A universal joint (U-joint) assembly transmits torque from a drive component to a driven component across an articulating joint. The U-joint assembly includes male and female U-joint members, a central ball joint, and a retaining device configured to secure the assembly in an assembled configuration. The female U-joint member includes a cavity extending into a receptacle end thereof. The cavity terminates in a circular receptacle and includes a plurality of rectangular channels extending radially outward from the cavity at equal intervals, each channel defined by three planar drive surfaces. The male U-joint member has a drive end with a plurality of corresponding rectangular extensions protruding from an outer periphery of the drive end, each extension including a plurality of axial angular surfaces. When assembled, each of the angular surfaces of the drive end opposes a corresponding one of the drive surfaces of the cavity. Other embodiments are also disclosed.

In a joint (100) for a structure that includes at least one rod (104) and a plurality of cables (102), each cable (102) having an outside diameter, a rod end (160) is affixable to the rod (104) so that the rod has a rod (104) centerline that passes through the rod end (160). The rod end (160) includes a mechanism (166) that allows the rod end (160) to pivot about a center point that is on the rod centerline. A cable attachment device (150) is couplable to each cable (102) and to the rod end (160). The cable attachment device (150) holds each cable (102) coupled thereto in a relationship to the rod end (160) so that each cable (102) has a cable centerline that intersects the center point so as to minimize any moments from the rod (104) or the cables (102) on the joint (100).

In a joint (100) for a structure that includes at least one rod (104) and a plurality of cables (102), each cable (102) having an outside diameter, a rod end (160) is affixable to the rod (104) so that the rod has a rod (104) centerline that passes through the rod end (160). The rod end (160) includes a mechanism (166) that allows the rod end (160) to pivot about a center point that is on the rod centerline. A cable attachment device (150) is couplable to each cable (102) and to the rod end (160). The cable attachment device (150) holds each cable (102) coupled thereto in a relationship to the rod end (160) so that each cable (102) has a cable centerline that intersects the center point so as to minimize any moments from the rod (104) or the cables (102) on the joint (100).

Modular tracker systems that include at least first and second tables or are continuous without the use of tables, a single motor driving the first and second tables, first and second intra-table drive shafts and an inter-table drive shaft. Each table includes a support structure including first and second mounting posts, a frame supported by the support structure, at least one solar panel supported by the frame, and first and second gearboxes being concentrically aligned for each table. The first and second gearboxes are each configured to produce first and second outputs. The first output has a first rotational speed, and the second output has a second rotational speed less than the first rotational speed, and is operatively coupled to the frame. The inter-table drive shaft couples the second gearbox of the first table with the first gearbox of the second table, whereby the first and second tables are rotated synchronously.

A gas turbine engine for an aircraft includes an engine core with a turbine, a compressor, and a core shaft connecting the turbine and compressor; a fan upstream of the engine core including a plurality of fan blades; and a gearbox that receives an input from a gearbox input shaft portion of the core shaft and outputs drive to a fan shaft so as to drive the fan at a lower rotational speed than the core shaft, the gearbox being an epicyclic gearbox including a sun gear, a plurality of planet gears, a ring gear, and a planet carrier arranged to have the plurality of planet gears mounted thereon, and wherein the sun gear receives input from the core shaft. At cruise conditions the torque on the core shaft is greater than 10,000 Nm and a ratio of core shaft stiffness to core shaft torque is within a specified range.

A flexible driveshaft includes a proximal coupler and a distal coupler each configured to couple to a respective component of an instrument, and a flexible shaft having a proximal end connected to the proximal coupler, a distal end connected to the distal coupler, and a longitudinal axis. The flexible shaft may include a sleeve, and a core having a first end and a second end. The core is housed within the sleeve. The flexible shaft also includes a plurality of coils arranged around the longitudinal axis in at least one layer.

A flexible driveshaft includes a proximal coupler and a distal coupler each configured to couple to a respective component of an instrument, and a flexible shaft having a proximal end connected to the proximal coupler, a distal end connected to the distal coupler, and a longitudinal axis. The flexible shaft may include a sleeve, and a core having a first end and a second end. The core is housed within the sleeve. The flexible shaft also includes a plurality of coils arranged around the longitudinal axis in at least one layer.

A torsion bar includes a central portion extending in an axial direction about a longitudinal axis. The torsion bar also includes a first end portion having a splined outer surface, the first end portion disposed proximate a first end of the torsion bar, the first end portion spaced from the central portion with a first annular groove extending circumferentially about the torsion bar.

A torsion bar includes a central portion extending in an axial direction about a longitudinal axis. The torsion bar also includes a first end portion having a splined outer surface, the first end portion disposed proximate a first end of the torsion bar, the first end portion spaced from the central portion with a first annular groove extending circumferentially about the torsion bar.

A fixture pin assembly for presenting a pin in a specified location and orientation to provide positioning or dimensional verification for a target part. The fixture pin assembly comprises a block, a pin, and an actuator set. The block includes a plurality of holes on a plurality of surfaces to attach directly or indirectly to mating bushings, pins, and actuation component sets. Pin and bushing act in combination to present a pin which is fixed or may allow motion in specified directions. Actuation component set provides motion control of the pin to either fix the location in longitudinal direction or allow longitudinal motion with or without springs to impart force either rearward or forward. A cable actuation system provides for remote release functionality of pin. Entire system design is configurable and interchangeable to provide cost-effective and space-effective implementation.