This invention, the Motor-wing Gimbal Aircraft (MGA) is an aerial vehicle and waterborne craft. It launches and lands vertically from the ground and water. In flight, it transitions from vertical, hovering and forward flight to horizontal flight. The MGA embodies multiple configurations and arrangements of motor-wings, propulsion systems and hybrid engine combinations. The MGA uses a fly-by-light system for flight maneuvering and controlling the motorized multi-axis gimbal cockpit. The MGA uses cellular communications together with the Global Positioning System (GPS) for navigation, collision avoidance and restricted airspace avoidance. The MGA uses visible lights to signal its elevation and flight maneuvers. The MGA is constructed of modular apparatuses and assemblies that are interchangeable and work in concert to power and maneuver the vehicle. This invention includes: the method of construction, the method of control, the method of visual light signaling, the method of electronic mapping of airspace (EMA) and the method of navigation. This invention includes flight operation applications and military applications.

A seat fixing device for fixing a vehicle seat, in particular an aircraft passenger seat, to at least one fixing rail that is attached to a vehicle structure, comprising a fixing means that is to be coupled to the at least one fixing rail, and comprising a force transmitting unit that is used in a normal olperating mode to provide a first force application path of a weight and acceleration force that is introduced into the vehicle structure via the vehicle seat. The force transmitting unit has a transmitting means that is used in an impact mode to at least initiate a generation of at least one second force application path of the weight and acceleration force that is introduced into the vehicle structure via the vehicle seat.

A base assembly for an aircraft seat is disclosed. The base assembly may include one or more leg sub-assemblies. Each leg sub-assembly may include a front leg, a rear leg, and a link beam configured to couple the front leg to a portion of the rear leg. At least one of the front leg or the rear leg being at least partially formed of a hybrid composite structure. The link beam being at least partially formed of the hybrid composite structure. The hybrid composite structure formed of at least a first material and a second material, where the first material is different from the second material, the first material including a thermoplastic material configured to provide ductility for the base assembly, the second material being a composite material configured to provide strength for the base assembly.

In a method for producing a rail-shaped hybrid component, in particular for an aircraft or spacecraft, a second rail component made of a titanium material is positioned on a first bar of a first profile rail that is made of a carbon-fiber reinforced plastic material and moved in an advancing direction, in a fixed position relative to the first profile rail, such that a bar portion of the first bar is arranged between a first connecting portion of the second rail component and a second connecting portion of the second rail component, and the second rail component is cohesively connected to the first profile rail. Furthermore, the hybrid component has a first profile rail made of a carbon-fiber reinforced plastic material and a second rail component made of a titanium material.

A rail for the fastening of equipment elements, such as, in particular, seats, in aircraft, includes a holding region for connection to an equipment element of an aircraft, and a support region to fasten the rail to a carrier element of the aircraft. The rail has a metallic shell which is, for example, made of titanium and which is filled with a fiber-reinforced thermoplastic filler material which is reinforced by short fibers. To produce the rail, a metallic molded part is used as a casting mold and is filled, for example by injection, with the filler material and, after the rail has been produced, forms the metallic shell for the filler material.

Seat fittings for attaching seats to seat tracks in a vehicle and related systems and methods are described herein. An example seat fitting includes a body having a bottom surface to face a seat track, a locking stud, and a solenoid disposed in the body. The solenoid is operable to move the locking stud between a retracted position in which the locking stud is disposed in the body and an extended position in which the locking stud extends outward from the bottom surface of the body and into the seat track.

An adapter for receiving a vehicle attendant seat in a cabin of a vehicle comprises a flat retaining body, a receiving device for a vehicle attendant seat, at least one first pivoting means and at least one first securing means. The at least one first pivoting means is arranged on a pivoting edge of the retaining body and is adapted for forming a hinge with at least one correspondingly formed second pivoting means. The receiving device is arranged on a surface of the at least one retaining body, which surface extends parallel to the plane, and is adapted for mechanically connecting the vehicle attendant seat with the at least one retaining body. Thus in a vehicle cabin a vehicle attendant seat may be accommodated in a very space-saving manner even at locations to which in conventional vehicle operation access is required.

An aircraft passenger seating system comprises an array of floor panels (4) fixed within an aircraft cabin deck section (1), the floor panels (4) providing an array of discrete fixing means for removable attachment of a plurality of passenger seating units. The seating units may be of mutually different configurations each having a common footprint, such that the different configurations are interchangeable without having to re-arrange other seating units. The common footprint may be provided by a common size and shape of floor panel (4) or the floor panels (4) may provide a regular array of discrete fixing means such that the configurations may be positioned regardless of the position of the floor panels (4).

Described are base frame assemblies (10) for a passenger seat including a main frame (12) with a seat support structure (16) and a lateral support structure (18), wherein the lateral support structure (18) includes two seat fittings (28), and the seat support structure includes one seat fitting (30), and a secondary frame (14) pivotally coupled to the main frame (16), wherein the secondary frame (14) includes one seat fitting (50). A passenger seat (20) and a surrounding monument (26) are mounted to the base frame assembly (10).

A vehicle body includes a primary vehicle structure and interior vehicle fittings as well as a coupling device for fastening the interior vehicle fittings to the primary vehicle structure. The coupling device is configured to generate a magnetic field, so as to fasten the interior vehicle fittings to the primary vehicle structure without contact. Methods for assembling a vehicle body as well as an edifice are also described.