Three=axis steering aircraft of canard type

Three=axis steering aircraft of canard type

The rear fin and rudder assembly (19) is V-shaped, while the propeller circle (4) is covered on the down side by fins (3). The fuselage (1) support is in the form of a lattice frame (5), with the cross-beam (2) forming part of the frame. Pref., the aircraft fuselage has a triangular configuration in...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: SCHLACHTER, MANFRED, 67133 MAXDORF, DE
Format: Patent
Sprache:eng ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The rear fin and rudder assembly (19) is V-shaped, while the propeller circle (4) is covered on the down side by fins (3). The fuselage (1) support is in the form of a lattice frame (5), with the cross-beam (2) forming part of the frame. Pref., the aircraft fuselage has a triangular configuration in side view and has a horizontal lower edge (6). Typically the fuselage frame extends into rear rudder supports (7). In plan view the fuselage has laterally tapering extensions (8) joined by wings (9), releasably bolted to the fuselage.