Outer fuel tank access cover, wing and aircraft

The present invention describes an outer fuel tank access cover (4) (FTAC) of an aircraft comprising an explosion gas relief means (8) adapted for letting the explosion gases escape to the atmosphere, a wing comprising such outer FTAC (4) of an aircraft and an aircraft. The invention belongs to the...

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Bibliographische Detailangaben
1. Verfasser:	ALAZRAKI, MARCOS
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE TRANSPORTING
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Beschreibung
Zusammenfassung:	The present invention describes an outer fuel tank access cover (4) (FTAC) of an aircraft comprising an explosion gas relief means (8) adapted for letting the explosion gases escape to the atmosphere, a wing comprising such outer FTAC (4) of an aircraft and an aircraft. The invention belongs to the field of designing auxiliary pieces in the wing of aircraft to control the risk of gases from an explosion occurred in the FTAC entering the fuel tank.