RU2006140136A - Illuminator frame for aircraft - Google Patents

Illuminator frame for aircraft Download PDF

Info

Publication number
RU2006140136A
RU2006140136A RU2006140136/11A RU2006140136A RU2006140136A RU 2006140136 A RU2006140136 A RU 2006140136A RU 2006140136/11 A RU2006140136/11 A RU 2006140136/11A RU 2006140136 A RU2006140136 A RU 2006140136A RU 2006140136 A RU2006140136 A RU 2006140136A
Authority
RU
Russia
Prior art keywords
frame
porthole
flange
aircraft
clamp
Prior art date
Application number
RU2006140136/11A
Other languages
Russian (ru)
Inventor
Енс БОЛД (DE)
Енс БОЛД
Original Assignee
Эйрбас Дойчланд Гмбх (De)
Эйрбас Дойчланд Гмбх
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
Priority claimed from DE102004025383A external-priority patent/DE102004025383B4/en
Application filed by Эйрбас Дойчланд Гмбх (De), Эйрбас Дойчланд Гмбх filed Critical Эйрбас Дойчланд Гмбх (De)
Publication of RU2006140136A publication Critical patent/RU2006140136A/en

Links

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
    • B64C1/1476—Canopies; Windscreens or similar transparent elements
    • B64C1/1492—Structure and mounting of the transparent elements in the window or windscreen

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Securing Of Glass Panes Or The Like (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
  • Laminated Bodies (AREA)

Claims (3)

1. Рама иллюминатора для установки во внешнем корпусе летательного аппарата, которая содержит1. The frame of the porthole for installation in the outer casing of the aircraft, which contains внешний фланец;outer flange; внутренний фланец;inner flange; вертикальный фланец;vertical flange; прозрачную часть иллюминатора; иthe transparent part of the porthole; and прижимной фиксатор;clamping clamp; причем вертикальный фланец размещается между внешним и внутренним фланцами и расположен перпендикулярно по отношению к ним;moreover, a vertical flange is placed between the outer and inner flanges and is perpendicular to them; внешний фланец предназначен для формирования соединения рамы иллюминатора с несущим элементом летательного аппарата;the outer flange is designed to form the connection of the window frame with the supporting element of the aircraft; прозрачная часть иллюминатора опирается по меньшей мере на внутренний фланец или вертикальный фланец;the transparent portion of the porthole rests at least on the inner flange or vertical flange; прозрачная часть иллюминатора фиксируется прижимным фиксатором, который соединен с рамой иллюминатора;the transparent part of the porthole is fixed with a clamping clamp, which is connected to the frame of the porthole; и прижимной фиксатор выполнен из синтетической смолы, усиленной волокном и получен штамповкой с глубокой вытяжкой.and the clamping lock is made of synthetic resin reinforced with fiber and obtained by stamping with deep drawing. 2. Рама иллюминатора по п.1, в которой прижимной фиксатор содержит многослойную структуру, которая представляет собой квазиизотропную пластину.2. The frame of the window according to claim 1, in which the clamp holder contains a multilayer structure, which is a quasi-isotropic plate. 3. Способ изготовления прижимного фиксатора для рамы иллюминатора по п.1, содержащий следующие операции:3. A method of manufacturing a clamp retainer for the frame of the window according to claim 1, containing the following operations: получение из термопластичного материала и тканой ленты заготовки, которая представляет собой квазиизотропный листовой материал,obtaining from a thermoplastic material and a woven tape preform, which is a quasi-isotropic sheet material, и затем осуществление процесса штамповки с глубокой вытяжкой для получения из заготовки прижимного фиксатора.and then the implementation of the stamping process with deep drawing to obtain from the workpiece clamping clamp.
RU2006140136/11A 2004-05-24 2005-05-24 Illuminator frame for aircraft RU2006140136A (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE102004025383.8 2004-05-24
DE102004025383A DE102004025383B4 (en) 2004-05-24 2004-05-24 Window frame for aircraft
US60010204P 2004-08-09 2004-08-09
US60/600,102 2004-08-09

Publications (1)

Publication Number Publication Date
RU2006140136A true RU2006140136A (en) 2008-05-20

Family

ID=34970359

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2006140136/11A RU2006140136A (en) 2004-05-24 2005-05-24 Illuminator frame for aircraft

Country Status (6)

Country Link
EP (1) EP1755944A1 (en)
JP (1) JP2008500235A (en)
BR (1) BRPI0510970A (en)
CA (1) CA2564173A1 (en)
RU (1) RU2006140136A (en)
WO (1) WO2005115841A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009008903A1 (en) * 2007-01-12 2009-01-15 The Nordam Group, Inc. Aircraft window erosion shield
FR2928343B1 (en) 2008-03-10 2010-08-20 Airbus France PORCH PANEL AND METHOD OF MANUFACTURING SUCH AN AIRCRAFT PANEL COMPRISING A DOOR PANEL
DE102020125610A1 (en) 2020-09-30 2022-03-31 Premium Aerotec Gmbh Window frame for a vehicle and method of manufacturing a window frame

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2507565B2 (en) * 1988-11-24 1996-06-12 東レ株式会社 Composite board of thermoplastic resin and reinforcing fiber
US5271581A (en) * 1992-05-29 1993-12-21 Irish Michael J Window clip for aircraft
JP3214646B2 (en) * 1994-03-07 2001-10-02 東レ株式会社 Preform and manufacturing method thereof

Also Published As

Publication number Publication date
BRPI0510970A (en) 2007-11-27
CA2564173A1 (en) 2005-12-08
JP2008500235A (en) 2008-01-10
EP1755944A1 (en) 2007-02-28
WO2005115841A1 (en) 2005-12-08

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Legal Events

Date Code Title Description
FA94 Acknowledgement of application withdrawn (non-payment of fees)

Effective date: 20100701