Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes
Patent
1986-06-27
1988-01-19
Peters, Jr., Joseph F.
Aeronautics and astronautics
Aircraft, heavier-than-air
Helicopter or auto-rotating wing sustained, i.e., gyroplanes
248555, 248559, 416500, 188379, B64C 2704
Patent
active
047200600
ABSTRACT:
The device comprises four identical assemblies evenly spaced apart about the vertical axis of a speed reducer (1), offset 90.degree. from each other and each comprising an isotropic flexible beam (4) carrying a beating weight (14) and connected by its ends to the fuselage, this beam being perpendicular to the vertical axis, and rigid triangulation means (9, 10) connecting the speed reducer (1) to the beam (4) so as transmit its forces and its moments to the beam in a plane parallel to an offset from said vertical axis of the speed reducer (1).
REFERENCES:
patent: 3858831 (1975-01-01), Halwes
patent: 4405101 (1983-09-01), Carlson et al.
patent: 4431148 (1984-02-01), Mouille
patent: 4458862 (1984-07-01), Mouille et al.
Aerospatiale - Societe Nationale Industrielle
Corl Rodney
Peters Jr. Joseph F.
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