Patent classifications
F17C2270/0186
SYSTEMS AND METHODS FOR ORGANIC COMPOUND STORAGE AND TRANSFER
A method for mitigating gas and vapor absorption into organic compounds includes degassing an organic compound to generate a degassed organic compound that includes an O.sub.2 content less than or equal to 50% of a saturated value of the organic compound. The method includes transferring the degassed organic compound while preventing contamination of the organic compound through gas absorption. The method includes storing the degassed organic compound in a storage receptacle to mitigate gas and vapor absorption. An organic compound storage and transfer system includes an organic compound source. An organic compound from the organic compound source includes an O.sub.2 content less than or equal to 50% of a saturated value of the organic compound. A storage receptacle is in fluid communication with the organic compound source. An inert gas source is in fluid communication with the storage receptacle to purge the storage receptacle of other gasses and vapors.
SYSTEMS AND METHODS FOR PRESSURE CONTROL
A pressure control system includes at least one tank storing a mixture of oxygen and nitrogen. The system further includes a first branch of a pressure control line configured to transport a first portion of the mixture of oxygen and nitrogen to a pressurized enclosed volume. The system also includes a second branch of the pressure control line configured to transport a second portion of the mixture of oxygen and nitrogen to at least one flight suit removably coupled to the second branch.
Composite inner frame multi-bonded barrel, shell-integrated projectile propellant tank including same, and method for manufacturing those
Provided is a composite inner frame multi-bonded barrel, a shell-integrated projectile propellant tank including the same, and a method for manufacturing the barrel and the tank. The shell-integrated projectile propellant tank may include the composite inner frame multi-bonded barrel including a cylinder portion including a plurality of inner frames bonded together; a dome portion including an upper dome frame and a lower dome frame bonded to an upper end and a lower end of the cylinder portion, respectively; a cylindrical shell coated on an outside of the composite inner frame multi-bonded barrel; and at least one manhole cover sealing a manhole cover coupling hole formed in a center of the upper dome frame or the lower door frame, and the at least one manhole cover has a fluid injection port formed on one side thereof.
METHOD OF FABRICATING SPACE SATELLITE TANK COMPONENTS UTILIZING ADDITIVE MANUFACTURING AND SPIN FORMING
A thin wall spinformed metallic tank shell includes a first region with a first thickness and at least one second region with a second thickness greater than the first thickness including structural features formed by an additive manufacturing process, where the features are added outside and inside of the metallic tank shell and can include: polar bosses added to one or both external polar regions of a spherical section of the tank; mounting tabs on a circumferential skirt of the tank; mounting rings containing threaded holes attached to the interior or exterior surface of the tank; mounting trunnions attached to the external surface of the tank; propellant management devices attached to the interior surface of the tank; structural reinforcement vanes and ribs attached to the inside surface of the tank; and brackets and/or shelves attached to the inside surface of the tank.
Method of fabricating space satellite tank components utilizing additive manufacturing and spin forming
A method of forming a thick wall section on a specific region of a thin wall spinformed metallic tank shell includes forming a thin wall metallic tank shell blank by spinforming a metal sheet over a mandrel and removing the tank shell blank from the mandrel. The method further includes mounting the blank in an additive manufacturing system and adding metallic structural features to the tank shell according to a 3D model stored in memory in the additive manufacturing system.
Tank
A tank includes a liner including an inner shell; and a reinforcing layer covering an outer surface of the liner; wherein the reinforcing layer is formed by continuously winding resin-impregnated fiber bundles around the liner, the reinforcing layer includes a hoop layer placed in a side of the liner, and a helical layer, gaps are formed between adjacent bundles of the resin-impregnated fiber bundles wound in the hoop layer, there is at least one site where the resin-impregnated fiber bundles are wound without forming a gap between adjacent bundles in the helical layer, and resin in the resin-impregnated fiber bundles has a resin toughness value of not less than 1.0 MPa.Math.m.sup.0.5.
PRESSURE VESSEL COMPRISING AN INTERIOR CHAMBER, AND METHOD FOR MANUFACTURING A PRESSURE VESSEL
The invention relates to a pressure vessel (1) with an interior chamber (30), in particular for storing hydrogen, comprising a vessel wall (12) which has or consists of a composite material unit (14, 22, 26) with reinforcing fibers (16) and a thermoplastic plastic matrix (18), wherein the composite material unit (14, 22, 26) is arranged and configured such that the reinforcing fibers (16) can be removed as continuous fibers, in particular non-destructively, so that the composite material unit can be reused.
FLUID-STORAGE TANK
Fluid storage tank, comprising at least one layer, wherein the at least one layer encloses at least one chamber, further comprising a valve, the valve connecting an interior of the at least one chamber with an exterior of the at least one chamber, wherein the fluid storage tank is made at least partially by means of 3D-printing.
Vapor Cooled Shielding Liner for Cryogenic Storage in Composite Pressure Vessels
A novel tank cryogenic-compatible composite pressure vessel that beneficially utilizes Vapor Cooled Shielding (VCS) is introduced to minimize thermal gradients along support structures and reduces heat loads on cryogenic systems. In particular, the configurations and mechanisms to be utilized herein include: providing for a desired number of passageways and a given thickness of the VCS, reducing the thermal conductivity of the VCS material, and increasing the cooling capacitance of the hydrogen vapors.
Wire wrapped pressure vessels
A pressure vessel (2) for the storage of fluid has a core (10) made of metal or polymer and is wrapped either completely or partially from outside with a high strength fibers (21, 22) for reinforcement wherein one of the reinforcing fibers is a metal wire (21) of a single filament or cables of multi filaments having strength from 2000 MPa to 6000 MPa. The wire has a plastic ductility of over 20% in reduction in area (RA) at tensile fracture. The metal wire (21) is made of steel or nickel or titanium or their respective alloys. The core (10) of the vessel (2) is first wrapped with a resin covered ceramic fibers such as carbon, fiberglass and subsequently wrapped with the metal wire (21) with or without other fibers (22). The metal wires (21) can be of different diameters in parallel or cabled forms.