CN200980714Y - Induced labor airbag - Google Patents

Induced labor airbag Download PDF

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Publication number
CN200980714Y
CN200980714Y CN 200620161354 CN200620161354U CN200980714Y CN 200980714 Y CN200980714 Y CN 200980714Y CN 200620161354 CN200620161354 CN 200620161354 CN 200620161354 U CN200620161354 U CN 200620161354U CN 200980714 Y CN200980714 Y CN 200980714Y
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CN
China
Prior art keywords
balloon
airbag
uterus
inner wall
inner walls
Prior art date
Application number
CN 200620161354
Other languages
Chinese (zh)
Inventor
赵红芳
肖航
吴美英
Original Assignee
赵红芳
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 赵红芳 filed Critical 赵红芳
Priority to CN 200620161354 priority Critical patent/CN200980714Y/en
Application granted granted Critical
Publication of CN200980714Y publication Critical patent/CN200980714Y/en

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Abstract

The utility model discloses an induced labor balloon, which essentially comprises an ellipsoidal balloon (1) with a joint (2) and is characterized in that grooves (3) evenly or unevenly arranged are provided on the inner wall of the balloon (1), wherein when the balloon is charged with the compressed air or the liquid, due to the inner walls are different in thickness and the inner walls located on the grooves (3) are thinner, the inner walls project outwards for forming the configuration like the structure of blunt stings on the outer walls of the balloon (1), and surfaces become unsmooth. Thus the stimulation of the uterus inner wall is speeded up for forming more intensive compaction to uterus and achieving the goal of faster parturitions and abortions. Mastering the quantity of the air pressure or the water pressure can fit to the demands of different publics.

Description

一种引产气囊 One kind of abortion balloon

技术领域 FIELD

本实用新型属于医疗器械,确切的讲是一种引产气囊。 The present invention belongs to medical devices, the exact stresses induced abortion is a balloon.

背景技术 Background technique

对于妇产科的流产引产手术,一般都采用引产气囊刺激子宫内壁增加宫缩强度,达到辅助流产引产的目的。 Gynecologic surgery for induction of abortion, induction of labor airbag generally used to stimulate contractions of the uterus to increase strength, achieve the purpose of the auxiliary induction of abortion. 而目前使用的气囊为内外表面均是平滑的结构,这样,刺激的强度就不怎么明显、不够大,因此有时候手术需要较长的时间,被手术者也很痛苦。 The air bags currently used for the inner and outer surfaces are smooth structure, so that the intensity of the stimulus is not clear how, is not big enough, so sometimes surgery takes a long time, the surgery is very painful. 为了解决这个问题,本实用新型的设计人做了认真地研究,提出了本实用新型的发明目的。 To solve this problem, the present invention is designed to make a person seriously studied, the purpose of the present invention invention.

发明内容 SUMMARY

本实用新型的发明目的是为了克服目前使用的气囊为内外表面均是平滑的结构,因产、流产手术时对子宫产生的刺激的强度不明显、不够大,而使手术需要较长的时间,被手术者也很痛苦的不足而提出来的。 The object of the present invention is to overcome the invention currently used for the airbag are both smooth inner and outer surfaces of the structure, due to birth, abortion of the uterus when the stimulus intensity generated obvious, is not big enough, the operation takes a long time, surgery is very painful deficiencies of their argument.

本实用新型的技术解决方案是这样实现的,该引产气囊,主要具有一个带有接头[2]的椭球形的气囊[1],其特征在于在气囊[1]的内壁上具有均匀或者不均匀排列的凹槽[3]。 The present invention technical solution is achieved, the induction airbag, the airbag having a main connection with [2] ellipsoidal [1], characterized by having a uniform or non-uniform on the inner wall of the airbag [1] arranged in the recess [3].

本实用新型的有益的技术效果是显而易见的。 This has the beneficial technical effect is obvious. 当气囊内通入压缩空气或者液体时,由于其内壁厚度不同,凹槽[3]处的内壁较薄,则会在压力的作用下向外凸起,使得气囊[1]的外壁形成类似钝刺的结构形状,即表面变得不光滑了。 When the pressurized air or a liquid into the balloon, due to different wall thicknesses within the recess [3] at the inner wall is thin, will be outwardly convex under the effect of pressure, so that the airbag [1] is similar to the external wall forming obtuse thorn structural shape, i.e., the surface becomes smoother. 这样,会加速刺激子宫内壁,以形成更加强烈的宫缩,实现比较快速的引产、流产的目的。 In this way, it will accelerate to stimulate the lining of the uterus to form a more intense contractions, achieve more rapid induction of labor, abortion purposes. 掌握气压或者水压的大小,可以适应不同人群的需要。 Grasp the size of the air pressure or water pressure, you can meet the needs of different groups of people.

附图说明 BRIEF DESCRIPTION

附图是本实用新型的结构剖面示意视图。 Figures present invention is a schematic cross-sectional view of the structure. 在附图中的序号描述为:1、气囊,2、接头,3、凹槽。 Reference is depicted in the drawings: 1, the airbag 2, linker 3, a groove.

具体实施方式 Detailed ways

下面结合附图中给出的实施例,对本实用新型的结构和使用进行详细说明。 DRAWINGS embodiments given in the examples, the present invention is described in detail the structure and use. 参照附图,该装置主要具有一个带有接头[2]的椭球形的气囊[1],在气囊[1]的内壁上具有均匀或者不均匀排列的凹槽[3]。 Referring to the drawings, the apparatus having an airbag with a primary linker [2] ellipsoidal [1], having a uniform or non-uniform arrangement of the airbag on the inner wall of the groove [1] of [3]. 使用时,将气囊[2]导入子宫内,向气囊内通入压缩空气或者液体,由于其内壁厚度不同,凹槽[3]处的内壁较薄,则会在气压或者液压的压力作用下向外凸起,使得气囊[1]的外壁形成类似钝刺的结构形状,即表面变得不光滑了。 In use, the airbag [2] is introduced into the uterus, into the air or a liquid into the balloon, due to different wall thicknesses within the recess [3] at the inner wall is thin, will be under pressure to the pneumatic or hydraulic an outer projection, such that the airbag [1] is formed in the outer wall structure is shaped like a blunt spines, i.e., the surface becomes smoother. 这样,会加速刺激子宫内壁,以形成更加强烈的宫缩,实现比较快速的引产、流产的目的。 In this way, it will accelerate to stimulate the lining of the uterus to form a more intense contractions, achieve more rapid induction of labor, abortion purposes. 在实际操作时还可以通过增加和减小气囊[2]内的压力的方法实现凹槽[3]的膨胀和收缩,以进一步增加对子宫内壁的刺激。 Grooves may be achieved by increasing and decreasing the pressure of the airbag [2] a method in practice Shihai [3] of the expansion and contraction, to further increase the stimulation of the lining of the uterus.

Claims (1)

1.一种引产气囊,主要具有一个带有接头[2]的椭球形的气囊[1],其特征在于在气囊[1]的内壁上具有均匀或者不均匀排列的凹槽[3]。 An induction air bag, having a predominantly spheroidal joint [2] of the airbag [1], characterized by having a uniform or non-uniform arrangement of the airbag on the inner wall of the groove [1] of [3].
CN 200620161354 2006-12-04 2006-12-04 Induced labor airbag CN200980714Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200620161354 CN200980714Y (en) 2006-12-04 2006-12-04 Induced labor airbag

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200620161354 CN200980714Y (en) 2006-12-04 2006-12-04 Induced labor airbag

Publications (1)

Publication Number Publication Date
CN200980714Y true CN200980714Y (en) 2007-11-28

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN 200620161354 CN200980714Y (en) 2006-12-04 2006-12-04 Induced labor airbag

Country Status (1)

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CN (1) CN200980714Y (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8684954B1 (en) 2013-03-14 2014-04-01 Plexus Biomedical, Inc. Labor management devices for decreasing the incidence of Cesarean childbirth
US10080520B2 (en) 2015-02-27 2018-09-25 Stetrix, Inc. Labor monitoring of pelvic floor

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8684954B1 (en) 2013-03-14 2014-04-01 Plexus Biomedical, Inc. Labor management devices for decreasing the incidence of Cesarean childbirth
US8888719B2 (en) 2013-03-14 2014-11-18 Plexus Biomedical, Inc. Labor management devices for decreasing the incidence of cesarean childbirth
US9089301B2 (en) 2013-03-14 2015-07-28 Stetrix Inc. Labor management devices providing pelvic floor support
US9089300B2 (en) 2013-03-14 2015-07-28 Stretrix Inc. Labor management devices for decreasing the incidence of cesarean childbirth
US9326721B2 (en) 2013-03-14 2016-05-03 Stetrix, Inc. Labor management devices for pelvic floor support
US9993192B2 (en) 2013-03-14 2018-06-12 Stetrix, Inc. Labor management methods for decreasing the duration of second stage labor
US10080520B2 (en) 2015-02-27 2018-09-25 Stetrix, Inc. Labor monitoring of pelvic floor

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