33results about How to "Effective transmission torque" patented technology

An apparatus for use in a cylinder machine having a shoe with a concavely-shaped pressure surface that forms a substantially mating relationship with a cylinder mould or sieve. The concavely-shaped pressure surface of the shoe increases the amount of wrap that a making fabric has on a cylinder mould or sieve thereby increasing the amount of friction generated between the making fabric and the cylinder mould or sieve. The increased friction results in an improved torque transfer between the making fabric and the cylinder mould or sieve.

A drive clutch having a compressible torque transfer mechanism configured to transfer torque from an engine or motor to a moveable sheave and configured to reduce wear on components of the drive clutch by eliminating sliding contact between surfaces to transfer torque and change the gear ratio. The torque transfer mechanism increases efficiency and reduces wear and may comprise a torque bellows, which is configured to transfer torque from the engine to the moveable sheave upon radial compression of the torque bellows. Sliding blocks and corresponding slide tracks are concentrically positioned between the moveable sheave and the shift plate and centrifugal force provides a force for linear movement for the sliding blocks, which results in movement of the moveable sheave and the cover, which can act to compress the torque bellows. This configuration reduces costs because precise machining is not needed and reduces premature wear and tear on the drive clutch.

A torque transmission system is provided for an aircraft drive wheel drive system mounted on nose or main landing gear wheels to move the aircraft autonomously on the ground that effectively transmits torque through drive system components. The drive system includes a drive means capable of generating sufficient torque to move the aircraft, a drive system capable of generating a high torque capacity that activates the drive means, a clutch assembly that can be selectively engaged to control torque transmission to the drive system and activate the drive means, and a landing gear torque takeout element. The clutch assembly is configured to be inactivated and prevented from transmitting torque to other drive wheel drive system components when an overtorque event occurs. Aircraft drive wheel drive system components in the present torque transmission system are designed to withstand torque in excess of a determined maximum for the system.

The invention relates to a main gearbox assembly of a single-screw extruder and application of the main gearbox assembly. The main gearbox assembly comprises a main gearbox and a thrust screw, wherein the main gearbox is a hollow output shaft, an internal spline is arranged at the tail end of the main gearbox, and two locating holes are formed in the tail end at the same time; a thrust spiral is arranged at the front part of the thrust screw, a locating neck is arranged at the rear part, an external spline and bulged shaft necks are arranged on the locating neck, the diameters of the bulged shaft necks are larger than that of the thrust spiral, and smaller than that of the external spline at the tail end; the hollow output shaft is equipped with an adjusting pad and a rear pressing cover on the surface of the tail end, and equipped with an external gear sleeve at the front end, the external gear sleeve is provided with an internal hole, and the diameter of the internal hole in the external gear sleeve is larger than that of the thrust spiral; after the thrust spiral at the front end of the thrust screw penetrates the inner hole in the external gear sleeve, the bulged shaft necks are placed in the locating holes of the hollow output shaft, and the external spline is engaged with the internal spline; a rotation joint penetrates the rear pressing cover and the adjusting pad, and is connected with the thrust screw and communicated with a circulating water channel in the thrust screw. During use, a rubber extruding unit is equipped with at least one material conveyor containing the gearbox assembly of the single-screw extruder.

The invention discloses a drive axle gearbox wheel set for large railway maintenance machinery. The drive axle gearbox wheel set comprises an axle, two wheels, a sliding bearing, a locking steel ball, an inner sleeve, an outer sleeve, a rolling steel ball, an axle retainer ring, a hole retainer ring, a spring and an end cover. The two wheels are positioned on wheel seats at two ends of the axle respectively. The locking steel balls, spherical grooves, a radial cylindrical hole of the inner sleeve and the outer sleeve form a locking mechanism; the rolling steel balls, first semicircular grooves and second semicircular grooves are matched to form a rolling ball key mechanism; the end cover is fixed to the end face of one side, away from the wheels, of the outer sleeve, a gap is reserved between the end cover and the circumference of the inner sleeve, the end cover is capable of axially moving left and right along the inner sleeve, and the springs are mounted in a closed annular inner cavity formed by the outer sleeve, the end cover and the inner sleeve. The drive axle gearbox wheel set for large railway maintenance machinery is simple in structure, convenient to operate and capable of fitting different rail gauges.

The invention provides a connection structure and a connection system, the connection structure includes a first connection body, which is provided with a connection through hole and a limiting through hole; a second connection body, which is provided with a tapered hole, a tapered hole, a limiting through hole Bit through holes and connecting through holes are distributed sequentially; tapered studs pass through the tapered holes, limiting through holes and connecting through holes, and the tapered studs have a first cylindrical part, a tapered part and a second connected in sequence. Cylindrical part; a conical fitting structure arranged in the limiting through hole, the conical fitting structure is provided with a first conical surface matched with the tapered part, and a limiting cylindrical surface matched with the inner wall of the limiting through hole; The tapered nut screwed on the first cylindrical part, the tapered nut is provided with a second tapered surface matching the tapered hole; the set nut screwed on the second cylindrical part, the set nut and the first connecting body The end surface facing away from the second connecting body abuts. Through the present invention, the technical problem that it is difficult to effectively transmit the vibration load to the aircraft or its sections in the vibration test of the large aircraft is alleviated.

A constant velocity joint includes: an outer joint member having a raceway groove; an inner joint member having a leg shaft; a roller that is able to roll on the raceway groove; and a needle bearing that supports an inner periphery of the roller such that the inner periphery of the roller is able to rotate with respect to the leg shaft. The leg shaft includes: a roll portion that supports the needle bearing; a contact portion that is able to contact an end face of the needle bearing, the end face facing a first side in the direction of a central axis of the needle bearing; and a recess portion formed between the roll portion and the contact portion, in a position where the recess portion is recessed from a space in which the needle bearing is disposed.