Cold liquid CO2 is stored subsea and warmed by surrounding seawater, enabling offshore reservoir injection without added heaters.
Continuous inert gas purging and pressure control keep hydrogen connection spaces non-ignitable while reducing ventilation needs and space.
Temperature and pressure sensing estimate remaining hydrogen in solid fuel storage without flow meters, improving accuracy during outages and shifts.
A polymeric collar and foot ring add drainage, regulator protection, and stable support to reduce water buildup and corrosion on pressurized tanks.
Dynamic sensor-based valve control replaces static PRV set-points to reduce wear, dead bands, and hysteresis across varying conditions.
A rotating arm coupling with abutment surfaces and shock-absorbing coating secures gas containers to bars while reducing deformation and handling interference.
Aligned access orifices and a bellows-linked pipe enable cryogenic tank inspection without demounting pipes or degrading vacuum insulation.
A check valve bypasses the pump when tank pressure is high enough, cutting drive air use and saving space in firefighter air fill systems.
Segmented protectors bond on the smoother tank body while covering the dome, preventing detachment under impact on curved surfaces.
Modular steel shell segments raise hydrogen storage above 200 bar while easing manufacturing, handling, and monitoring complexity.
Pressure, level, and temperature sensing let a controller estimate liquid and gas CO2 in transit tanks, automating handling and emissions tracking.
An initial high pressure-rise phase cools the charging hose and pipeline faster, then shifts to a reference rate to shorten fuel tank filling time.
A co-fastened lid and nozzle body secure the tank valve filter, eliminating gaps and wobble while keeping filtration effective.
A vented thermal siphon keeps heat input low while cooling an external cryogenic pump quickly for efficient fluid delivery.
Positioning teeth, grooves, and a rotation stopper align the cartridge so gas is released in the intended direction, even at high temperature.
Indirect control lets a smaller solenoid coil open a hydrogen tank shut-off valve by combining magnetic actuation with pneumatic force.
A liner is blow molded inside a cylindrical insert member to avoid pinched portions, improving vessel strength and sealing against fluid leakage.
Using onboard tanks, dual supply pipes, and a refill port, this case enables simpler, lower-cost hydrogen transfer to external destinations.
A burner-fed pre-heater and heat exchanger regulate cryogenic hydrogen temperature and flow for stable aircraft fuel delivery.
An adhesive interlayer in flat pressure-vessel regions compensates thermal expansion mismatch and prevents gap formation between layers.
A pressure-controlled refuel chamber limits tank-to-chamber pressure difference, reducing structural loads and refueling damage.
A neck seal placed ahead of the threads and a radial fill channel reduce wear, block oxidation, and allow refilling without full unscrewing.
Dynamic fuel storage and blending adjusts hydrogen and hydrocarbon ratios to match demand, improving safety, emissions, and power efficiency.
A sealed disposable gas canister stores pressurized fluid inside a medical device, replacing cumbersome external power with pin-triggered release.
Raised tank framing, corrosion-resistant lining, wash systems, and a scrubber help prevent leaks, ease inspection, and contain fumes.
Nitrogen blanketing keeps hazardous chemicals above vapor pressure in a mobile pressure tank, reducing vent treatment needs and improving safe storage.
A roller-guided wire path in the nozzle support arm blocks rainwater ingress while easing heavy gas filling nozzle handling.
A dual-bent cover shields the support arm from rainwater while counterbalancing a heavy gas filling nozzle for easier, reliable operation.
A retrofit vapor plug adapter adds protected sensor and data logger integration to dry vapor dewars for real-time shipment temperature monitoring.
A shared support holds 35 MPa and 70 MPa pressure vessels in one assembly, cutting ground area and construction labor.
A PEEK/PEDEK-based PAEK component improves cryogenic ductility, strength, and low hydrogen permeability for handling and storage.
Communication valves and coordinated control keep fuel gas flowing when a supply valve fails and help balance valve wear across tanks.
A softened barrier layer supported by base and reinforcement layers cuts permeation while preserving vessel strength during high-temperature curing.
Waste cold from liquid nitrogen is reused to sub-cool liquid CO2, stabilizing flow and boosting dry ice yield without extra energy use.
Bent upper and lower covers block rainwater at moving joints while supporting a heavy gas filling nozzle for easier, more reliable operation.
A guided wire and roller layout stabilizes the filling nozzle support arm while blocking rainwater ingress with a simpler structure.
A submerged pump and external booster raise liquid hydrogen to delivery pressure while avoiding cavitation, vapor lock, and bulky high-pressure tanks.
A segmented dewar plug uses stacked disks and sheets to vent pressure while limiting warm air ingress and cryogenic evaporation.
A softened barrier layer is held in shape by base and reinforcement layers during curing, improving pressure vessel strength and impermeability.
Inner and outer cable nets, a metal-layer membrane, and interlayer pressure control enable larger gas storage with less rupture risk and leakage.
Directly coupling both ends of conformable tanks through an on-tank manifold reduces filling temperature gradients and avoids pre-cooling.
Support collars and saddle brackets isolate cryogenic tank loads from the fuselage while allowing axial thermal expansion in aircraft.
A radial flange cable path for dewar temperature sensors cuts heat inleak, protects cables from thermal stress, and preserves cryogenic hold time.
Multiple angled outlet ports and a movable flow element keep injection velocity high, improving gas mixing and preventing tank hot spots during filling.
Separate support collars carry radial and axial loads while allowing tank expansion, isolating aircraft cryogenic tanks from fuselage heat and stress.
A blow pin with an annular recess forms a smooth resin liner neck surface, preventing parting-line leaks and reducing sealing-member wear.
A concrete pad mixed with perlite or glass marbles insulates cryogenic tank supports, protects steel from cold, and enables off-site prefabrication.
A rigid reinforcement ring at the liner neck boosts end-piece torque resistance, speeds filament winding, and improves sealing without enlarging the tank.
An ejector on the tank injection line uses motive gas and venturi suction to maintain cryogenic tank pressure during high liquid withdrawal.
Redundant IR, NFC, Bluetooth, or WiFi links improve hydrogen vehicle refueling reliability despite line-of-sight interference.