Patent classifications
F16H3/34
Multi-speed gear box for a rotary wing aircraft
A gear system for a rotary wing aircraft includes a first gear including an inner gear portion having a first pitch and an outer gear portion having a second pitch that is distinct from the first pitch. A second gear includes a third pitch driven at a driving rotational speed. An actuator member is coupled to the second gear while driven at the driving rotational speed. The actuator member shifts the second gear along the first gear to engage with one of the inner gear portion and the outer gear portion to drive the first gear at a first rotational speed and engage with other one of the inner gear portion and the outer gear portion to drive the first gear at a second rotational speed. A controller is operable to control the actuator member to shift the second gear between the inner gear portion and the outer gear portion.
Multi-speed gear box for a rotary wing aircraft
A gear system for a rotary wing aircraft includes a first gear including an inner gear portion having a first pitch and an outer gear portion having a second pitch that is distinct from the first pitch. A second gear includes a third pitch driven at a driving rotational speed. An actuator member is coupled to the second gear while driven at the driving rotational speed. The actuator member shifts the second gear along the first gear to engage with one of the inner gear portion and the outer gear portion to drive the first gear at a first rotational speed and engage with other one of the inner gear portion and the outer gear portion to drive the first gear at a second rotational speed. A controller is operable to control the actuator member to shift the second gear between the inner gear portion and the outer gear portion.
Rotating direction change device for microtome
A rotating direction change device for a microtome includes: a first shaft arranged in a first fixed position; a first gear wheel non-rotatably mounted to the first shaft; a second shaft movable in a first direction; a second gear wheel non-rotatably mounted to the second shaft; a third shaft movable in a second direction; a third gear wheel non-rotatably mounted to the third shaft; and a first connection part connecting the second shaft and the third shaft such that the second gear wheel is constantly meshed with the third gear wheel, in which the second gear wheel can be driven by the first gear wheel directly or indirectly. Hence, the rotating direction change device has advantages of simple structure and low friction.
TOROIDAL CONTINUOUSLY VARIABLE TRANSMISSION AND DRIVE MECHANISM-INTEGRATED ELECTRICITY GENERATION APPARATUS FOR AIRCRAFT
Provided is a toroidal continuously variable transmission that can achieve suitable oil feed both for lubrication at contact interfaces between a power roller and discs and for cooling of the power roller; and a drive mechanism-integrated electricity generation apparatus for an aircraft, the electricity generation apparatus including the toroidal continuously variable transmission. The toroidal continuously variable transmission includes at least one lubrication outlet that discharges an oil toward at least one contact interface between an input or output disc and the power roller; and at least one cooling outlet that discharges the oil toward the power roller. The cooling outlet and the lubrication outlet are arranged such that a distance between the cooling outlet and a point at which the oil discharged from the cooling outlet contacts the power roller is smaller than a distance between the lubrication outlet and the contact interface.
TOROIDAL CONTINUOUSLY VARIABLE TRANSMISSION AND DRIVE MECHANISM-INTEGRATED ELECTRICITY GENERATION APPARATUS FOR AIRCRAFT
Provided is a toroidal continuously variable transmission that can achieve suitable oil feed both for lubrication at contact interfaces between a power roller and discs and for cooling of the power roller; and a drive mechanism-integrated electricity generation apparatus for an aircraft, the electricity generation apparatus including the toroidal continuously variable transmission. The toroidal continuously variable transmission includes at least one lubrication outlet that discharges an oil toward at least one contact interface between an input or output disc and the power roller; and at least one cooling outlet that discharges the oil toward the power roller. The cooling outlet and the lubrication outlet are arranged such that a distance between the cooling outlet and a point at which the oil discharged from the cooling outlet contacts the power roller is smaller than a distance between the lubrication outlet and the contact interface.
Gear transmission device and image forming apparatus
A gear transmission device includes a frame, a sun gear including a first shaft having a first axis, a driven gear, a planet gear movable between an engaged position and a disengaged position and including a second shaft having a second axis, an auxiliary gear including a third shaft, a first guide portion to guide the second shaft, and a second guide portion to guide the third shaft. At least a portion of the third shaft is positioned opposite to the driven gear relative to a first imaginary line passing the first axis and the second axis of the planet gear located at the disengaged position. As the sun gear rotates with the auxiliary gear in mesh with the planet gear, the third shaft moves with contacting a guide surface and the second shaft moves in a direction opposite to a direction in which the third shaft moves.
Gear transmission device and image forming apparatus
A gear transmission device includes a frame, a sun gear, a driven gear, a planetary gear, a contact member, and a guide. The guide guides the contact member as described below. When the planetary gear is at a meshing position, a first tooth portion and a first contact portion of the contact member are away from the planetary gear. When the planetary gear is at a farthest position, the first contact portion is in contact with the planetary gear and the first tooth portion is away from the planetary gear. When the planetary gear is between the meshing position and the farthest position, the first tooth portion moves in mesh with the planetary gear in a direction opposite to a moving direction of the planetary gear around the sun gear, and the first contact portion is switched between a state in contact with the planetary gear and a state away from the planetary gear.
Automatic pool cleaner gear mechanism
A gear change and gear change biasing mechanism for use in an automatic swimming pool cleaner.
Automatic pool cleaner gear mechanism
A gear change and gear change biasing mechanism for use in an automatic swimming pool cleaner.
Reversing mechanism for irrigation sprinkler with disengaging gears
An irrigation sprinkler can include a reversing mechanism configured to transition the nozzle turret of the irrigation sprinkler between a forward direction of rotation and a reverse direction of rotation. The reversing mechanism can include shifting frame having an input gear and at least one output gear. The at least one output gear can be mounted on an axle of rotation which permits lateral movement of the at least one output gear between a power transmitting position, wherein rotational power from a gear reduction is transferred to the nozzle turret, and a disengaged position wherein rotational power from the gear reduction is not transferred to the nozzle turret.