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Clean Hydrogen Partnership

Fire during LH2 transfer from tanker

Event

Event ID
353
Quality
Description
During the preparation for a liquid hydrogen transfer from a tanker to a stationary storage system, the safety valve opened and the gas ignited.
The incident occurred when a pressure build-up was initiated by opening the liquid hydrogen valve to the build-up coil. Flames filled the control cabinet. The fire appeared at three pipe connections to the vent line, all on the vent side of the relief valve. The fires were terminated after all the valves were closed. However, the release continued through the high pressure relief valve. The fire was put out by terminating the supply to all the leaks. The gas was allowed to burn out and also slowed by using helium in the gas phase.

[Ordin, NASA (1974)]
Event Initiating system
Classification of the physical effects
Hydrogen Release and Ignition
Nature of the consequences
Fire (No additional details provided)
Macro-region
North America
Country
United States
Date
-
Main component involved?
Prd (Valve)
How was it involved?
Correct Activation
Initiating cause
Over-Pressurisation
Root causes
Root CAUSE analysis
The INITIATING CAUSE the build-up of an overpressure in the liquid hydrogen tanker the preparatory pressurisation step, with consequent correct activation of the pressure relief valve.
IGNITION occurred most likely by static charges.

A few FACTORS contributed to an escalation:

(1) The blow down probably caused a pressure rise in the vent line manifold into which all the relief and vent lines were connected. The pressure rise broke a pipe on the vent line and a large amount of high velocity gas was vented through that crack.
(2) Hydrogen leaks and fires developed at the threaded sections at the ruptured pipe nipple. The reason for this was road vibrations and limited pipe support, which caused blockage at the threaded sections and rupture of the pipe nipple.
(3) The pressure relief valve did not reclose, because impeded by a metallic piece, and the hydrogen flow from the tanker continued.

The ROOT CAUSE could be identified as a combination of shortcomings in design (vent pipe structure, vibrations and overpressure in the vent), and in liquid hydrogen transfer procedures.

Facility

Application
Hydrogen Transport And Distribution
Sub-application
LH2 tanker
Hydrogen supply chain stage
Hydrogen Transfer (No additional details provided)
All components affected
safety valve, vent, LH2 storage
Location type
Open
Location description
Industrial Area
Operational condition
Pre-event occurrences
The preparation of the tanker for LH2 transfer had just started.

Emergency & Consequences

Number of injured persons
0
Number of fatalities
0
Environmental damage
0
Property loss (offsite)
0
Post-event summary
Probably the whole content of the tanker was lost. Assuming a cost of LH2 of approximately 0.2 US$/kg (in 1968: https://ntrs.nasa.gov/api/citations/19680018755/downloads/19680018755.pdf), and a tanker load of approximately 3 t, result in a property loss of only 600 US$.
The LH2 cost provided corresponds to large scale production, it doe not cosnider conditioning and transport. Assuming one order of magnitude higher, 2 US$/kg would result in 6000 US$ of losses.

Lesson Learnt

Lesson Learnt
At the time of this event, the LH2 transfer technology was still in its infancy. This and similar mishaps reported by Ordin in the ears 1950-70 have been critical in reaching technological maturity of LH2 production, handling and transport, thanks also to mishaps of relatively very small consequences.

Event Nature

Release type
gas
Involved substances (% vol)
H2 100%
Release duration
unknown
Released amount
3000
Actual pressure (MPa)
<1.0
Design pressure (MPa)
<1.0
Presumed ignition source
Static electricity

References

Reference & weblink

Mishap no 1 in <br />
P. L. Ordin, Review of hydrogen accidents and incidents in NASA operations, 1974, NASA TM X-71565<br />
https://ntrs.nasa.gov/citations/19740020344

JRC assessment