CN106741832A - 一种对接式可调节内饰口盖 - Google Patents

一种对接式可调节内饰口盖 Download PDF

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Publication number
CN106741832A
CN106741832A CN201611160301.6A CN201611160301A CN106741832A CN 106741832 A CN106741832 A CN 106741832A CN 201611160301 A CN201611160301 A CN 201611160301A CN 106741832 A CN106741832 A CN 106741832A
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CN
China
Prior art keywords
lid
dock
trim panel
trim
interior trim
Prior art date
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Pending
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CN201611160301.6A
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English (en)
Inventor
孙迪
黄奕佳
王雯
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Xian Aircraft Design and Research Institute of AVIC
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Xian Aircraft Design and Research Institute of AVIC
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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 CN201611160301.6A priority Critical patent/CN106741832A/zh
Publication of CN106741832A publication Critical patent/CN106741832A/zh
Pending legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1407—Doors; surrounding frames
    • B64C1/1446—Inspection hatches

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)

Abstract

本发明涉及舱内机载设备与内饰板对接方式的优化设计，涉及一种对接式可调节内饰口盖。口盖用于对接外部设备，其特征为：所述的口盖呈喇叭形，口盖安装固定在内饰板上。本发明构型较为简单，可显著消除累积误差，增加对接调节余量，整体性好，同时降低安装人员定位的工作量，方便易操作。对接式可调节内饰口盖材料可选用复合材料及非金属塑料件，成型方便，成本较低。

Description

一种对接式可调节内饰口盖
技术领域
本发明涉及舱内机载设备与内饰板对接方式的优化设计，涉及一种对接式可调节内饰口盖。
背景技术
目前舱内常见的内饰对接形式包括两种，一种是直接在内饰板上开口对接设备，另一种是在内饰板上做翻遍对接设备。这两种方式均对安装精度要求较高，若设备预先固定在结构支架上，内饰板对接时易因安装误差积累无法精确对接。
发明内容
本发明的目的：提供一种能够对结构支架上的设备进行精准包覆对接的可调节内饰口盖。
本发明的技术方案：一种对接式可调节内饰口盖，口盖用于对接外部设备，其特征为：所述的口盖呈喇叭形，口盖安装固定在内饰板上。
优选地，喇叭形口盖纵深角度为15°～30°。
优选地，口盖嵌在内饰板开口内，内饰板开口尺寸为设备外露尺寸的1.5～2倍。
优选地，口盖嵌在内饰板开口内，口盖四周与内饰板均有3-4mm调节余量。
本发明的有益效果：本发明构型较为简单，可显著消除累积误差，增加对接调节余量，整体性好，同时降低安装人员定位的工作量，方便易操作。对接式可调节内饰口盖材料可选用复合材料及非金属塑料件，成型方便，成本较低。
附图说明
图1为本发明的结构示意图；
图2为内饰板开口示意图；
图3为口盖主视图；
图4为口盖立体图；
图5为组装示意图。
具体实施方式
下面对本发明做进一步详细说明。
口盖2用螺钉固定在内饰板上1，也可通过尼龙搭扣直接粘接在内饰板上1，内饰板1开口尺寸根据设备3外露尺寸确定，建议为设备3外露尺寸X、Y的1.5～2倍，见图2。
口盖2的特征在于造型为喇叭形，可四向调节，见图3和图4。其长L、宽W尺寸比内饰板1多40mm，相当于四边均比内饰板1开口长20mm，四边有14mm搭接在内饰板1上，除去口盖倒角设计，四向均有3～4mm调节余量，口盖深度h根据设备3需外露部分距内饰板1的直线距离确定，喇叭形纵深角度无固定要求，建议为15°～30°，具体可根据实际内饰板分块及舱内布置区域大小确定。

Claims (4)

1.一种对接式可调节内饰口盖，口盖用于对接外部设备，其特征为：所述的口盖呈喇叭形，口盖安装固定在内饰板上。
2.根据权利要求1所述的一种对接式可调节内饰口盖，其特征为：喇叭形口盖纵深角度为15°～30°。
3.根据权利要求1所述的一种对接式可调节内饰口盖，其特征为：口盖嵌在内饰板开口内，内饰板开口尺寸为设备外露尺寸的1.5～2倍。
4.根据权利要求1所述的一种对接式可调节内饰口盖，其特征为：口盖嵌在内饰板开口内，口盖四周与内饰板均有3-4mm调节余量。
CN201611160301.6A 2016-12-15 2016-12-15 一种对接式可调节内饰口盖 Pending CN106741832A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611160301.6A CN106741832A (zh) 2016-12-15 2016-12-15 一种对接式可调节内饰口盖

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611160301.6A CN106741832A (zh) 2016-12-15 2016-12-15 一种对接式可调节内饰口盖

Publications (1)

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CN106741832A true CN106741832A (zh) 2017-05-31

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109592042A (zh) * 2018-11-02 2019-04-09 中国航空工业集团公司西安飞机设计研究所 一种在飞机内饰板上安装设备的方法

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5014934A (en) * 1989-06-30 1991-05-14 The Boeing Company Removable seal for discontinuities in aircraft skin
US20080190568A1 (en) * 2007-02-09 2008-08-14 Airbus Deutschland Gmbh Aircraft Window Darkening System
US20150040484A1 (en) * 2011-08-19 2015-02-12 Aerovironment, Inc. Water-tight compartment with removable hatch and two-sided gel seal for multiple conduit access
CN205203357U (zh) * 2015-12-11 2016-05-04 中国航空工业集团公司西安飞机设计研究所 一种飞机增压舱外蒙皮系统操纵件气密安装结构
CN205293060U (zh) * 2015-11-25 2016-06-08 中航贵州飞机有限责任公司 一种飞机壁板维修用整体口盖

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5014934A (en) * 1989-06-30 1991-05-14 The Boeing Company Removable seal for discontinuities in aircraft skin
US20080190568A1 (en) * 2007-02-09 2008-08-14 Airbus Deutschland Gmbh Aircraft Window Darkening System
US20150040484A1 (en) * 2011-08-19 2015-02-12 Aerovironment, Inc. Water-tight compartment with removable hatch and two-sided gel seal for multiple conduit access
CN205293060U (zh) * 2015-11-25 2016-06-08 中航贵州飞机有限责任公司 一种飞机壁板维修用整体口盖
CN205203357U (zh) * 2015-12-11 2016-05-04 中国航空工业集团公司西安飞机设计研究所 一种飞机增压舱外蒙皮系统操纵件气密安装结构

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109592042A (zh) * 2018-11-02 2019-04-09 中国航空工业集团公司西安飞机设计研究所 一种在飞机内饰板上安装设备的方法

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