FLAP ADJUSTING SYSTEM OF AN AIRCRAFT WITH A REGULATING FLAP

The invention pertains to a flap adjusting system of an aircraft that features: - at least one regulating flap (A1, A2; B1, B2) that is respectively mounted on one of the airfoils of an aircraft by means of at least two bearing devices (LS) and movable relative to the airfoil, - at least one adjusti...

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Bibliographische Detailangaben
Hauptverfasser:	GREIF, STEFAN, SCHWINN, ROBERT, RECKSIEK, MARTIN
Format:	Patent
Sprache:	eng ; fre
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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