯的外轮廓呈圆柱形，以提高手握的舒适感。且为了提高闭合性，以方便清理，可以进一步地，使卡件5的外侧面上下两侧分别与上壳体1和下壳体2毗邻，以避免卡件5与上壳体1和下壳体2之间存在间隙槽，容易藏污，不方便后期做卫生清理。同样的，为了美观，此处优选上述铰链设置在上壳体1的内侧，且设置有下壳体2的内侧，以避免铰链的销轴凸起。
进一步的，优选沿纵向方向上，所述卡件5的前端设置有卡槽6，后端设置有拉动凸起。以在取出卡件5时，可以通过手持拉动凸起，拖动卡件5滑离卡凸。通过拉动凸起的设置，大大方便操作手对卡件5施加拉动力。
本说明书中各个实施例采用递进的方式描述，每个实施例重点说明的都是与其他实施例的不同之处，各个实施例之间相同相似部分互相参见即可。
对所公开的实施例的上述说明，使本领域专业技术人员能够实现或使用本发明。对这些实施例的多种修改对本领域的专业技术人员来说将是显而易见的，本文中所定义的一般原理可以在不脱离本发明的精神或范围的情况下，在其它实施例中实现。因此，本发明将不会被限制于本文所示的这些实施例，而是要符合与本文所公开的原理和新颖特点相一致的最宽的范围。

Claims (7)

  1. 一种飞机杯，包括上壳体和下壳体，其特征在于，包括卡凸和卡件，所述卡凸由沿上下分离设置的上卡凸和下卡凸组成，所述卡件的卡槽与卡凸沿纵向方向滑动配合以阻止所述上卡凸与所述下卡凸沿上下方向脱离，所述上卡凸与所述上壳体相对固定，所述下卡凸与所述下壳体相对固定。
  2. 根据权利要求1所述的飞机杯，其特征在于，所述上壳体的一侧和所述下壳体的一侧通过铰链铰接；所述上壳体的另一侧设置有所述上卡凸，所述下壳体的另一侧设置有所述下卡凸。
  3. 根据权利要求2所述的飞机杯，其特征在于，所述卡凸的横截面呈燕尾型，所述卡槽为燕尾型槽。
  4. 根据权利要求3所述的飞机杯，其特征在于，所述上壳体、所述下壳体和所述卡件的外侧面均位于同一圆柱侧面上。
  5. 根据权利要求4所述的飞机杯，其特征在于，所述卡件的外侧面上下两侧分别与所述上壳体和所述下壳体毗邻。
  6. 根据权利要求5所述的飞机杯，其特征在于，所述铰链设置在所述上壳体的内侧，且设置在所述下壳体的内侧。
  7. 根据权利要求6所述的飞机杯，其特征在于，沿纵向方向上，所述卡件的一端设置有卡槽，另一端设置有拉动凸起。
PCT/CN2017/078379 2017-03-28 2017-03-28 一种飞机杯 WO2018176209A1 (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/CN2017/078379 WO2018176209A1 (zh) 2017-03-28 2017-03-28 一种飞机杯

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2017/078379 WO2018176209A1 (zh) 2017-03-28 2017-03-28 一种飞机杯

Publications (1)

Publication Number Publication Date
WO2018176209A1 true WO2018176209A1 (zh) 2018-10-04

Family

ID=63673910

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2017/078379 WO2018176209A1 (zh) 2017-03-28 2017-03-28 一种飞机杯

Country Status (1)

Country Link
WO (1) WO2018176209A1 (zh)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2650180A (en) * 1951-07-05 1953-08-25 Stanley F Walker Insulating device for pipes, faucets, and the like
US3455336A (en) * 1965-11-03 1969-07-15 Raychem Corp Heat recoverable article and process
US4133442A (en) * 1976-12-27 1979-01-09 Structural Fibers, Inc. Tank closure assembly
EP0223424A1 (en) * 1985-10-21 1987-05-27 N.V. Raychem S.A. Closure for wraparound sleeve
CN1152203A (zh) * 1995-09-21 1997-06-18 阿尔卡泰尔电缆公司 一种底物的紧密包封装置
CN102475590A (zh) * 2010-11-26 2012-05-30 翁浩琪 一种治疗早泄或刺激男性充血状海绵体的装置

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2650180A (en) * 1951-07-05 1953-08-25 Stanley F Walker Insulating device for pipes, faucets, and the like
US3455336A (en) * 1965-11-03 1969-07-15 Raychem Corp Heat recoverable article and process
US4133442A (en) * 1976-12-27 1979-01-09 Structural Fibers, Inc. Tank closure assembly
EP0223424A1 (en) * 1985-10-21 1987-05-27 N.V. Raychem S.A. Closure for wraparound sleeve
CN1152203A (zh) * 1995-09-21 1997-06-18 阿尔卡泰尔电缆公司 一种底物的紧密包封装置
CN102475590A (zh) * 2010-11-26 2012-05-30 翁浩琪 一种治疗早泄或刺激男性充血状海绵体的装置

Similar Documents

Publication Publication Date Title
USD931212S1 (en) Earpiece charging case
USD931206S1 (en) Earpiece charging case with window
USD912015S1 (en) Combined earphone with charging cradle
US9226550B1 (en) Zipper head assembly structure
KR101965468B1 (ko) 클립
US20130318751A1 (en) Zipper head and pull tab replacement method
MX2010002105A (es) Estuche para almacenar maquinas de afeitar que poseen miembros de cierre en union completa.
EP3412167B1 (en) Paint fixture for shoe portions
USD877613S1 (en) Clamshell package for a cartridge valve
WO2018176209A1 (zh) 一种飞机杯
US20160143493A1 (en) Combination Heightened Toilet Seat Assembly
CN108336567A (zh) 一种改进型的信息终端电源设备
CN209644789U (zh) 一种马桶刷及与之配套的马桶刷座
US20190111852A1 (en) Vehicle Sun Visor Multiple Glasses Storage Apparatus
CN207366854U (zh) 便携式眼镜
KR200427550Y1 (ko) 피어싱 장신구
KR20160003369U (ko) 힌지 개폐 구조를 갖는 화장품용기
CN202402261U (zh) 一种充气泵的壳体结构
WO2015142096A1 (ko) 안경테의 결합구조체
CN208957671U (zh) 手柄及锅盖及压力锅
US20180252013A1 (en) Detachable hinge assembly
KR20120006903A (ko) 자동차용 후드 스테이 로드
CN206465636U (zh) 开合装置及其打印机
CN213890933U (zh) 用于热水器的发泡定位工装
KR200376047Y1 (ko) 원터치 튜브피팅의 로크클러 구조

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 17903076

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

32PN Ep: public notification in the ep bulletin as address of the adressee cannot be established

Free format text: NOTING OF LOSS OF RIGHTS PURSUANT TO RULE 112(1) EPC (EPO FORM 1205A DATED 23/01/2020)

122 Ep: pct application non-entry in european phase

Ref document number: 17903076

Country of ref document: EP

Kind code of ref document: A1