Device for damping oscillations

A device for damping mechanical oscillations, in a helicopter transmission test system which includes:

• a programming device setting the desired sequence of test conditions for said helicopter transmission and having several inputs and outputs:
• a first integrator whose input is connected to the first output of said programming device;
• a second integrator whose input is connected to the second output of said programming device;
• a controlled drive incorporating:
• a speed governor whose input is connected to the output of said first integrator;
• a first current regulator whose input is connected to said speed governor;
• a voltage source whose input is connected to the output of said current regulator;
• a d-c motor whose armature is electrically coupled to the output of said voltage source;
• a speed transducer arranged on the shaft of said d-c motor and connected via its output to the input of said speed governor;
• a current generator placed in the armature supply circuit of the motor and connected via its output to the input of said first current regulator;
• a control unit whose input is connected to the third output of said programming device;
• a first exciter, the input of which is connected to the output of said control unit and whose output is electrically coupled to the field winding of said motor;
• a first exciting current generator of said motor placed in the field winding circuit of said motor and connected via its output to the input of said control unit;
• a loading moment regulator whose input is connected to the output of said second integrator;
• a second current regulator whose input is connected to the output of said loading moment regulator;
• an exciting current regulator whose input is connected to the output of said second current regulator;
• a synchronous motor whose shaft is rigidly coupled to the shaft of said d-c motor;
• an actuator loading said helicopter transmission and comprising a synchronous generator, the stator windings of which are connected to the stator windings of said synchronous motor and whose field winding is connected in series with the field winding of said synchronous motor;
• a second exciter of said synchronous generator and motor, the input of which is connected to the output of said exciting current regulator and whose output is coupled to a circuit incorporating:
• two series-connected field windings of said synchronous motor and said synchronous generator;
• a flexible member formed with said helicopter transmission under test, one end of which is mechanically coupled to the shaft of said synchronous motor and the other end to the shaft of said synchronous generator;
• a moment transducer arranged on said transmission under test and connected via its output to the input of said loading moment regulator;
• a second current generator placed in the stator circuit of said synchronous generator and connected via its output to the input of the second current regulator;
• a corrective assembly damping oscillations within said system and incorporating;
• a fundamental-frequency sine-wave signal generation unit whose input is connected to the output of said moment transducer;
• a differentiating unit whose input is connected to the output of said fundamental-frequence sine-wave signal generation unit;
• a net time lag tuning unit whose input is connected to the output of said differentiating unit;
• an amplitude tuning unit, the input of which is connected to the output of said net time lag tuning unit and whose output is connected at the same time to said exciting current regulator of said synchronous machines, to the input of the first current regulator and to the input of said control unit.

A device for damping mechanical oscillations, in a mill roll control system comprising:

• a controller used to control said system and having several inputs and outputs;
• a controlled drive incorporating:
• an integrator whose input is connected to one output of said controller;
• a speed governor whose input is connected to the output of said integrator;
• a current regulator whose input is connected to the output of said speed regulator;
• a regulated voltage source whose input is connected to the output of said current regulator;
• a d-c motor whose armature is connected to the output of said regulated voltage source;
• a speed transducer mechanically coupled to the shaft of said motor and connected via its output to the input of said speed governor;
• first and second current generators of said motor placed in the armature circuit of said motor, the output of the first current generator being connected to the input of said current regulator;
• an e.m.f. transducer of said motor connected via the inputs thereof to said regulated voltage source and to the output of said second current generator;
• an e.m.f. regulator whose input is connected at the same time to the second output of said controller and to the output of said e.m.f. transducer;
• an exciting current regulator whose input is connected to the output of said e.m.f. regulator;
• an exciter of said motor, the input of which is connected to the output of said exciting current regulator and whose output is connected to the field winding of said motor;
• an exciting current generator place in the field winding circuit of said motor and connected via its output to the input of said exciting current regulator;
• a flexible member comprising the shaft of said mill
• a moment transducer arranged on said shaft;
• an actuator comprising rolls of said mill, mechanically coupled to the shaft of said motor through said shaft of said mill;
• a primary element comprising a d-c machine, the shaft of which is rigidly coupled to the rolls of said mill and whose armature is connected to the armature of said motor;
• a current generator of said primary element placed in the armature circuit of said d-c machine;
• a primary element current regulator whose input is connected to the third output of said controller and to the output of said primary element current generator;
• an exciting current regulator of said primary element, the input of which is connected to the output of said current regulator of the primary element;
• a primary element exciter, the input of which is connected to the output of said exciting current regulator and whose output is placed in the field winding circuit of said primary element;
• an exciting current generator of said primary element, placed in the field winding circuit of said primary element and connected via its output to the input of said exciting current regulator of the primary element;
• a signal frequency separation unit discriminating fundamental-frequency signals for the given system and connected to the output of said moment transducer;
• corrective assemblies whose number corresponds to the number of fundamental frequencies, each assembly comprising a channel and having an individual differentiating unit whose input is connected to the output of said signal frequency separation unit;
• an individual net time lag tuning unit whose input is connected to the output of said individual differentiating unit;
• an individual amplitude tuning unit whose input is connected to the output of the net time lag tuning unit;
• a unit adding up signals of all channels, the input of which is connected to the output of the amplitude tuning units of all said channels and whose output is connected to the input of said exciting current regulator of the motor, to the input of said motor current generator and to the input of said exciting current regulator of the primary element.

A device for damping mechanical oscillations used in an extensive multimember helicopter transmission test system which comprises:

• a multiconnection helicopter transmission incorporating:
• a main reduction gear;
• a first moment transducer arranged on a first shaft;
• a first flexible member formed with a first input shaft with a free-wheeling clutch mounted thereon, said shaft being coupled to the first moment transducer arranged on said first shaft;
• a second flexible member formed with a second input shaft having a free-wheeling clutch arranged thereon, said shaft being mechanically coupled to the first shaft and the main reduction gear;
• a second moment transducer arranged on said second shaft;
• a third flexible member comprising a helicopter steering rotor shaft, which is mechanically coupled to said first and second shafts through said main reduction gear;
• a moment transducer mounted on said steering rotor shaft;
• a fourth flexible member comprising a helicopter main rotor shaft, which is mechanically coupled to said first, second and third shafts of said main reduction gear;
• a moment transducer mounted on said main rotor shaft;
• a programming device comprising a computer, setting the desired sequence of test conditions for the helicopter transmission and having several inputs and outputs;
• a first integrator converting an intermittent input signal into a signal linearly changing with time and connected via its input to the first output of said programming device;
• a second integrator connected to the second output of said programming device;
• a third integrator connected to the third output of said programming device;
• a fourth integrator connected to the fourth output of said programming device;
• a fifth integrator connected to the fifth output of said programming device;
• a controlled drive of said first flexible member including a first mains transformer;
• a first controlled rectifier connected via its power input to said first mains transformer;
• a first converter connected via its input to said first controlled rectifier;
• a first induction motor connected to said first converter;
• a speed governor mounted on the shaft of said first induction motor;
• a current generator placed in the output circuit of the first controlled rectifier;
• a speed governor of said first motor whose input is connected to the output of said first integrator and to the output of said speed governor of first induction motor;
• a current regulator of said first induction motor connected via its input to the output of said speed governor and to the output of said current generator and via its output to a control input of said first controlled rectifier;
• a controlled drive of said second flexible member including a second mains transformer;
• a second controlled rectifier connected via its power input to said second mains transformer;
• a second converter connected via its input to said second controlled rectifier;
• a second induction motor connected to said second converter;
• a second transducer mounted on the shaft of said second induction motor;
• a current generator placed in the output circuit of the second controlled rectifier;
• a speed governor of said second motor, the input of which is connected to the output of said second integrator and to the output of said speed transducer of said second induction motor;
• a current regulator of said second induction motor connected via its input to the output of said speed regulator and to the output of said current generator and via its output to the input of said first controlled rectifier;
• an actuator including a first synchronous generator whose shaft is mechanically coupled to the steering rotor shaft;
• a third rectifier whose power input is connected to the output of said first synchronous generator;
• an inverter whose input is connected to the output of said third rectifier;
• a third mains transformer connected via its input to said inverter;
• a second synchronous generator whose shaft is mechanically coupled to the main rotor shaft;
• a first transformer whose input is connected to said second synchronous generator;
• a fourth recitifer, the input of which is connected to said first transformer and whose output is placed in the circuit of the second controlled rectifier and the second converter;
• a second transformer whose input is connected to said synchronous generator;
• a fifth rectifier, the input of which is connected to the second transformer and whose output is placed in the circuit of the first controlled rectifier and the first converter;
• a e.m.f. setter and current limiter the input of which is connected to the output of said fifth integrator and whose output is connected to the control input of said inverter;
• a moment transducer mounted on the steering rotor shaft;
• a moment transducer mounted on the main rotor shaft;
• a moment regulator connected via its input to the output of said third integrator and to the output of said moment transducer mounted on the steering rotor shaft;
• an exciting current regulator of said first synchronous generator connected via its input to the output of said moment regulator;
• an exciter, the input of which is connected to the output of said exciting current regulator and whose output is placed in the field winding circuit of said first synchronous generator;
• an exciting current generator placed in the field winding circuit of said first synchronous generator and connected via its output to the input of said exciting current regulator of the first synchronous generator;
• a moment regulator of the second synchronous generator whose input is connected to the output of said fourth integrator and to the output of said moment transducer mounted on the main rotor shaft;
• an exciting current regulator of the second synchronous generator whose input is connected to the output of said moment regulator of the second generator;
• an exciter of said second generator connected via its input to said exciting current regulator and placed via the output thereof in the field winding circuit of said second synchronous generator;
• an exciting current generator of said second generator placed via its input in the field winding circuit of said generator and connected via the output thereof to the input of said exciting current regulator of said second generator;
• a corrective assembly of said controlled drive of said first flexible member of the helicopter transmission, the input of which is connected to the moment transducer mounted on the first input shaft and whose output is connected to the input of said current regulator of the first induction motor;
• a corrective assembly of said controlled drive of the second input shaft of the helicopter transmission, the input of which is connected to said moment transducer arranged on the second input shaft and whose output is connected to the input of said current regulator of the second induction motor;
• a corrective assembly of said first synchronous generator, the input of which is connected to the output of the moment transducer arranged on the steering rotor shaft and whose output is connected to the input of said exciting current regulator of the first synchronous generator;
• a corrective assembly of said synchronous generator, the input of which is connected to the output of the moment transducer arranged on the main rotor shaft and whose output is connected to the input of said exciting current regulator of the second synchronous generator.