CN105952758A - 一种蜂窝弹性复合材料用潜藏式螺纹组件及其锁紧方法 - Google Patents

一种蜂窝弹性复合材料用潜藏式螺纹组件及其锁紧方法 Download PDF

Info

Publication number
CN105952758A
CN105952758A CN201610516554.6A CN201610516554A CN105952758A CN 105952758 A CN105952758 A CN 105952758A CN 201610516554 A CN201610516554 A CN 201610516554A CN 105952758 A CN105952758 A CN 105952758A
Authority
CN
China
Prior art keywords
gradually
screw nut
pressure type
type
derotation
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.)
Pending
Application number
CN201610516554.6A
Other languages
English (en)
Inventor
王鹏
陈立
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tianjin Chengli Aviation Technology Co Ltd
Original Assignee
Tianjin Chengli Aviation Technology Co Ltd
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 Tianjin Chengli Aviation Technology Co Ltd filed Critical Tianjin Chengli Aviation Technology Co Ltd
Priority to CN201610516554.6A priority Critical patent/CN105952758A/zh
Publication of CN105952758A publication Critical patent/CN105952758A/zh
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B35/00Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws
    • F16B35/04Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws with specially-shaped head or shaft in order to fix the bolt on or in an object
    • F16B35/041Specially-shaped shafts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B23/00Specially shaped nuts or heads of bolts or screws for rotations by a tool
    • F16B23/0007Specially shaped nuts or heads of bolts or screws for rotations by a tool characterised by the shape of the recess or the protrusion engaging the tool
    • F16B23/0038Specially shaped nuts or heads of bolts or screws for rotations by a tool characterised by the shape of the recess or the protrusion engaging the tool substantially prismatic with up to six edges, e.g. triangular, square, pentagonal, Allen-type cross-sections
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B37/00Nuts or like thread-engaging members
    • F16B37/04Devices for fastening nuts to surfaces, e.g. sheets, plates
    • F16B37/041Releasable devices
    • F16B37/042Releasable devices locking by rotation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/01Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
    • F16B5/0275Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread the screw-threaded element having at least two axially separated threaded portions

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Prostheses (AREA)

Abstract

本发明属于航空航天用紧固件技术领域,尤其涉及一种蜂窝弹性复合材料用潜藏式螺纹组件。本发明包括潜藏式双头螺栓、渐压式正旋螺纹螺母和渐压式反旋螺纹螺母;所述渐压式正旋螺纹螺母和渐压式反旋螺纹螺母均包括内螺纹,渐压式正旋螺纹螺母的内螺纹为正旋内螺纹,渐压式反旋螺纹螺母的内螺纹为反旋内螺纹,还包括渐压壁;所述潜藏式双头螺栓包括承力杆,承力杆的两端外壁上分别设置有正旋外螺纹和反旋外螺纹,承力杆的两端分别向内凹陷设置有内扳拧结构。本发明结构简单、可反复拆装使用、由于采用渐压壁逐渐压缩复合材料基体,不会对基体造成损伤。本发明还涉及一种采用上述潜藏式螺纹组件进行锁紧的方法。

Description

一种蜂窝弹性复合材料用潜藏式螺纹组件及其锁紧方法
技术领域
本发明属于航空航天用紧固件技术领域,尤其涉及一种蜂窝弹性复合材料用潜藏式螺纹组件,还涉及一种采用上述潜藏式螺纹组件进行锁紧的方法。
背景技术
蜂窝复合材料起源于仿生学,并最早应用于航空航天领域,它是应航空航天科技的特殊需要而发展起来的一种超轻型的复合材料。
而在航空航天领域的应用中,各蜂窝弹性复合材料基体之间的连接固定,通常采用普通螺栓螺母连接,这些连接固定方式都会损伤蜂窝弹性复合材料基体,很多弹性复合材料是不允许有割伤或损伤的;有些采用铆钉铆接,铆钉铆接是永久固定,是不能进行再固定的,尤其是在某些区域需要多次拆装,还不能损伤蜂窝弹性复合材料;另外,在航空航天领域的使用中,要求复合材料的外表面平滑美观,用于连接固定的组件需要隐藏起来,上述的普通螺栓螺母连接和铆钉铆接不能满足隐藏安装的要求,同时安全可靠性等方面的性能也不能满足要求。
因此,为解决现有技术中存在的上述一系列难题,需要研发设计一种安装过程不损伤复合材料、可多次拆装且安全可靠性高的潜藏式螺纹组件。
发明内容
本发明为解决公知技术中存在的技术问题而提供一种建构简单、安装过程不损伤复合材料、可多次拆装且安全可靠性高的蜂窝弹性复合材料用潜藏式螺纹组件。
本发明为解决公知技术中存在的技术问题所采取的技术方案是:一种蜂窝弹性复合材料用潜藏式螺纹组件包括潜藏式双头螺栓,还包括可安装于潜藏式双头螺栓两端的渐压式正旋螺纹螺母和渐压式反旋螺纹螺母;所述渐压式正旋螺纹螺母和渐压式反旋螺纹螺母均包括贯穿螺母前端面和后端面的螺孔,螺孔内设置有内螺纹,渐压式正旋螺纹螺母的内螺纹为正旋内螺纹,渐压式反旋螺纹螺母的内螺纹为反旋内螺纹;还包括渐压壁,所述渐压壁的形状为沿螺母前端面至后端面呈渐开线式的曲面;所述潜藏式双头螺栓包括承力杆,承力杆的两端外壁上分别设置有与正旋内螺纹和反旋内螺纹相配合的正旋外螺纹和反旋外螺纹,承力杆的两端分别向内凹陷设置有内扳拧结构。
本发明的优点和积极效果是:由于采用渐压壁,安装过程中渐开线式的曲面逐渐压缩弹性复合材料基体而不会损伤到蜂窝弹性复合材料基体;通过旋转扳手就可将螺纹组件拧紧或拧松,因此可以反复拆装使用;由于采用潜藏式结构,紧固件零件都隐藏在复合材料内部,复合材料基体外部平滑美观,不易造成损伤。
优选地:所述内扳拧结构为内五角扳拧结构或内六角扳拧结构。
本发明的另一个目的是提供一种采用上述潜藏式螺纹组件对蜂窝弹性复合材料进行锁紧的方法。
本发明为解决公知技术中存在的技术问题所采取的技术方案是:一种采用上述蜂窝弹性复合材料用潜藏式螺纹组件进行锁紧的方法,包括以下步骤:a、从蜂窝弹性复合材料基体的一端插入将渐压式正旋螺纹螺母,从另一端放入潜藏式内五角双头螺栓,再继续插入渐压式反旋螺纹螺母;b、将扳手插入到渐压式反旋螺纹螺母的内扳拧结构中,顺时针旋转扳手,将两端的渐压式正旋螺纹螺母和渐压式反旋螺纹螺母拧紧,渐压壁逐渐压缩蜂窝弹性复合材料基体,螺纹组件处于紧固状态;c、需要拆卸螺纹组件时,将扳手插入到渐压式反旋螺纹螺母的内扳拧结构中,逆时针旋转扳手,将两端的渐压式正旋螺纹螺母和渐压式反旋螺纹螺母拧松。
附图说明
图1是本发明的半剖结构示意图;
图2是图1中渐压式反旋螺纹螺母的半剖结构示意图;
图3是图1中潜藏式双头螺栓的半剖结构示意图;
图4是本发明的安装实例的剖面结构示意图。
图中:1、渐压式正旋螺纹螺母;2、潜藏式双头螺栓;3、渐压式反旋螺纹螺母;4、渐压壁;5、正旋内螺纹;6、反旋内螺纹;7、正旋外螺纹;8、承力杆;9、反旋外螺纹;10、内扳拧结构;11、蜂窝弹性复合材料基体。
具体实施方式
为能进一步了解本发明的发明内容、特点及功效,兹例举以下实施例详细说明如下:
请参见图1,本发明包括潜藏式双头螺栓2,还包括可安装于潜藏式双头螺栓2两端的渐压式正旋螺纹螺母1和渐压式反旋螺纹螺母3。
请参见图2,所述渐压式正旋螺纹螺母1和渐压式反旋螺纹螺母3均包括贯穿螺母前端面和后端面的螺孔,螺孔内设置有内螺纹,渐压式正旋螺纹螺母1的内螺纹为正旋内螺纹5,渐压式反旋螺纹螺母3的内螺纹为反旋内螺纹6;还包括渐压壁4,所述渐压壁4的形状为沿螺母前端面至后端面呈渐开线式的曲面。
请参见图3,所述潜藏式双头螺栓2包括承力杆8,承力杆8的两端外壁上分别设置有与正旋内螺纹5和反旋内螺纹6相配合的正旋外螺纹7和反旋外螺纹9,承力杆8的两端分别向内凹陷设置有内扳拧结构10,所述内扳拧结构10为内五角扳拧结构或内六角扳拧结构。
请参见图4,采用上述蜂窝弹性复合材料用潜藏式螺纹组件进行锁紧的方法,包括以下步骤:a、从蜂窝弹性复合材料基体11的一端插入将渐压式正旋螺纹螺母1,从另一端放入潜藏式内五角双头螺栓2,再继续插入渐压式反旋螺纹螺母3;b、将扳手插入到渐压式反旋螺纹螺母3的内扳拧结构10中,顺时针旋转扳手,将两端的渐压式正旋螺纹螺母1和渐压式反旋螺纹螺母3拧紧,渐压壁4逐渐压缩蜂窝弹性复合材料基体11,螺纹组件处于紧固状态;c、需要拆卸螺纹组件时,将扳手插入到渐压式反旋螺纹螺母(3)的内扳拧结构10中,逆时针旋转扳手,将两端的渐压式正旋螺纹螺母1和渐压式反旋螺纹螺母3拧松。
本发明由于采用渐压壁,安装过程中渐开线式的曲面逐渐压缩弹性复合材料基体而不会损伤到蜂窝弹性复合材料基体;通过旋转扳手就可将螺纹组件拧紧或拧松,因此可以反复拆装使用;由于采用潜藏式结构,紧固件零件都隐藏在复合材料内部,复合材料基体外部平滑美观,不易造成损伤。
尽管已经示出和描述了本发明最佳的实施例,对于本领域的普通技术人员而言,可以理解在不脱离本发明的原理和精神的情况下可以对这些实施例进行多种变化、修改、替换和变型,本发明的范围由所附权利要求及其等同物限定。

Claims (3)

1.一种蜂窝弹性复合材料用潜藏式螺纹组件,其特征在于:包括潜藏式双头螺栓(2),还包括可安装于潜藏式双头螺栓(2)两端的渐压式正旋螺纹螺母(1)和渐压式反旋螺纹螺母(3);
所述渐压式正旋螺纹螺母(1)和渐压式反旋螺纹螺母(3)均包括贯穿螺母前端面和后端面的螺孔,螺孔内设置有内螺纹,渐压式正旋螺纹螺母(1)的内螺纹为正旋内螺纹(5),渐压式反旋螺纹螺母(3)的内螺纹为反旋内螺纹(6);还包括渐压壁(4),所述渐压壁(4)的形状为沿螺母前端面至后端面呈渐开线式的曲面;
所述潜藏式双头螺栓(2)包括承力杆(8),承力杆(8)的两端外壁上分别设置有与正旋内螺纹(5)和反旋内螺纹(6)相配合的正旋外螺纹(7)和反旋外螺纹(9),承力杆(8)的两端分别向内凹陷设置有内扳拧结构(10)。
2.如权利要求1所述的蜂窝弹性复合材料用潜藏式螺纹组件,其特征在于:所述内扳拧结构(10)为内五角扳拧结构或内六角扳拧结构。
3.采用如权利要求1或2所述的蜂窝弹性复合材料用潜藏式螺纹组件对复合材料进行锁紧的方法,其特征在于:包括以下步骤,
a、从蜂窝弹性复合材料基体(11)的一端插入将渐压式正旋螺纹螺母(1),从另一端放入潜藏式内五角双头螺栓(2),再继续插入渐压式反旋螺纹螺母(3);
b、将扳手插入到渐压式反旋螺纹螺母(3)的内扳拧结构(10)中,顺时针旋转扳手,将两端的渐压式正旋螺纹螺母(1)和渐压式反旋螺纹螺母(3)拧紧,渐压壁(4)逐渐压缩蜂窝弹性复合材料基体(11),螺纹组件处于紧固状态;
c、需要拆卸螺纹组件时,将扳手插入到渐压式反旋螺纹螺母(3)的内扳拧结构(10)中,逆时针旋转扳手,将两端的渐压式正旋螺纹螺母(1)和渐压式反旋螺纹螺母(3)拧松。
CN201610516554.6A 2016-06-30 2016-06-30 一种蜂窝弹性复合材料用潜藏式螺纹组件及其锁紧方法 Pending CN105952758A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610516554.6A CN105952758A (zh) 2016-06-30 2016-06-30 一种蜂窝弹性复合材料用潜藏式螺纹组件及其锁紧方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610516554.6A CN105952758A (zh) 2016-06-30 2016-06-30 一种蜂窝弹性复合材料用潜藏式螺纹组件及其锁紧方法

Publications (1)

Publication Number Publication Date
CN105952758A true CN105952758A (zh) 2016-09-21

Family

ID=56903220

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610516554.6A Pending CN105952758A (zh) 2016-06-30 2016-06-30 一种蜂窝弹性复合材料用潜藏式螺纹组件及其锁紧方法

Country Status (1)

Country Link
CN (1) CN105952758A (zh)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111268146A (zh) * 2020-02-24 2020-06-12 北京中航智科技有限公司 一种调节方法、机构及无人机

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4770584A (en) * 1986-03-27 1988-09-13 Nuovopignone Industrie Meccaniche E Fonderia S.P.A. Demountable pin, particularly suitable for the lever mechanisms of textile machines
DE202004000512U1 (de) * 2003-01-24 2004-04-08 Prüftechnik Dieter Busch AG Vorrichtung zum Befestigen eines Beschleunigungsaufnehmers
AU2005201707A1 (en) * 2005-04-22 2006-11-09 McGrogan, Kenneth John An Adjustable Support
CN102606569A (zh) * 2012-03-22 2012-07-25 宋丽萍 一种型腔板材多向连接件
CN203130718U (zh) * 2013-01-30 2013-08-14 李宇箭 正反牙双头中间六角盘膨胀螺栓
WO2014116972A1 (en) * 2013-01-28 2014-07-31 Patterson Richard Maclean Receipt and/or coupling of threaded rods respectively having incompatible thread patterns
CN205876922U (zh) * 2016-06-30 2017-01-11 天津成立航空技术有限公司 一种蜂窝弹性复合材料用潜藏式螺纹组件

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4770584A (en) * 1986-03-27 1988-09-13 Nuovopignone Industrie Meccaniche E Fonderia S.P.A. Demountable pin, particularly suitable for the lever mechanisms of textile machines
DE202004000512U1 (de) * 2003-01-24 2004-04-08 Prüftechnik Dieter Busch AG Vorrichtung zum Befestigen eines Beschleunigungsaufnehmers
AU2005201707A1 (en) * 2005-04-22 2006-11-09 McGrogan, Kenneth John An Adjustable Support
CN102606569A (zh) * 2012-03-22 2012-07-25 宋丽萍 一种型腔板材多向连接件
WO2014116972A1 (en) * 2013-01-28 2014-07-31 Patterson Richard Maclean Receipt and/or coupling of threaded rods respectively having incompatible thread patterns
CN203130718U (zh) * 2013-01-30 2013-08-14 李宇箭 正反牙双头中间六角盘膨胀螺栓
CN205876922U (zh) * 2016-06-30 2017-01-11 天津成立航空技术有限公司 一种蜂窝弹性复合材料用潜藏式螺纹组件

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111268146A (zh) * 2020-02-24 2020-06-12 北京中航智科技有限公司 一种调节方法、机构及无人机

Similar Documents

Publication Publication Date Title
CN202187997U (zh) 一种防转翻铆式自锁螺母
CN205592264U (zh) 一种自锁式插销
CN205876922U (zh) 一种蜂窝弹性复合材料用潜藏式螺纹组件
CN110145525A (zh) 一种拉铆紧固件
CN105952758A (zh) 一种蜂窝弹性复合材料用潜藏式螺纹组件及其锁紧方法
CN204664109U (zh) 一种挤压装配螺母连接副
CN107781273A (zh) 一种对开自锁螺母
CN206190708U (zh) 螺纹紧固件伴侣
US20140312610A1 (en) Pipe joint structure
CN108644216A (zh) 一种具有防松功能的不脱落螺钉组件
CN207364078U (zh) 一种防松动易装配的螺栓组件
CN206738364U (zh) 组合式螺母
CN102588418A (zh) 一种防止锁紧螺栓松动的方法及锁紧螺栓组合件
CN202749609U (zh) 一种带有直推式防松锁紧装置的尾部附件
CN203023236U (zh) 插齿加翻铆的组合防转锁紧螺母组件
CN106837976A (zh) 一种螺纹紧固件伴侣
CN104826757A (zh) 高压水枪
CN205876923U (zh) 一种夹层锁紧用潜藏式空心内锁螺纹组件
CN210218371U (zh) 组合锁紧螺母
CN211820309U (zh) 一种防松螺栓
CN211261451U (zh) 一种冰箱
CN209294209U (zh) 一种汽车锁紧螺丝
CN204921619U (zh) 一种新型螺钉
CN203809465U (zh) 飞行器用防转动螺栓螺母组件
CN206175444U (zh) 螺母紧固件

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20160921

RJ01 Rejection of invention patent application after publication