Application of a titanium-carbon fiber metal laminate in an in-flight opening fighter door loaded in acoustic fatigue. Part 1: Design and Analysis

MJL van Tooren; P de Haan; S Brouwer; C Verhoeven; E Veen

Application of a titanium-carbon fiber metal laminate in an in-flight opening fighter door loaded in acoustic fatigue. Part 1: Design and Analysis

MJL van Tooren, P de Haan, S Brouwer, C Verhoeven, E Veen

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

Abstract

This paper discusses the results of a design project with the goal to research and promote the use of Fiber Metal Laminates (FML) in other applications than currently under exploration. In vieuw of one of the strong points of Glare (an FML of glass fiber reinforced epoxy prepreg between aluminum sheets), superior fatigue properties compared to solid aluminum, an in-flight opening door of a fighter aircraft was selected to be designed in a new FML. This fighter door is subject to a high acoustic loading and operated at high temperature. This paper deals with the design and analysis of the component in an FML of titanium and a carbon fiber reinforced polymer. Also tests on material and component level are discussed.

Original language	Undefined/Unknown
Title of host publication	ICCM-14
Place of Publication	San Diego, Californie
Pages	-
Publication status	Published - 2003
Event	14th International Conference on Composite Materials - San Diego, Californie Duration: 14 Jul 2003 → 18 Jul 2003

Conference

Conference	14th International Conference on Composite Materials
Period	14/07/03 → 18/07/03

Bibliographical note

CD-rom, paper # 1582

Keywords

conference contrib. refereed
Conf.proc. > 3 pag

Cite this

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title = "Application of a titanium-carbon fiber metal laminate in an in-flight opening fighter door loaded in acoustic fatigue. Part 1: Design and Analysis",

abstract = "This paper discusses the results of a design project with the goal to research and promote the use of Fiber Metal Laminates (FML) in other applications than currently under exploration. In vieuw of one of the strong points of Glare (an FML of glass fiber reinforced epoxy prepreg between aluminum sheets), superior fatigue properties compared to solid aluminum, an in-flight opening door of a fighter aircraft was selected to be designed in a new FML. This fighter door is subject to a high acoustic loading and operated at high temperature. This paper deals with the design and analysis of the component in an FML of titanium and a carbon fiber reinforced polymer. Also tests on material and component level are discussed.",

keywords = "conference contrib. refereed, Conf.proc. > 3 pag",

author = "{van Tooren}, MJL and {de Haan}, P and S Brouwer and C Verhoeven and E Veen",

note = "CD-rom, paper # 1582; 14th International Conference on Composite Materials ; Conference date: 14-07-2003 Through 18-07-2003",

year = "2003",

language = "Undefined/Unknown",

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T1 - Application of a titanium-carbon fiber metal laminate in an in-flight opening fighter door loaded in acoustic fatigue. Part 1: Design and Analysis

AU - van Tooren, MJL

AU - de Haan, P

AU - Brouwer, S

AU - Verhoeven, C

AU - Veen, E

N1 - CD-rom, paper # 1582

PY - 2003

Y1 - 2003

N2 - This paper discusses the results of a design project with the goal to research and promote the use of Fiber Metal Laminates (FML) in other applications than currently under exploration. In vieuw of one of the strong points of Glare (an FML of glass fiber reinforced epoxy prepreg between aluminum sheets), superior fatigue properties compared to solid aluminum, an in-flight opening door of a fighter aircraft was selected to be designed in a new FML. This fighter door is subject to a high acoustic loading and operated at high temperature. This paper deals with the design and analysis of the component in an FML of titanium and a carbon fiber reinforced polymer. Also tests on material and component level are discussed.

AB - This paper discusses the results of a design project with the goal to research and promote the use of Fiber Metal Laminates (FML) in other applications than currently under exploration. In vieuw of one of the strong points of Glare (an FML of glass fiber reinforced epoxy prepreg between aluminum sheets), superior fatigue properties compared to solid aluminum, an in-flight opening door of a fighter aircraft was selected to be designed in a new FML. This fighter door is subject to a high acoustic loading and operated at high temperature. This paper deals with the design and analysis of the component in an FML of titanium and a carbon fiber reinforced polymer. Also tests on material and component level are discussed.

KW - conference contrib. refereed

KW - Conf.proc. > 3 pag

M3 - Conference contribution

SP - -

BT - ICCM-14

CY - San Diego, Californie

T2 - 14th International Conference on Composite Materials

Y2 - 14 July 2003 through 18 July 2003

ER -