Boil-off shielded coupling for hydrogen tank filling
A hydrogen fuel coupling system may include a hydrogen fuel tank and a hydrogen fuel supply connector. The tank has a first connector, and a second connector disposed around the first connector. The second connector has a boil-off inlet port for receiving gaseous hydrogen from the tank. The hydrogen fuel supply connector may include a hydrogen fuel transfer line, a third connector for operably sealably connecting the transfer line to a first connector of the tank for supplying liquid hydrogen, and a shroud extending around the third connector and the transfer line defining a gap therebetween. A fourth connector operably sealably connects a first end of the shroud to a second connector of the tank. A second end of the shroud is operably sealably engageable with the transfer line. A boil-off vent is connected to the shroud for venting gas from the gap.
1. A hydrogen fuel coupling system comprising:
a hydrogen fuel tank comprising:
a body with a chamber therein for storing liquid hydrogen;
a first connector in fluid communication with the chamber;
a second connector disposed around the first connector, the second connector having a boil-off inlet port for receiving gaseous hydrogen from the chamber;
a hydrogen fuel supply connector comprising:
a hydrogen fuel transfer line having a passageway therethrough and operably connectable to a liquid hydrogen supply;
a third connector for operably sealably connecting the hydrogen fuel transfer line to the first connector of the hydrogen fuel tank for supplying liquid hydrogen, via the passageway, to the chamber in the hydrogen fuel tank;
a shroud extending around the third connector and the hydrogen fuel transfer line defining a gap therebetween, the shroud having a first end and a second end, the second end operably sealably engageable with the hydrogen fuel transfer line;
a fourth connector for operably sealably connecting a first end of the shroud to the second connector of the hydrogen fuel tank; and
a boil-off vent connected to the shroud for venting gas from the gap.
2. The system of claim 1 further comprising:
a grooved collar fixedly disposed around the hydrogen fuel transfer line, the grooved collar having a first groove and a spaced-apart second groove;
a ring slidably disposed around the grooved collar;
a compression spring disposed between the shroud and the ring for biasing the shroud away from the ring;
at least one first handle fixedly attached to the ring;
at least one second handle movably attached to the ring, the second handle attached to a movable member having a distal end selectably disposable in the first groove and the second groove; and
a cover extending around the shroud, the cover fixedly connected to the ring, the cover comprising:
at least one catch selectively engageable with at least one first pin attached to the shroud to selectively rotatably lock the cover to the shroud; and
at least one curved groove selectively engageable with at least one second pin attached to the second connector of the hydrogen fuel tank to move the cover and ring relative to the shroud.
3. The system of claim 2 wherein:
the cover is slidable axially along a longitudinal axis of the hydrogen fuel supply connector to disengage the catch from the at least one first pin to allow rotation of the cover relative to the shroud; and
the curved groove is slidably movable around the longitudinal axis of the hydrogen fuel supply connector and the at least one second pin to longitudinally move the cover relative to the shroud.
4. The system of claim 2 wherein:
the at least one first handle is rotatable about a longitudinal axis of the hydrogen fuel transfer line to rotate the third connector; and
the at least one first handle is movable axially along the longitudinally axis to engage the fourth connector with the second connector.
5. The system of claim 1 wherein:
the second connector comprise an annular sealing surface disposed perpendicular to the longitudinal axis of the first connector; and
the fourth connector comprises an annular seal engageable with the annular sealing surface of the second connector.
6. The system of claim 5 wherein:
the annular seal comprises an O-ring.
7. The system of claim 1 wherein:
the shroud is movable independently relative to the hydrogen fuel transfer line.
8. The system of claim 1 wherein:
the first connector comprises a male quick connector;
the third connector comprises a female quick connector; and
the second connector and the fourth connector comprises a non-quick connector.
9. The system of claim 1 wherein:
the third connector is sealably connectable to the first connector prior to the fourth connector being sealably connectable to the second connector.
10. The system of claim 1 wherein:
the shroud comprises an inner wall, an outer wall, and a first end and a second end connecting the inner wall to the outer wall to define a cavity therebetween.
11. The system of claim 10 wherein:
the cavity in the shroud comprises an insulation material.
12. The system of claim 1 further comprising an unmanned aerial vehicle, and the hydrogen fuel tank disposed in the unmanned aerial vehicle.
13. A method comprising:
providing the hydrogen fuel coupling system of claim 1 ;
connecting the hydrogen fuel supply connector to the hydrogen fuel tank;
supplying liquid hydrogen from a liquid hydrogen supply via the hydrogen fuel supply connector to the hydrogen fuel tank; and
venting boil-off gas from the shroud.