An aerial workstation which comprises a seat having a sitting portion, a backrest that is connected by a first articulation that allows the backrest to pivot relative to the sitting portion, and an arm configured to position the seat in various positions and orientations in space as required. The aerial workstation makes it possible to be able to translate the seat in a cockpit in an introduction direction, and to make it pivot about a pivot axis that coincides with the direction of introduction within the cockpit.

A seat, in particular an aircraft seat, having a seat support structure having at least one seat surface with a seat surface frame and a backrest with a backrest frame being pivotable relative to the seat surface, a base support element supporting the seat support structure, and a seat adjustment arrangement, which includes at least one coupling unit movable relative to the base support element, the coupling unit is configured to connect the seat surface frame and the backrest frame to one another and which is provided with at least one bearing element, and which includes at least one guide element in which the bearing element is movably guided. The seat adjustment arrangement being adapted to transfer the seat support structure into a sitting position, a comfort position or lying position by displacing the bearing element along the guide element.

An actuating drive, in particular for seat adjustment devices, comprising at least one electric motor, a downstream reduction gear, a coupling device which has a coupling engagement spring that ensures an engaged position of the coupling device during motorized operation and permits a manual disengagement against its coupling force. The coupling device has a coupling lever pivotably mounted in a pivot bearing of a bearing block. The coupling lever is connected at one end of the pivot bearing to a mechanical actuating unit and by which at the other end of the pivot bearing a coupling means can be adjusted to disengage the coupling device. The actuating drive ensures both reliable electrical and reliable manual operation, a high degree of efficiency during electrical operation and simple assembly for a generic actuating drive.

A seat is disclosed. The seat comprises a moveable seat carriage having a seat pan and a seat back supported thereon. The seat also comprises a seat base supporting the moveable seat carriage thereupon and a support member moveable between a retracted configuration and an extended configuration, wherein a first end of the support member is coupled to the moveable seat carriage and a second end of the support member is coupled to the seat base. The seat also comprises an actuator to move the moveable seat carriage relative to the seat base to thereby transition the seat between an upright and a reclined position, with the movement of the seat carriage driving the support member between the retracted configuration and the extended configuration, wherein the support member stiffens the seat as the seat transitions away from the upright to the reclined position and while in the reclined position.

A transformable seat assembly includes a seat support structure and a back support structure connected to the seat support structure with a hinge defining an axis of rotation. An actuator assembly includes a cylinder and a piston positioned within the cylinder, wherein the cylinder is secured to one of the back support structure or the seat support structure and the piston is secured to other of the one of the back support structure or the seat support structure. Additionally a blocking member is positioned within and adjustable along the cylinder. With blocking member in a first position, piston is limited to travel to a first limit position and the back support structure to a first reclined position. With the blocking member in a second position, piston is limited to travel to a second limit position and back support structure is permitted to rotate to second reclined position.

Systems, methods, and computer-readable media storing instructions for utilizing space associated with unoccupied seats in organized seating arrangements are disclosed herein. The disclosed techniques identify unoccupied seats within an organized seating arrangement, such as seats on an aircraft. Upgradable seats within the organized seating arrangement are determined based upon the unoccupied seats and the transformation capabilities of the seats. Upgradable seats are directly in front of or behind unoccupied seats, such that either the upgradable seat or the associated unoccupied seat is transformable to enable an upgrade. An occupant of a seat is selected for an upgrade associated with an upgradable seat and assigned the upgrade to enable the occupant to utilize a portion of the space associated with the unoccupied seat while sitting in the upgradable seat.

A transformable seat assembly which includes a seat support structure and a seat connected to the seat support structure with a hinge. The hinge defines an axis of rotation. A back support structure connected to the seat support structure, which extends in an upward direction relative to the seat support structure. A back cushion is secured to the back support structure and a lumbar cushion extends along the back support structure positioned between the back cushion and the seat, wherein the lumbar cushion is releasably secured to one of the back cushion or the back support structure and an end portion of the seat positioned closer to the back support structure with the seat positioned in an occupant support position than the hinge, can rotate in a direction of rotation about the axis of rotation, which includes the upward direction and a direction away from the back support structure.

This actuator comprises a frame, a motor, an output shaft, and a drive train for driving the output shaft via the motor. The drive train comprises an upstream element, a downstream element, and a device for coupling the upstream element to the downstream element. Said coupling device has a first configuration for transmitting all of the torque exerted by one of the upstream and downstream elements on the coupling device to the other of the upstream and downstream elements when said torque is below a threshold torque, and a second configuration for diverting at least part of said torque exerted by one of the upstream and downstream elements on the coupling device to the frame when said torque is at least equal to the threshold torque.

A seat base includes a plurality of linear actuators each having a first end pivotally mounted to a base member and a second end pivotally mounted to a seat member. A controller is adapted for controlling an extension length of each of the plurality of linear actuators in a coordinated manner for adjusting a position of the seat member with six degrees-of-freedom and for damping vibration of the seat member. An active vibration mitigation method for reducing vibrations of an aircraft seat includes receiving vibration data from one or more accelerometers mounted to the aircraft seat and determining a vibration profile based on the vibration data. When vibration mitigation is warranted, control signals for damping vibration are determined and transmitted to a plurality of linear actuators adapted to support the aircraft seat.

An aircraft seat device for an aircraft seat includes at least one mounting unit, having at least one seat bottom which is coupled with the mounting unit and is configured to implement a seating region and to this end has at least one main unit and at least one sub-unit that in relation to the mounting unit is implemented so as to be adjustable between a stowage position and a use position. The at least one adjustable sub-unit is configured for enlarging the seating region in at least one position, and having at least one actuation mechanism by means of which the adjustable sub-unit of the seat bottom is adjustable between its stowage position and its use position.