LIGHTER-THAN-AIR AIRCRAFT

LIGHTER-THAN-AIR AIRCRAFT

The present invention relates to a lighter-than-air aircraft (100), comprising: a hull (101); a gondola (102) mounted at the bottom of the hull (101) as a control station; at least two pairs of thrusters (103) mounted on the opposite side of the longitudinal axis of the hull (101); wherein each pair...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: AHMAD SALAHUDDIN BIN MOHD HARITHUDDIN, MOHD FAZRI BIN SEDAN, MOHD AZIZI BIN AB. MALEK
Format: Patent
Sprache:eng
Schlagworte:
AIRCRAFT
AVIATION
COSMONAUTICS
LIGHTER-THAN AIR AIRCRAFT
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The present invention relates to a lighter-than-air aircraft (100), comprising: a hull (101); a gondola (102) mounted at the bottom of the hull (101) as a control station; at least two pairs of thrusters (103) mounted on the opposite side of the longitudinal axis of the hull (101); wherein each pair of the thrusters (103) disposed each other in front and back; each of the thruster (103) being connected to the hull (101) with a thruster supporting means (104) and a tripod legs (105); characterized in that: a front pair thrusters (103a and 103c) are faced forward and a back pair thrusters (103b and 103d) are faced backward during forward flight and yawing motion; wherein each of the thruster (103) tilt-able to 90? from substantially horizontal axis to vertical axis. (Fig. 1)