thermal analysis of cryogenic hydrogen liquid separator
TRANSCRIPT
TFAWS Active Thermal Paper Session
Thermal Analysis of Cryogenic Hydrogen
Liquid SeparatorJ. F. CongiardoC. R. Fortier(NASA KSC)
Presented ByJared F. Congiardo
Thermal & Fluids Analysis WorkshopTFAWS 2014August 4 - 8, 2014NASA Glenn Research CenterCleveland, OH
Background
• Space Launch System Core Stage engine conditioning requires a high flowrate of liquid hydrogen to be accommodated by the launch pad systems.
• Launch pad flare stack designed to dispose of gaseous hydrogen.
• Analysis of ground system performance indicated that liquid hydrogen would not completely vaporize prior to arrival at the flare stack.
Background
• Therefore, a cryogenic liquid separator is being developed in order to detain liquid hydrogen and protect the flare stack.
TFAWS 2014 – August 4-8, 2014 3
Flare Stack
Design Considerations
• Separator must:– Detain liquid hydrogen at approximately 20% quality flow >10
lbm/s for 5 minutes.– Add minimal resistance to overall system flow. – Be capable of being emptied within 12 hours for scrub
turnaround, by some combination of drain and boiloff. – Have inlet and outlet piping above the anticipated maximum
liquid level.
Separator Performance Modeling
• The separator tank component was modeled in Thermal Desktop – Thermal node network generated with TD surfaces– Tank liquid volume represented with twinned lump– Lump connected to the tank surface with pool boiling ties– Inlet/outlet pipe represented with macros– Flow simulated with Set Mass Flow component
Component Model Assumptions
• The tank performance during the high flow portion of the operation was contingent on the following assumptions:– Environmental temperature at 99°F. (Per NASA-HDBK-1001)– Natural convection horizontal heat transfer around cylinder– Preliminary system operations chills the tank to cryogenic temps
(-400°F)– ½ inch thick tank wall
Tank Performance (Uninsulated)
Possible high temperature differential during boiloff
Approx. 2.5 psi delta P initially (possible startup artifact) Max 0.2 psi delta P during high flow
Boiloff in approx. 3 hours
Tank Performance (Insulated)
Lower temperature differential during boiloff
Approx. 2.5 psi delta P initially (possible startup artifact) Max 0.5 psi delta P during high flow
Boiloff in 18+ hours
Integrated Model
• Component model integrated into overall model of engine conditioning subsystem to validate:– Minimal resistance to system flow– Tank chilldown assumption
• Assumes:– Environmental boundary conditions at NASA-HDBK-1001
Min/Max (19°F/99°F)– Varying polyurethane insulation thickness on tank– Natural convection horizontal heat transfer on tank
Integrated Model
TO PAD
SEPARATOREXPANSION LOOP
FLARE STACK
System Performance, 99°F, Frost-Insulated Inlet Pipe
Tank Bottom/Bulk Temp, T=99F, Frost on Pipe
tem
pera
ture
, deg
F
0.0 0.5 1.0 1.5 2.0
100
0
-100
-200
-300
-400
-500
Time hr time from start of replenish
WinPlot v4.55 rc1
10:14:49PM 07/20/2014
f_10i_t99.csv T_37 deg F wall temf_10i_t99.csv T_1000 deg F liq tef_25i_t99.csv T_37 deg F wall temf_25i_t99.csv T_1000 deg F liq te
f_50i_t99.csv T_37 deg F wall temf_50i_t99.csv T_1000 deg F liq tef_75i_t99.csv T_37 deg F wall temf_75i_t99.csv T_1000 deg F liq te
f_100i_t99.csv T_37 deg F wall tef_100i_t99.csv T_1000 deg F liq t
Tank Liquid Volume, T=99F, Frost on Pipe
Volu
me,
ft^3
0.0 0.5 1.0 1.5 2.0
800
600
400
200
0
-200
Time hr time from start of replenish
WinPlot v4.55 rc1
10:04:04PM 07/20/2014
f_0i_t99.csv V_1000 ft^3 tk liquidf_10i_t99.csv V_1000 ft^3 tk liqui
f_25i_t99.csv V_1000 ft^3 tk liquif_50i_t99.csv V_1000 ft^3 tk liqui
f_75i_t99.csv V_1000 ft^3 tk liquif_100i_t99.csv V_1000 ft^3 tk liqu
Hydrogen in tank becomes saturated vapor
Liquid begins to form in tank during low flow portion
Tank begins to fill with liquid during low flow portion
Wall temp at bottom of tank
System Performance, 19°F, Frost-Insulated Inlet Pipe
Tank Bottom/Bulk Temp, T=19F, Frost on Pipe
tem
pera
ture
, deg
F
0.0 0.5 1.0 1.5 2.0
100
0
-100
-200
-300
-400
-500
Time hr time from start of replenish
WinPlot v4.55 rc1
9:53:46AM 07/21/2014
f_0i_t19.csv T_37 deg F wall temf_0i_t19.csv T_1000 deg F liq temf_25i_t19.csv T_37 deg F wall temf_25i_t19.csv T_1000 deg F liq te
f_50i_t19.csv T_37 deg F wall temf_50i_t19.csv T_1000 deg F liq tef_75i_t19.csv T_37 deg F wall temf_75i_t19.csv T_1000 deg F liq te
f_100i_t19.csv T_37 deg F wall tef_100i_t19.csv T_1000 deg F liq t
Tank Liquid Volume, T=19F, Frost on Pipe
volu
me,
ft^3
0.0 0.5 1.0 1.5 2.0
1000
800
600
400
200
0
Time hr time from start of replenish
WinPlot v4.55 rc1
9:56:28AM 07/21/2014
f_0i_t19.csv V_1000 ft^3 tk liquidf_25i_t19.csv V_1000 ft^3 tk liqu
f_50i_t19.csv V_1000 ft^3 tk liquf_75i_t19.csv V_1000 ft^3 tk liqu
f_100i_t19.csv V_1000 ft^3 tk liq
Performance similar to 99°F. Time to first liquid formation shortened by 15 minutes.
System Performance, 99°F, Bare Inlet Pipe
Tank Bottom/Bulk Temp, T=99F, No Frost
tem
pera
ture
, deg
F
0.0 0.5 1.0 1.5 2.0
100
0
-100
-200
-300
-400
-500
Time hr time from start of replenish
WinPlot v4.55 rc1
12:11:36AM 07/21/2014
nf_0i_t99.csv T_37 deg F wall temnf_0i_t99.csv T_1000 deg F liq tenf_25i_t99.csv T_37 deg F wall tenf_25i_t99.csv T_1000 deg F liq t
nf_50i_t99.csv T_37 deg F wall tenf_50i_t99.csv T_1000 deg F liq tnf_75i_t99.csv T_37 deg F wall tenf_75i_t99.csv T_1000 deg F liq t
nf_100i_t99.csv T_37 deg F wall tnf_100i_t99.csv T_1000 deg F liq
Tank Liquid Volume, T=99F, No Frost
Volu
me,
ft^3
0.0 0.5 1.0 1.5 2.0
400
300
200
100
0
Time hr time from start of replenish
WinPlot v4.55 rc1
9:50:51AM 07/21/2014
nf_0i_t99.csv V_1000 ft^3 tk liquinf_25i_t99.csv V_1000 ft^3 tk liqu
nf_50i_t99.csv V_1000 ft^3 tk liqunf_75i_t99.csv V_1000 ft^3 tk liqu
nf_100i_t99.csv V_1000 ft^3 tk liq
Hydrogen in tank cold, but still superheated during
Liquid begins to form in tank during high flow portion
Tank begins to fill with during high flow portion
Wall temp at bottom of tank
System Performance, 99°F, Frost-Insulated Inlet Pipe, Thin Walled Tank
Tank Wall/Bulk Temperature, 1/2" vs 3/16"
tem
pera
ture
, deg
F
0.0 0.5 1.0 1.5 2.0
100
0
-100
-200
-300
-400
-500
Time hr time from start of replenish
WinPlot v4.55 rc1
10:10:43AM 07/21/2014
f_25i_t99.csv T_37 deg F wall tempf_25i_t99.csv T_1000 deg F liq temp
f_25i_t99_thin.csv T_37 deg F wall tempf_25i_t99_thin.csv T_1000 deg F liq temp
Tank Liquid Volume, 3/16" wall, Frost on Pipe
volu
me,
ft^3
0.0 0.5 1.0 1.5 2.0
1200
1000
800
600
400
200
0
Time hr time from start of replenish
WinPlot v4.55 rc1
10:16:14AM 07/21/2014
f_10i_t99_thin.csv V_1000 ft^3 tkf_25i_t99_thin.csv V_1000 ft^3 tk
f_50i_t99_thin.csv V_1000 ft^3 tkf_75i_t99_thin.csv V_1000 ft^3 tk
f_100i_t99_thin.csv V_1000 ft^3f_0i_t99_thin.csv V_1000 ft^3 tk
Liquid formation begins approx. 30 min sooner
Tank Differential Pressure
Tank Differential PressureD
iffer
entia
l Pre
ssur
e, p
sid
0.0 0.5 1.0 1.5 2.0
0.02
0.00
-0.02
-0.04
-0.06
-0.08
Time hr time from start of replenish
WinPlot v4.55 rc1
10:06:17AM 07/21/2014
f_25i_t99.csv [P_11970]-[P_11971]f_25i_t99_thin.csv [P_11970]-[P_1
f_25i_t19.csv [P_11970]-[P_11971]nf_25i_t99.csv [P_11970]-[P_1197
nf_25i_t99_thin.csv [P_11970]-[P_
Conclusions
• Separator is capable of detaining flow as required• Insulation has direct effect on boiloff time and liquid
formation– Drain line necessary
• Tank will chill, though not necessarily as assumed in component model– Little effect on prepress behavior for warmer tank – Potential for initial liquid formation affects volume assumptions– Tank wall thickness affects system performance significantly
• Separator tank shows no evidence of adding major resistance to overall system.
Questions?