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Patent Agency Ranking
公开(公告)号：DE3161298D1
公开(公告)日：1983-12-08
申请号：DE3161298
申请日：1981-02-03
Applicant: AEROSPATIALE
Abstract: The invention relates to aeronautics in general, and in particular to a suspension device for helicopter, comprising a flexible mounting plate at the center of which is fixed the bottom of the main gear box whose top is supported by hinged oblique bars. The mounting plate offers radial arms hinged to the base of the bars and to the fuselage of the helicopter. These arms bear flapping weights creating forces of inertia with reactions at the attachment points of direction opposite the elastic reactions of deformation of the mounting plate. A device of this type enables the vibrations on board helicopters to be reduced.
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公开(公告)号：FR2474996A1
公开(公告)日：1981-08-07
申请号：FR8002505
申请日：1980-02-05
Applicant: AEROSPATIALE
Inventor： MOUILLE RENE LOUIS , GENOUX GERARD CHARLES LOUIS , HEGE PIERRE ETIENNE
Abstract: The invention relates to aeronautics in general, and in particular to a suspension device for helicopter, comprising a flexible mounting plate at the center of which is fixed the bottom of the main gear box whose top is supported by hinged oblique bars. The mounting plate offers radial arms hinged to the base of the bars and to the fuselage of the helicopter. These arms bear flapping weights creating forces of inertia with reactions at the attachment points of direction opposite the elastic reactions of deformation of the mounting plate. A device of this type enables the vibrations on board helicopters to be reduced.
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公开(公告)号：FR2416838A1
公开(公告)日：1979-09-07
申请号：FR7803809
申请日：1978-02-10
Applicant: AEROSPATIALE
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公开(公告)号：FR2416839A1
公开(公告)日：1979-09-07
申请号：FR7803810
申请日：1978-02-10
Applicant: AEROSPATIALE
Inventor： MOUILLE RENE LOUIS , GENOUX GERARD CHARLES LOUIS , DECLERCQ MARC AUGUSTE , LEMAN JEAN-LUC MICHEL , SUZZI ROBERT JEAN
Abstract: The invention relates to a device for damping the vibrations of a rotary-wing aircraft rotor. An annular weight is disposed concentrically of the rotor axis. This weight is supported by at least three resiliently deformable elements such as helical springs, radially biased in directions distributed regularly around the rotor axis. The inner ends of the springs directly bear on a part extending the rotor shaft axially. Their outer ends directly bear on the annular weight so that the spring apply statically balanced centrifugal thrusts to the annular weight. The springs are so still that they support the annular weight without substantially bending.
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公开(公告)号：DE2903856A1
公开(公告)日：1979-08-16
申请号：DE2903856
申请日：1979-02-01
Applicant: AEROSPATIALE
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