AIRCRAFT SYSTEM FOR REDUCED OBSERVER VISIBILITY

AIRCRAFT SYSTEM FOR REDUCED OBSERVER VISIBILITY

An aircraft apparatus is disclosed that has a fuselage boom (102) having proximal (110) and distal (103) ends, a wing (108) coupled to a proximal end (110) of the fuselage boom (102) and at least one transparent stabilizer (104, 106) coupled to a distal end (103) of the fuselage boom (102). L'i...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: FISHER, CHRISTOPHER, BELIK, PAVIL, GUNDER, AUSTIN, ZWAAN, JOHN PETER, CHAMBERS, STEVEN
Format: Patent
Sprache:eng ; fre
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:An aircraft apparatus is disclosed that has a fuselage boom (102) having proximal (110) and distal (103) ends, a wing (108) coupled to a proximal end (110) of the fuselage boom (102) and at least one transparent stabilizer (104, 106) coupled to a distal end (103) of the fuselage boom (102). L'invention porte sur un appareil d'aéronef, lequel appareil a une flèche de fuselage (102) ayant des extrémités proximale (110) et distale (103), une aile (108) couplée à une extrémité proximale (110) de la flèche de fuselage (102) et au moins un stabilisateur transparent (104, 106) couplé à une extrémité distale (103) de la flèche de fuselage (102).