Abstract: A track system for a vehicle on a ground, wherein the track system is reconfigurable, such as by rearranging or otherwise altering one or more components of the track system (e.g., wheels, pivots or other joints, frame members, etc., by changing their position, movability, etc.) and/or by repositioning the track system relative to a frame of the vehicle, which may be useful, for instance, to enhance performance of the vehicle (e.g., maximize or otherwise increase traction and/or pulling force (e.g., drawbar pull); improve steerability; etc.), ride quality (e.g., comfort), effects on the ground (e.g., minimize or otherwise reduce soil compaction and/or soil shear stress; provide headland protection; etc.), and/or other aspects of the track system and/or the vehicle, and/or for various other purposes.

Abstract: An aircraft includes a fuselage defining a mold line, at least one frame disposed in the fuselage, at least one transparent pane suspended within the frame. The transparent pane is a deformable material that defines a first surface position h1 when not subjected to a differential pressure ?P thereacross and a second surface position h2 when subject to the differential pressure ?P thereacross. The first and second surface positions are defined with reference to the outside mold line. The first surface position h1 defines a reverse curvature. In response to the differential pressure ?P, the second surface position h2 includes bulging of the transparent pane by a predetermined distance ?h. The frame is constructed to be positioned within the aircraft such that the transparent pane presents a surface, when subjected to the pressure differential ?P, that is substantially consistent with the outside mold line of the vehicle.

Abstract: An aircraft includes a fuselage defining a mold line, at least one frame disposed in the fuselage, at least one transparent pane suspended within the frame. The transparent pane is a deformable material that defines a first surface position h1 when not subjected to a differential pressure ?P thereacross and a second surface position h2 when subject to the differential pressure ?P thereacross. The first and second surface positions are defined with reference to the outside mold line. The first surface position h1 defines a reverse curvature. In response to the differential pressure ?P, the second surface position h2 includes bulging of the transparent pane by a predetermined distance ?h. The frame is constructed to be positioned within the aircraft such that the transparent pane presents a surface, when subjected to the pressure differential ?P, that is substantially consistent with the outside mold line of the vehicle.

Abstract: A window for a vehicle includes at least one transparent pane suspendable within a frame. The transparent pane comprises a deformable material. The transparent pane defines a first surface position h1 when not subjected to a pressure differential thereacross and a second surface position h2 when subject to the differential pressure thereacross. The first and second surface positions are defined with reference to an outside mold line. The first surface position h1 defines a reverse curvature with respect to the outside mold line. In response to the differential pressure ?P, the second surface position h2 includes bulging of the transparent pane by a predetermined distance ?h. The frame is constructed to be positioned within the vehicle such that the transparent pane presents a surface, when subjected to the pressure differential ?P, that is substantially consistent with the outside mold line of the vehicle.

Abstract: The invention relates to a protection panel (115) for a vehicle that comprises an outer surface (140) including at least one composite material, and is mounted via deformable parts on a mounting (135) attached to the vehicle structure. The deformable parts are attached to several stiffening parts (145) of the mounting. In some embodiments, the deformable parts are perpendicular to the outer surface of the panel and are capable of buckling under the effect of impacts. In some embodiments, the deformable parts are in the form of clips, the composite material consists of CFRP and the mounting is rigid.

Abstract: A window for a vehicle includes at least one transparent pane suspendable within a frame. The transparent pane comprises a deformable material. The transparent pane defines a first surface position h1 when not subjected to a pressure differential thereacross and a second surface position h2 when subject to the differential pressure thereacross. The first and second surface positions are defined with reference to an outside mold line. The first surface position h1 defines a reverse curvature with respect to the outside mold line. In response to the differential pressure ?P, the second surface position h2 includes bulging of the transparent pane by a predetermined distance ?h. The frame is constructed to be positioned within the vehicle such that the transparent pane presents a surface, when subjected to the pressure differential ?P, that is substantially consistent with the outside mold line of the vehicle.

Abstract: An installation of systems in aircraft fuselages such as thermophonic insulation mattresses and devices such as onboard systems, and bundles of electric wires or fluid ducts (air, water, oxygen, hydraulic fluid). A structure for fastening onto an aircraft fuselage includes at least frames and stringers, the structure further including: fuselage stabilizers connecting the frames and stringers, wherein two stabilizers of two consecutive frames face each other between the two consecutive frames; and a strip board connecting the two stabilizers and including a fastening mechanism arranged so as to receive corresponding fastening mechanisms of the insulation mattresses and the devices.

Abstract: An installation of systems in aircraft fuselages such as thermophonic insulation mattresses and devices such as onboard systems, and bundles of electric wires or fluid ducts (air, water, oxygen, hydraulic fluid). A structure for fastening onto an aircraft fuselage includes at least frames and stringers, the structure further including: fuselage stabilizers connecting the frames and stringers, wherein two stabilizers of two consecutive frames face each other between the two consecutive frames; and a strip board connecting the two stabilizers and including a fastening mechanism arranged so as to receive corresponding fastening mechanisms of the insulation mattresses and the devices.

Abstract: The invention relates to a protection panel (115) for a vehicle that comprises an outer surface (140) including at least one composite material, and is mounted via deformable parts on a mounting (135) attached to the vehicle structure. The deformable parts are attached to several stiffening parts (145) of the mounting. In some embodiments, the deformable parts are perpendicular to the outer surface of the panel and are capable of buckling under the effect of impacts. In some embodiments, the deformable parts are in the form of clips, the composite material consists of CFRP and the mounting is rigid.