For travel on a cable, the zipline trolley includes a wheel, a brake, a frame, a hanger, and a lower slot. The wheel is disposed on a proximal end of a frame. The wheel includes a groove that receives a cable at a lower portion of the wheel and a wheel bearing. The brake is disposed on a distal end of the frame. The brake is connected to a given lever point and includes a groove along a brake bottom that receives the cable. The frame includes an array of lever points disposed between the brake and the wheel. The hanger is connected to a given lever point and suspends a weight. The weight applies a force about the wheel to the brake to control a rate of descent of the device along the cable. The lower slot receives the cable.

For travel on a cable, the zipline trolley includes a wheel, a brake, a frame, a hanger, and a lower slot. The wheel is disposed on a proximal end of a frame. The wheel includes a groove that receives a cable at a lower portion of the wheel and a wheel bearing. The brake is disposed on a distal end of the frame. The brake is connected to a given lever point and includes a groove along a brake bottom that receives the cable. The frame includes an array of lever points disposed between the brake and the wheel. The hanger is connected to a given lever point and suspends a weight. The weight applies a force about the wheel to the brake to control a rate of descent of the device along the cable. The lower slot receives the cable.

An inverted Stewart platform assembly includes a first platform having a first surface, a second platform having a second surface facing the first surface of the first platform, and six legs extending between and coupling the first platform and the second platform. The six legs are configured to be actuated between a first arrangement in which adjustable lengths of the six legs, measured from the first platform to the second platform, are substantially equal to one another, and a plurality of second arrangements in which the adjustable lengths of the six legs are not substantially equal to one another, wherein each leg of the six legs forms, in the first arrangement, an angle of less than or equal to 45 degrees with a plane defined by the first platform.

An inverted Stewart platform assembly includes a first platform having a first surface, a second platform having a second surface facing the first surface of the first platform, and six legs extending between and coupling the first platform and the second platform. The six legs are configured to be actuated between a first arrangement in which adjustable lengths of the six legs, measured from the first platform to the second platform, are substantially equal to one another, and a plurality of second arrangements in which the adjustable lengths of the six legs are not substantially equal to one another, wherein each leg of the six legs forms, in the first arrangement, an angle of less than or equal to 45 degrees with a plane defined by the first platform.

A trolley 100 for a rail 10 is described. The trolley 100 comprises a frame 110, a set S of wheels 120, including a first wheel 120A and a second wheel 120B, rotatably coupled to the frame 110 and an attachment member 130, coupled to the frame 110, for suspension of a load W therefrom, in use. The first wheel 120A is rotatable in a first plane P1 about a first axis A1 and the second wheel 120B is rotatable in a second plane P2 about a second axis A2. The first plane P1 and the second plane P2 define a line L. The trolley 100 is arrangeable in a first configuration, wherein the attachment member 130 is arranged at a first angular displacement D1 about the line L. The trolley 100 is arrangeable in a second configuration, wherein the attachment member 130 is arranged at a second angular displacement D2 about the line L, wherein the first angular displacement D1 and the second angular displacement D2 are different. A rail assembly 1, including the trolley 100 and the rail 10, is also described.

A flying simulator ride in accordance with present embodiments may include a suspended rotator ring capable of motion in six degrees of freedom. The flying simulator ride may also include a passenger support system suspended from the rotator ring wherein the passenger support system includes a first passenger support unit; and a second passenger support unit, wherein at least one of the first passenger support unit or the second passenger support unit are configured to move relative to one another to assume a stacked configuration and a loading configuration, wherein a distance between the rotator ring and the first passenger support unit is decreased in the stacked configuration relative to the loading configuration.

A flying simulator ride in accordance with present embodiments may include a suspended rotator ring capable of motion in six degrees of freedom. The flying simulator ride may also include a passenger support system suspended from the rotator ring wherein the passenger support system includes a first passenger support unit; and a second passenger support unit, wherein at least one of the first passenger support unit or the second passenger support unit are configured to move relative to one another to assume a stacked configuration and a loading configuration, wherein a distance between the rotator ring and the first passenger support unit is decreased in the stacked configuration relative to the loading configuration.

A cable in suspension (clear span) supports a trolley. At the upper end, a launch block fixed to the cable registers the trolley in all directions, including a safety release link holding the trolley near the launch block. After release and descent with a rider, the trolley strikes an attenuator of distributed springs and spacers. The spring stack absorbs momentum from the trolley, but a leash limits recoil bounce after reversing the trolley. A second, recoil, leash resists recoil by capturing a subset of the springs between respective ends of itself and the first leash. The doubly leashed trolley will oscillate to a stop in an equilibrium position.

A cable in suspension (clear span) supports a trolley. At the upper end, a launch block fixed to the cable registers the trolley in all directions, including a safety release link holding the trolley near the launch block. After release and descent with a rider, the trolley strikes an attenuator of distributed springs and spacers. The spring stack absorbs momentum from the trolley, but a leash limits recoil bounce after reversing the trolley. A second, recoil, leash resists recoil by capturing a subset of the springs between respective ends of itself and the first leash. The doubly leashed trolley will oscillate to a stop in an equilibrium position.

Described herein is an apparatus and method to convey an object through the air in a controlled and repeatable manner. The apparatus may comprise an object attached to at least one resilient member, the resilient member or members constraining object movement in a substantially vertical y-axis direction. The apparatus may also comprise at least one support member coupled to the at least one resilient member, and the support member or members constrain object movement in a substantially horizontal x-axis direction. In use, the resilient member is energised, movement initiated, and object movement then occurs in an x-axis and a y-axis direction, the movement path substantially governed by the resilient member(s) and the support member(s). The apparatus and method may allow the object to experience a variety of movement sensations, one being the feeling of flight or gliding.