CN105673630B - 一种可调节的内饰连接结构 - Google Patents

一种可调节的内饰连接结构 Download PDF

Info

Publication number
CN105673630B
CN105673630B CN201410662910.6A CN201410662910A CN105673630B CN 105673630 B CN105673630 B CN 105673630B CN 201410662910 A CN201410662910 A CN 201410662910A CN 105673630 B CN105673630 B CN 105673630B
Authority
CN
China
Prior art keywords
bracket
cornual plate
trim panel
hole
connection structure
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.)
Active
Application number
CN201410662910.6A
Other languages
English (en)
Other versions
CN105673630A (zh
Inventor
黄奕佳
孙迪
陈勇
谷煜
王磊
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.)
Xian Aircraft Design and Research Institute of AVIC
Original Assignee
Xian Aircraft Design and Research Institute of AVIC
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 Xian Aircraft Design and Research Institute of AVIC filed Critical Xian Aircraft Design and Research Institute of AVIC
Priority to CN201410662910.6A priority Critical patent/CN105673630B/zh
Publication of CN105673630A publication Critical patent/CN105673630A/zh
Application granted granted Critical
Publication of CN105673630B publication Critical patent/CN105673630B/zh
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Vehicle Interior And Exterior Ornaments, Soundproofing, And Insulation (AREA)

Abstract

本发明涉及一种飞机内饰。提供一种可调节的内饰连接结构,包括:在内饰板1上开有通孔,盲孔镶嵌件2预埋在内饰板1中,内饰板1背面使用盲孔镶嵌件2和螺钉3固定角片4,支架5直接安装于结构上,角片4和支架5上开有相互垂直的长条孔;安装时通过两处相互垂直的长条孔实现角片4相对支架5在四个方向的调节,调节到所需位置后,使用弹簧夹托板螺母6和螺钉7将角片4与支架5固定。本发明可有效消除安装过程中累积的误差,实现安装现场的快速调节,提高工作效率并降低成本。

Description

一种可调节的内饰连接结构
技术领域
本发明涉及一种用于飞机内饰的可调节连接结构。
背景技术
目前,飞机内饰板结构设计缺少有效的调节余度,无法消除在安装过程中产生的累积误差,经常导致原有的安装孔位无法使用,需现场重新配孔,影响安装精度及效果,降低工作效率。
发明内容
发明目的
提供一种可调节的内饰连接结构,可有效消除安装过程中累积的误差,实现安装现场的快速调节,提高工作效率并降低成本。
技术方案
一种可调节的内饰连接结构,包括:
在内饰板1上开有通孔,盲孔镶嵌件2预埋在内饰板1中,内饰板1背面使用盲孔镶嵌件2和螺钉3固定角片4,支架5直接安装于结构上,角片4和支架5上开有相互垂直的长条孔;安装时通过两处相互垂直的长条孔实现角片4相对支架5在四个方向的调节,调节到所需位置后,使用弹簧夹托板螺母6和螺钉7将角片4与支架5固定。
还包括:在内饰板1的通孔处安装堵盖8。
有益效果
本发明具有结构简单、安装便捷的优点,可实现四个方向的调节,有效消除安装过程中累积的误差,实现安装现场的快速调节,提高工作效率并降低成本,并可有效遮盖紧固件,起到防尘防异物进入的效果。
附图说明
图1为本发明内饰板可调节结构示意图背面。
图2为图1的A区域放大图。
图3为本发明内饰板可调节结构剖视图。
具体实施方式
本发明提供一种可调节的内饰连接结构,如图1、2、3所示,包括:内饰板1、盲孔镶嵌件2、螺钉3、7、角片4、支架5、弹簧夹托板螺母6、堵盖8。
在内饰板1上开有通孔,盲孔镶嵌件2预埋在内饰板1中,内饰板1背面使用盲孔镶嵌件2和螺钉3固定角片4,支架5直接安装于结构上,角片4和支架5上开有相互垂直的长条孔;安装时通过两处相互垂直的长条孔实现角片4相对支架5在四个方向的调节,调节到所需位置后,使用弹簧夹托板螺母6和螺钉7将角片4与支架5固定。在内饰板1的通孔处安装堵盖8,遮盖紧固件,起到防尘防异物进入的效果。
上述实施方式只为说明本发明的技术构思及特点,目的在于让熟悉此项技术的人士能够了解本发明的内容并加以实施,并不能以此限制本发明的保护范围,凡根据本发明精神实质所作的等效变化或修饰,都应涵盖在本发明的保护范围内。

Claims (2)

1.一种可调节的内饰连接结构,其特征在于,包括:
在内饰板(1)上开有通孔,盲孔镶嵌件(2)预埋在内饰板(1)中,内饰板(1)背面使用盲孔镶嵌件(2)和螺钉(3)固定角片(4),支架(5)直接安装于结构上,角片(4)和支架(5)上开有相互垂直的长条孔;安装时通过两处相互垂直的长条孔实现角片(4)相对支架(5)在四个方向的调节,调节到所需位置后,使用弹簧夹托板螺母(6)和螺钉(7)将角片(4)与支架(5)固定。
2.如权利要求1所述的一种可调节的内饰连接结构,其特征在于,还包括:在内饰板(1)的通孔处安装堵盖(8)。
CN201410662910.6A 2014-11-19 2014-11-19 一种可调节的内饰连接结构 Active CN105673630B (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410662910.6A CN105673630B (zh) 2014-11-19 2014-11-19 一种可调节的内饰连接结构

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410662910.6A CN105673630B (zh) 2014-11-19 2014-11-19 一种可调节的内饰连接结构

Publications (2)

Publication Number Publication Date
CN105673630A CN105673630A (zh) 2016-06-15
CN105673630B true CN105673630B (zh) 2019-05-10

Family

ID=56945665

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410662910.6A Active CN105673630B (zh) 2014-11-19 2014-11-19 一种可调节的内饰连接结构

Country Status (1)

Country Link
CN (1) CN105673630B (zh)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113650814A (zh) * 2021-09-17 2021-11-16 北京国电高科科技有限公司 一种便捷型防护装置

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201367052Y (zh) * 2009-02-18 2009-12-23 上海世科嘉车辆技术研发有限公司 一种汽车塑料翼子板安装固定结构
CN203906485U (zh) * 2014-04-10 2014-10-29 北汽福田汽车股份有限公司 自攻螺钉组件

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6263621B1 (en) * 1999-09-08 2001-07-24 General Electric Company Leveling and securing apparatus
NL2009393C2 (en) * 2012-08-30 2014-03-03 Driessen Aerospace Group Nv Locking assembly for locking an aircraft interior structure to an internal mounting frame in an aircraft cabin.

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201367052Y (zh) * 2009-02-18 2009-12-23 上海世科嘉车辆技术研发有限公司 一种汽车塑料翼子板安装固定结构
CN203906485U (zh) * 2014-04-10 2014-10-29 北汽福田汽车股份有限公司 自攻螺钉组件

Also Published As

Publication number Publication date
CN105673630A (zh) 2016-06-15

Similar Documents

Publication Publication Date Title
USD709419S1 (en) Vehicle door trim set
WO2012104064A3 (en) Aircraft interior component system and method for mounting an interior component system in an aircraft
EP4008610A3 (en) Aerodynamic system and adjustable fairings
MX2017013932A (es) Soporte integrado.
DE602006012335D1 (de) Halterung fuer flugzeugtriebwerk
EP2143638A3 (en) Lightning protection system for an aircraft composite structure
MX2013009589A (es) Soporte multifuncional para un vehiculo.
EP2669184A3 (en) Wall installation system and method
RU2014111672A (ru) Профиль ступени для аварийно-спасательной машины, в частности для пожарной машины
WO2014172719A3 (en) A transition arrangement for an aircraft
MX2010002720A (es) Conjunto de capa superficial del parachoques y medios de ocultamiento.
WO2010107829A3 (en) Systems and methods for providing an accessorizable frame system
EP2883793A3 (en) Luggage system having a component installation space
EP2476618A3 (en) Integrated bleed and engine controller
SG11201908810RA (en) Seat unit and lower structure thereof
MX351195B (es) Dispositivo de sujeción y método de alineación para montar partes de vehículos.
MX2017011672A (es) Soporte suspendido para sistemas de eje/suspension.
WO2009062047A3 (en) Frame with integrated surface attachment for drywall and drywall-like surfaces
WO2012154545A3 (en) Striker stiffener reinforcement
EP2700573A3 (en) A pressurized airplane fuselage, comprising a pressure bulkhead
CN105673630B (zh) 一种可调节的内饰连接结构
MX341407B (es) Placa de montaje de un solo sujetador para tomacorrientes electricos.
EP2569185A4 (en) AIR CIRCULATION CONTROL SYSTEM FOR VEHICLE AND METHOD OF CONTROLLING AIR CIRCULATION TO A RADIATOR BELONGING TO A VEHICLE COOLING SYSTEM
CN202303813U (zh) 空调器
RU2017145013A (ru) Монтажная система для крепления стенного уголка проводящей текучую среду установки на стене

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant