FUEL TANK DAM

A fuel tank dam (10) comprises a first section (11), a second section (12), a third section (13), and a flange section (14). The first section (11) can be fixed to a first structural component, and the second section (12) can be fixed to a second structural component. The third section (13) has a be...

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Bibliographische Detailangaben
Hauptverfasser:	TADA, Hajime, OKUDA, Akihisa, OKABE, Ryoji, KURITA, Tadasuke, TAGUCHI, Yoko, SAKON, Kana, YAMAGUCHI, Eizaburo
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A fuel tank dam (10) comprises a first section (11), a second section (12), a third section (13), and a flange section (14). The first section (11) can be fixed to a first structural component, and the second section (12) can be fixed to a second structural component. The third section (13) has a bellows (15) comprising a plurality of folded sections (16) and is disposed between the first section (11) and the second section (12). The flange section (14) extends along an outer plate at least from an edge section (22) of the third section (13) and can be fixed to the outer plate.