Rigid coaxial rotor helicopter with dual auxiliary propulsion

Transportation – Aircraft – spacecraft – or fuselage – Vertical takeoff type

Design Patent

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Design Patent

active

D0524718

CLAIM:
The ornamental design for a rigid coaxial rotor helicopter with dual auxiliary propulsion, as shown and described.

REFERENCES:
patent: D357894 (1995-05-01), Arnold et al.
patent: D361053 (1995-08-01), Whyte et al.
patent: D363054 (1995-10-01), Taylor et al.
patent: D375077 (1996-10-01), Taylor et al.
patent: D388048 (1997-12-01), Taylor et al.
patent: D425853 (2000-05-01), Caporaletti

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