Abstract:
A power starting dock for gyroscope is comprised of an outer housing that has a bottom and a concave head. The head is slanted at an angle relative to the housing, and engages a gyroscope rotor, an electric power source on the housing, a spring-mounted motor on the housing connected to the power source for producing a rotational power in response to a switching force, and a power rotor fastened to the motor and protruding into the concave head of the housing. The power rotor serves to resiliently transmit rotational motor power to the gyroscope rotor.
Abstract:
Structural elements (13, 16, 18) of an inertial sensor (10) are fabricated from molded plastic materials. The structural elements (13, 16, 18) are characterized by relatively, small cross-section areas, and further incorporate keys and keyways, as well as guide and alignment slots, (40, 42) molded into the elements (13, 16, 18) for coupling various structural elements.
Abstract:
Gyroscopes based on optomechanical designs to provide sensitive sensing while providing relatively large bandwidth and dynamic range with enhanced noise performance.
Abstract:
A power starting dock for gyroscope is comprised of an outer housing that has a bottom and a concave head. The head is slanted at an angle relative to the housing, and engages a gyroscope rotor, an electric power source on the housing, a spring-mounted motor on the housing connected to the power source for producing a rotational power in response to a switching force, and a power rotor fastened to the motor and protruding into the concave head of the housing. The power rotor serves to resiliently transmit rotational motor power to the gyroscope rotor.
Abstract:
A two-axis gyroscope in which precession may be effected by application of a DC current to the stationary precession windings (16). The rotor assembly (22) has a pair of ring-shaped permanent magnets (18, 20) with their magnetic vectors aligned parallel with the gyro spin axis. This structure presents a magnetic field to the precession windings (16) which does not change as the rotor assembly rotates. Thus the gyroscope may be precessed by application of a DC current to the precession windings. The precession windings are located along two orthogonal axes to allow precession of the gyro in two orthogonal directions.
Abstract:
A hydraulic machine includes an undercarriage; a rotating structure rotatably mounted on the undercarriage and configured to rotate with and with respect to the undercarriage; a first controller configured to receive user input and configured; a user interface configured to accept commands from a user and output a command signal to the controller; and a first gyroscope fixed to the rotating structure and electrically connected to the controller and configured to provide a data signal of rotation information of the rotating structure to the controller. An axis of rotation of the gyroscope is parallel to the axis of rotation of the rotating structure. The controller is configured to generate a control signal to control the rotating structure and cause the rotating structure to rotate with respect to the undercarriage based on the command signal from the user interface and the data signal from the first gyroscope.
Abstract:
A down hole surveying tool (10) for directional surveying of boreholes. The tool (10) comprises a body (11) which accommodates a two-axis gyroscope (13) and a two-axis accelerometer (15). The gyroscope (13) and accelerometer (15) are rigidly fixed with respect to each other to provide a composite sensor device (17). The sensor device (17) is supported in a rotary mount (31) for rotation about an indexing axis (4). The sensor device (17) can be indexed about the indexing axis between two indexing positions which are 180 degrees apart. An indexing mechanism (70) is provided for selectively indexing the sensor device (17) about the indexing axis (4). The indexing mechanism (70) comprises a drive portion (71) and a driven portion (72) adapted for selective interaction to impart indexing motion to the sensor device (17). The driven portion (72) is movable into and out of engagement with the drive portion (71) upon rotation of the rotary mount (31) about a pitch axis (1) using a pitch drive mechanism (51).
Abstract:
Techniques and devices for optical sensing of rotation based on measurements and sensing of optical polarization or changes in optical polarization in light waves in an optical loop due to rotation without using optical interferometry and a closed loop feedback in modulating the light in the optical loop.