An active system and a computer-implemented method for reducing vibrations of seats in a vehicle is described. The system and method adjust a damping and/or a stiffness of a vibration damper based on system input signals from the vehicle or seat system. The signals include one or more of a signal associated with a user weight, a signal associated with time-dependent movement of a vehicle frame, and a signal associated with time-dependent movement of a seat back or a seat pan. The damping or the stiffness are adjusted by a closed loop control.

An adjustable swiveling passenger seat assembly is disclosed. The adjustable swiveling passenger seat assembly includes a set of base rails coupled to a floor. The adjustable swiveling passenger seat assembly further includes a plurality of pitch clevises coupled on a top surface of each of the set of base rails. The adjustable swiveling passenger seat assembly includes a swivel outer plate aligned in parallel relative to the floor. The swivel outer plate of the adjustable swiveling passenger seat assembly further includes a plurality of slots located on corners of the swivel outer plate and a plurality of spacers disposed within the plurality of slots.

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.

Described are passenger seats having a seat frame and a seat bottom slidingly and pivotally attached to the seat frame that, when the passenger seats are reclined, are configured to articulate forward from an upright configuration of the passenger seat to a second seat position corresponding to a reclined configuration of the passenger seat. The seat bottom can include an aft articulating mechanism that defines a declining first path in an aft-to-forward direction to cause the aft end of the seat bottom to drop when the seat bottom articulates forward; and a forward articulating mechanism connected with the seat bottom near a forward end of the seat bottom that defines a second path shaped to cause the forward end of the seat bottom to move upward when the seat bottom articulates forward, such that the seat bottom tilts aft in response to articulating forward when the passenger seat is reclined.

A system for both onboard piloting and remote piloting an aircraft having thereon at least one onboard pilot includes an aircraft having an onboard flight control system, onboard flight control devices, and onboard condition indicators mounted proximal the pilot seat. A remote flight control system, in electronic communication with the onboard flight control system, includes remote flight control devices and remote condition indicators. At least in a remote piloting mode, the onboard flight control system transmits flight and aircraft condition-related signals to the remote flight control system, receives flight control signals from the remote flight control system, and actuates, according to the flight control signals received from the remote flight control system, onboard actuators thereby remote piloting the aircraft. In the remote piloting mode, the aircraft may be cooperatively piloted by a remote pilot and at least one alert onboard pilot as another onboard pilot rests.

The invention relates to a seat, in particular for an aircraft, including: a seat support, a seat base, a backrest hinged relative to the seat base by means of a pivot link, a leg rest hinged relative to the seat base by means of a pivot link, the seat being able to move between a sitting position and a bed position in which the backrest and the leg rest are situated in a continuation of the seat base, the seat base being mounted so as to be able to slide relative to the seat support, the seat comprising at least one connecting rod, referred to as the backrest pivot connecting rod, comprising a first end connected in rotation relative to the backrest and a second end connected in rotation relative to the seat support, the leg rest being mechanically connected to the backrest by means of a connecting rod deployment device, the seat further comprising a single actuator capable alone of moving a set of components of the seat formed at least by the seat base, the backrest, and the leg rest in order to move the seat from its sitting position to its bed position and vice versa.

An aircraft passenger seat is proposed, having an enclosure and a base component of a backrest of the aircraft passenger seat, wherein the base component assumes an upright position during the use of the backrest. According to the invention, a securing device is provided for releasably securing the base component in the upright position, wherein a securing element of the securing device is adjustable from a securing position of the securing element on the securing device into a release position of the securing element, wherein, in order to lock the securing element in the securing position, a movable locking member of the securing device comes to bear against a latching contour on the securing element in such a manner that the securing element is locked in the securing position.

A passenger seat comprises a backrest, a seat element and a size increasing mechanism which is configured to convert a weight acting on the seat element when a user sits in the passenger seat into an increase in the depth of a seat pan of the seat element that can be used by the user from a rest-position depth to a to an operational-position depth.

A passenger seating assembly with an integrated cabin attendant seat (CAS) is disclosed. In embodiments, a CAS folds down from a monument mounted to the cabin floor via a combined track fitting that secures into the left-side or right-side track rail. A group of passenger seats (e.g., two to five) faces opposite the CAS monument and includes left-side and right-side leg assemblies mountable to the track rails via track fittings. One rear portion of a leg assembly attaches to the combined track fitting to integrate the passenger seats and CAS monument, eliminating unused space between the passenger seats and CAS monument.

A reversible seat assembly for use with an airplane. The reversible seat comprises a base assembly and a vertical assembly. The base assembly and the vertical assembly are connected to a support structure and are collectively disposable into and out of a first travel position, a second travel position, and a third travel position. In the first and second travel positions a user or passenger may assume a usual sitting position. In the third travel position the user may assume a reverse sitting position. The base assembly comprises a right segment and a left segment connected and rotationally movable to a central segment. The vertical assembly comprises a lower segment and an upper segment connected to and rotationally movable a middle segment. The reversible seat assembly may further comprise a back armrest connected to an opposite side of said middle segment and structure to provide support to the arms of the user.