Control rod device
AssigneeZF Friedrichshafen AG
InventorsUwe Arnold, Matthias Muller, Jeurgen Goette
Life of this patent
Estimating the term…
Loading patent…
AssigneeZF Friedrichshafen AG
InventorsUwe Arnold, Matthias Muller, Jeurgen Goette
Estimating the term…
A control rod configuration for adjusting a position of a rotor blade of a helicopter. The control rod configuration includes a control rod which has a bearing eye, adjacent the swash plate, which is penetrated by an axle shaft which has a bearing supported by a bearing bracket. The control rod configuration, which can be simply constructed and is less susceptible to malfunction, has an eccentric with its pivotable bearing in the bearing bracket and which is provided between the bearing bracket and the bearing eye. In addition, a method in which a rotor blade of a helicopter has an assigned control rod which is supported by an axle shaft with a bearing in the bearing bracket which is mounted to the swash plate so as to enable adjustment of the control rod by pivoting the axle shaft during flight.
A control rod configuration, for adjusting a rotor blade of a helicopter, comprising:
A method of adjusting a control rod (12) which is connected to a rotor blade of a helicopter, the control rod (12) being supported by an axle body (5), and the axle body (5) being rotatably supported by a bearing in a bearing bracket (2) mounted to a swash plate (1), an eccentric (8), which is pivotable in the bearing bracket (2), being arranged between the bearing bracket (2) and a swash plate side bearing eye (11), the eccentric having a central axis that is offset from a rotational axis of the axle body (5) and is coaxial with a longitudinal axis of the swash plate bearing eye (11) of the control rod, the method comprising:
A control rod configuration, for adjusting a rotor blade with respect to a swash plate of a helicopter, the control rod configuration comprising:
Dependencies are inferred from the claim text.