Patent classifications
F17C2221/011
APPARATUS AND PROCESS FOR PRODUCING CO2 ENRICHED MEDICAL FOAM
The present invention provides an apparatus for producing medical foam for wound care or hair stimulation. The apparatus includes a foam generation unit having a fluid reservoir, a fluid delivery line and a foam generation tip. The apparatus also includes a compressed gas unit having at least one container of compressed gas, a source of electric power, and a gas regulator valve. A supply of wound care or hair stimulating solution is communicably connected to the foam generation tip such that when the apparatus is operated medical foam is produced by the foam generator tip.
CONTAINER FOR RECEIVING AND STORING CRYOGENIC FLUIDS PARTICULARLY CRYOGENIC LIQUIDS AND VISCOUS MATERIALS, AND METHOD FOR THE PRODUCTION THEREOF, AND USE THEREOF
The invention relates to a container for holding and storing liquids and viscous materials, in particular cryogenic fluids, comprising a jacket (12), which defines the interior (14) of the container (10) having a chamber (16), said container (10) being constituted of at least two container structures (20, 20′, 20″) and each of said at least two container structures (20, 20′, 20″) being formed as one piece from a blank (32) and having a dome portion (22), a branching portion (24), which is contiguous to the dome portion (22), and two cylinder portions (26, 28; 26′, 28′), which are contiguous to the branching portion (24), and the mutually facing container structures (20, 20; 20′, 20″) which are adjacent to each other being joined together.
GAS CONTROL SYSTEM
An apparatus includes a high-pressure tank, a controller, a valve, controlled by the controller, and a compressor.
Protection structure for gas cylinder and valve replacement
There is provided a protection structure for a gas cylinder assembly comprising a gas cylinder body and a valve. The gas cylinder body includes a base and a neck to which a proximal end of the valve is connectable in use. The protection structure comprises first and second structural sections, the first section being connectable to the valve such that the second section is spaced from the valve by the first section. Further, in use, the second section is arranged to transfer impact forces to the first section, and the second section is arranged to deform with respect to the second section in response to said impact forces to reduce the peak impact force on the valve.
Pressure Vessel Vented Boss with Sintered Metal Plug
A pressure vessel includes a shell, a liner, and a boss. The liner is positioned within the shell and defines the interior environment. The boss is located at a first interface between the shell and the liner. The boss includes a cavity and a venting structure located in the cavity. The cavity is located at a second interface between the liner and the boss, and the cavity is located at an interior surface of the boss in communication with the interior environment. A gas vent path is defined from the first interface, through the venting structure, and into the interior environment of the pressure vessel. The disclosure also describes a boss for a pressure vessel and a method of manufacturing the boss. The boss includes a port, a flange, a cavity and a gas venting structure. The cavity and gas venting structure are located on an interior of the flange.
Port/liner assembly method for pressure vessel
A pressure vessel includes a polymeric liner defining a fluid containment cavity and having an opening defining a port aperture extending between an inner surface and an outer surface of the polymeric liner and a rigid ring element is embedded within the polymeric liner and surrounding the port aperture. A metallic port element is disposed on the outer surface of the polymeric liner and fixed to the rigid ring element. A fiber composite material is disposed about the outer surface of the polymeric liner.
BOSS AND LINER INTERFACE FOR A PRESSURE VESSEL
A pressure vessel includes a liner, a composite shell covering the liner, and at least one boss assembly having a metal boss. The metal boss is positioned at respective openings though the liner and the composite shell. A plastic layer is formed between the liner and the metal boss. The plastic layer adheres to both the metal boss and the liner to form a seal at the interface between the metal boss and liner. The plastic layer further increases a torque strength of the metal boss.
Fresh Air/Oxygen Portable Breathing Device With or Without Aromas and Methods of Use
The present invention provides a portable, light-weight, breathing device and methods of use for delivering pristine, fresh air or varying high concentrations of oxygen with or without aroma, i.e., essential oils for stimulating appetite, boosting mood or decreasing stress and anxiety. The breathing device comprises an air container having a breathing air bag therein which contains the fresh air or the varying concentrations of oxygen optionally with the one or more essential oils, tubing for delivering the fresh air or oxygen to a breathing mask, and a plurality of movable valves included in the mask which directs air or oxygen into or out of the mask depending on whether the user is inhaling or exhaling. The breathing device also comprises the use of a can of compressed fresh air or oxygen with or without aroma to be used with an air reservoir or with an expandable air bag.
Fluid container resource management
Fluid tanks in a hospital or similar environment include sensors to detect, e.g., state and location, which can be communicated to a central station where this data can be processed to permit predictions of resource usage and enable automated management of the fluid tanks.
Tank for a spacecraft engine
Cryogenic propellant tank (1) for a spacecraft engine, comprising an external enclosure (10) defining an internal volume, characterized in that the internal volume of the tank comprises a primary volume (V1) and a secondary volume (V2) connected to the primary volume (V1) via a valve (20) configured to selectively allow a passage of fluid from the primary volume (V1) to the secondary volume (V2), or to isolate the secondary volume (V2) from the primary volume (V1), the primary volume (V1) having a primary orifice (11) adapted to be connected to a first pressurization source (41), the secondary volume (V2) having a supply orifice (4) adapted to be connected to a supply line of a spacecraft engine (30), and a secondary orifice (12) adapted to be connected to a second pressurization source (42).