Outer fuel tank access cover, wing and aircraft description

An outer fuel access tank cover (FTAC) of an aircraft, a wing including such outer FTAC of an aircraft, and an aircraft are disclosed. The outer FTAC of an aircraft is related to designing auxiliary pieces in the wing of aircrafts to control the risk of gases from an explosion occurred in the FTAC e...

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Bibliographische Detailangaben
1. Verfasser:	ALAZRAKI MARCOS
Format:	Patent
Sprache:	eng
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:	An outer fuel access tank cover (FTAC) of an aircraft, a wing including such outer FTAC of an aircraft, and an aircraft are disclosed. The outer FTAC of an aircraft is related to designing auxiliary pieces in the wing of aircrafts to control the risk of gases from an explosion occurred in the FTAC entering the fuel tank.