A fuel tank inerting system includes a cabin air source, a conduit, a heat exchanger, and a pressurized air source. In embodiments, the pressurized air source is configured to provide pressurized air to the heat exchanger, and the conduit is configured to provide cabin air from the cabin air source to the heat exchanger.

A system and method fare disclosed for inerting a protected space. Process water is delivered to an anode of an electrochemical cell where a portion of the process water is electrolyzed to form protons and oxygen. The protons are transferred across the separator to the cathode, and process water is directed through a process water fluid flow path including a first side of a membrane. Gas is transferred to a second side of the membrane to form a de-gassed process water on the first side of the membrane, and the de-gassed process water is recycled to the anode. Air is delivered to the cathode and oxygen is reduced at the cathode to generate oxygen-depleted air. The oxygen-depleted air is directed from the cathode of the electrochemical cell along an inerting gas flow path to the protected space.

This fuel tank dam closes a gap between a first structural component fixed to the inside surface of the outer plate of a fuel tank and a second structural component provided with a cutout part into which the first structural component is inserted. This fuel tank dam includes: a first portion that can be fixed to the first structural component; a second portion that has a surface extending in a direction intersecting with the first portion and can be fixed to the second structural component; and a third portion that has a bellows and is disposed between the first portion and the second portion. This fuel tank dam is configured such that the first portion, the second portion, and the third portion are integrated, the bellows has a thickness of 0.381 to 1.524 mm, and the second portion has a thickness of 0.762 to 7.620 mm.

Various techniques are provided for an expandable energy absorbing fluid bladder. In one example, the fluid bladder includes a primary portion and a secondary portion. The secondary portion can be configured to expand or increase in volume when the fluid bladder is subjected to a pulse greater than a threshold pulse. Expansion of the secondary portion can allow fluid or additional fluid to flow into the secondary portion and thus decrease a peak pulse and, thus, avoid rupture of the fluid bladder.

A kinetic energy absorption method includes receiving a force from kinetic energy at a composite article and distributing a load associated with the force across a designated pattern of lower strength length portions or lower modulus length portions of fibers within the composite article, where the load is distributed by: plastically deforming a ply and a matrix material; separating multiple substantially parallel fibers at the lower strength length portions or plastically stretching the multiple substantially parallel fibers at the lower modulus length portions; and creating gaps in the ply where the multiple substantially parallel fibers are separated or creating shear boundaries in the ply where the multiple substantially parallel fibers are plastically stretched.

A reinforced composite article includes a first ply, a second ply, and a third ply. A first interface material is between the first ply and the second ply. A second interface material is between the second ply and the third ply. A designated pattern of material property variation, geometric structure variation, spatial variation, or combinations thereof is distributed to selected locations identified in the first interface material or distributed between selected locations identified in the first interface material compared to the second interface material. The pattern is sufficient to measurably vary adhesion, toughness, strength, modulus, or combinations thereof. The article allows distribution of a load across the pattern when the first, second, and third plies receive a force from kinetic energy above a separation threshold by partially delaminating the first ply from the second ply, the second ply from the third ply, or both.

A storage system is provided in one example embodiment and may include a storage device that may include a plurality of outer walls; and a liner that covers one or more of the outer walls, wherein the liner comprises a woven material that is puncture-resistant. A storage device is provided in another example embodiment and may include a plurality of outer walls, wherein at least one of the outer walls comprises a woven material that is puncture-resistant. A vehicle is provided in another example embodiment and may include a fuel system that includes a fuel cell. The fuel cell may include a plurality of outer walls, and at least one of: a puncture-resistant liner covers one or more of the outer walls; and one or more of the outer walls comprises a woven material that is puncture resistant.

The use of flexible foam material to provide ignition mitigation in fuel tanks is described. In one example, a system for ignition mitigation includes a number of foam blocks, wherein each foam block is pre-cut from a flexible foam material. Each foam block can have a unique profile corresponding to inner surfaces of a fuel tank at a particular sector within a compartment of the fuel tank. In other aspects, one or more of the foam blocks can include one or more upper cutouts to provide clearance for upper stiffeners in the fuel tank, one or more lower cutouts to provide clearance for lower stiffeners in the fuel tank, and one or more arcuate cutouts to provide clearance for a tank fuel pump. The foam blocks can be arranged in a stack corresponding to a sequential installation at respective sectors within the compartment of the fuel tank.

Typical composite panels are brittle and unable to support transverse pressure loads that might be imposed on the panels. For example, the use of typical panels around fuel tanks of a vehicle are unable to support transverse pressure loads that might be imposed on the fuel tanks during a crash of the vehicle or a ballistic impact to the fuel tanks. In the embodiments described herein, panels include face sheets that are bonded to a foam core. The foam core includes a corrugated core sheet that is formed from a highly ductile material, such as Polyethylene or Aluminum. When a transverse pressure load is imposed on the panel, core crush of the foam occurs as the core sheet elongates from its original corrugated shape to a curve shape during deformation. This allows the panel to dissipate the energy of the transverse pressure load applied to the panel.

A kinetic energy absorption method includes receiving a force from kinetic energy at a composite article and distributing a load associated with the force across a designated pattern of lower strength length portions or lower modulus length portions of fibers within the composite article, where the load is distributed by: plastically deforming a ply and a matrix material; separating multiple substantially parallel fibers at the lower strength length portions or plastically stretching the multiple substantially parallel fibers at the lower modulus length portions; and creating gaps in the ply where the multiple substantially parallel fibers are separated or creating shear boundaries in the ply where the multiple substantially parallel fibers are plastically stretched.