AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING CAPABILITY

AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING CAPABILITY

Aircraft with vertical takeoff and landing capability and casing bodies The invention relates to an aircraft (1) with vertical takeoff and landing capability, comprising a fuselage (2) with a longitudinal axis (L) and with multiple casing bodies (30) arranged on the fuselage (2), wherein at least on...

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Bibliographische Detailangaben
Hauptverfasser: SANCHA GARCIA, Luis Antonio, FRICKE, Martin, SAUER, Sebastian, LÜDERS, Ralf, KURZ, Carlo, ZLATKOV, Branislav, TAPPE, Oliver
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:Aircraft with vertical takeoff and landing capability and casing bodies The invention relates to an aircraft (1) with vertical takeoff and landing capability, comprising a fuselage (2) with a longitudinal axis (L) and with multiple casing bodies (30) arranged on the fuselage (2), wherein at least one of the casing bodies (30) is mounted so as to be rotatable about a transverse axis (Q) arranged at an angle with respect to the longitudinal axis (L), and wherein the aircraft (1) comprises at least one propulsion device (10) with a rotatable turbomachine (20) and one of the casing bodies (30), wherein the rotatable turbomachine (20) has an axis of rotation (R) which is rotatable by means of the transverse axis (Q), and the casing body (30) has a substantially cylindrical section (31) extending along the axis of rotation (R), wherein the cylindrical section (31) coaxially surrounds the turbomachine (20). It is provided that the casing body (30) is designed to generate lift, in particular during horizontal flight of the aircraft (1), whereby the casing body is thus in the form of an annular wing.