Hybrid helicopter that is fast and has long range

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane and helicopter sustained

Reexamination Certificate

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Details

C244S00700B, C244S00700B, C244S04500R, C244S017110

Reexamination Certificate

active

08070089

ABSTRACT:
A hybrid helicopter (1) includes a central fuselage (2) defining a front end (3) and a rear end (4), the hybrid helicopter (1) having a main lift rotor (10), an additional lift surface (20), a mechanical interconnection system (40), and at least one turbine engine (61, 62) for continuously driving the main rotor (10) in rotation. Furthermore, the main rotor (10) is mechanically connected to the mechanical interconnection system (40) by rotary rotor mast (12), and the additional lift surface (20) is arranged at the rear of the hybrid helicopter (1) between the rotor mast (12) and the rear end (4) of the fuselage (2), each end zone (21′, 22′) of the wings (21, 22) of the additional lift surface (20) being provided with a vertical element (23, 24) fitted with a rudder (23′, 24′).

REFERENCES:
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patent: 3426982 (1969-02-01), Markwood
patent: 3540680 (1970-11-01), Peterson
patent: 3698666 (1972-10-01), Monti
patent: 3954231 (1976-05-01), Fraser
patent: 5454530 (1995-10-01), Rutherford et al.
patent: 5454531 (1995-10-01), Melkuti
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patent: 6471158 (2002-10-01), Davis
patent: 6561456 (2003-05-01), Devine
patent: 6974106 (2005-12-01), Churchman
patent: 7267300 (2007-09-01), Heath et al.
patent: 2002/0011539 (2002-01-01), Carter, Jr.
patent: 2007/0170307 (2007-07-01), de la Cierva Hoces
patent: 1078557 (2002-01-01), None
patent: 1978277 (2007-06-01), None
patent: 20303024 (2003-08-01), None
patent: 2007014531 (2007-02-01), None
French search report in corresponding FR 0801613.

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