Flexible mounting plate eliminates bushings to prevent debris binding while accommodating tank expansion and contraction.
Controller measures gas pressure differences across electric lock-off valves to determine individual valve health status in split bottle systems.
Inductive power transmission eliminates wired connections and battery replacements, resolving explosive environment risks while securing LPG filling valves.
A gas vessel releasing system displaces external air with pressurized inert gas to create a protective internal environment.
Optimizing shell thickness with full radiography inspection reduces tare weight by 2000 lbs, allowing full cargo capacity without exceeding transport limits.
A reinforcing ring covers the screw-threaded portion of a hydrogen pressure vessel cylinder to isolate the joint from direct gas contact.
A high pressure tank cap uses a repelling coating to keep matrix resin out of the gas discharge flow path.
A self-saturating LNG delivery system uses a nested overflow tank to maintain hydraulic pressure for continuous engine fuel supply.
A continuous storage tank extends spanwise through aircraft wing spars, eliminating discrete connections and reducing weight for higher gravimetric efficiency.
Segmented sleeve design resolves the contradiction between preventing unauthorized removal and enabling authorized maintenance access.
Skid-mounted compressed gas dispensing station integrates compressors, storage tanks, and controls to reduce installation complexity.
An integrated safety valve opens a branch line to exhaust excess pressure, preventing container explosions without altering the existing filling structure.
Frangible nets trigger relief valves during localized fires, preventing tank ruptures without adding complex piping.
A hydrogen filling apparatus control unit adjusts initial required pressure to ensure reliable tank filling.
Segmented dry and impregnated fiber layers eliminate polymerization delays, boosting production speed and tank burst resistance.
A rapid fill apparatus conveys pressurized fluid to pneumatic firearm simulator magazines using a receiver and controlled passage.
Template-based mounting apparatus aligns cryogen injection nozzles to eliminate manual measurement errors and reduce installation time.
An underwater inflatable bladder stores pressurized gas and transfers it through liquid displacement without mechanical compression.
Movement limiter prevents irreversible deformation of the inner tube, allowing reduced wall thickness to minimize conductive heat transfer.
Nested handles maintain cryogenic contact during removal, preventing rapid warming of stored samples.
A thermally responsive pressurization device releases stored fluid into an enclosure via a fracturing hollow bulb to maintain internal pressure.
Segmented modules with universal interfaces resolve fixed-capacity bottlenecks in traditional refueling stations.
Telescopic extension mechanism moves tank manhole cover vertically and rotationally to bypass obstacles without increasing overall height.
Segmenting compression into two stages with intermediate cooling suppresses Joule-Thomson heating, maintaining safe tank temperatures.
A gas filling method calculates effective heat mass and pressure loss parameters to dynamically adjust filling conditions.
An automated shutoff device detects fuel leaks and closes regulator valves without manual intervention, preventing accidents when occupants are absent.
Segmented rigid tubular walls and exterior braces manage dynamic sloshing loads to reduce deformation in large volume LNG storage tanks.
Encapsulating the metal end within the plastic shell prevents axial displacement and gas leakage under thermal cycling.
Matching heat transfer fluid pressure to hydrogen levels reduces thermal resistance and weight in metal hydride storage heat exchangers.
Segmented mobile storage and regasification unit reduces site preparation costs by nesting tanks within containment structures.
Central tie rod moves end caps to compress annular seals radially, eliminating bottom ports and reducing leak risk while maintaining 150 PSI integrity.
Dynamic pressure adjustment overlaps sensor error ranges to resolve monitoring accuracy versus downstream device weight trade-offs.
Segmented adhesion between the resin liner and CFRP layer prevents stress concentration at ferrules during thermal shrinkage.
Leak detectors trigger automatic inert gas release to prevent explosive risks from flammable fuel degassing.
Segmented control valves stabilize hydrogen supply pressure in cryogenic tanks, resolving fluctuations from supercritical withdrawal cycles.
Segmented seat and intermediary sealing element maintain reliability against wear in pressurized gas containers.
Automated valves regulate pressure in a VOC collection system to separate emissions into liquid and gas phases while an inert atmosphere prevents fire hazards.
Segmented composite walls and local reinforcement resolve hydrogen storage density versus weight trade-offs in aircraft cryogenic tanks.
A compressed gas supply device uses automatic switchover between reservoirs to maintain continuous flow.
Tensioned straps anchor aircraft fuel tanks to coupling portions, reducing stress concentration on composite skins while maintaining structural integrity.
Reinforcing ring distributes pressure in CFRP tank openings, preventing leaks at lateral connections.
A computing device monitors pressure and flow rate to automatically switch gas tanks via electronic valves.
A mobile pressure reduction unit regulates high-pressure gas to 80 psig using automated throttling stages, preventing condensation during remote offloading.
Shock detection triggers inert gas release into the inter-wall space, preventing oxygen enrichment and maintaining thermal insulation integrity.
Deflectable tabs engage collar gaps to prevent misalignment during transport while absorbing impact energy.
An elastic intermediate member absorbs differential settlement between outer and inner supports, reducing localized bending stress on the tank bottom.
A multipurpose valve cap integrates a dedicated cavity to house the sealing washer within its structure.
Dual-material sealing rings in composite pressure vessel end bosses utilize internal pressure to expand the liner against elastomeric seals.
A blow molding method uses a shaft assembly to expand a parison into a liner shape.