IP Library › Granted Patent US 8,950,195
Granted Patent B2
US 8,950,195 · App. 12/972,428 · Granted Feb 10, 2015

Continuous flow thermodynamic pump

Inventor: Daniel A. Watts (Surfside, CA)
Assignee: The Boeing Company
F17C5/06F17C9/02Y02E60/321
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Quick Facts
Patent No.
US 8,950,195
App. No.
12/972,428
Granted
Feb 10, 2015
Kind
B2
Abstract

A thermodynamic pump for provides gaseous hydrogen employing a plurality of liquid hydrogen (LH2) tanks sequentially pressurized with gaseous hydrogen (GH2) from an accumulator. A heat exchanger receiving LH2 from each of the plurality of tanks as sequentially pressurized returns pressurized GH2 to the accumulator for supply to an engine.

Claims (13)

1. A thermodynamic pump system for providing gaseous hydrogen comprising:

an accumulator for storing pressurized gaseous hydrogen;

a plurality of liquid hydrogen (LH2) tanks in fluid communication with an outlet of the accumulator and controlled for sequential pressurization; and

a heat exchanger in fluid communication with the accumulator and in controlled fluid communication with the plurality of tanks for sequentially receiving LH2;

a supply manifold directly connecting the plurality of tanks to the heat exchanger;

a pressurization manifold directly connecting the accumulator to the plurality of tanks;

a fill manifold directly connecting the plurality of tanks to a dewar; and,

a blow down manifold directly connecting the plurality of tanks to the dewar.

2. The thermodynamic pump defined in claim 1 wherein the supply manifold further comprises a plurality of supply valves for sequential supply of LH2 from the plurality of tanks to the heat exchanger.

3. The thermodynamic pump as defined in claim 2 wherein the pressurization manifold further comprises a plurality of pressurization valves for sequential pressurization of the tanks concurrent with the sequential supply of LH2.

4. The thermodynamic pump as defined in claim 1 wherein the fill manifold further comprises a plurality of fill valves for sequential fill of the tanks with LH2.

5. The thermodynamic pump as defined in claim 4 wherein the blow down manifold further comprises a plurality of depressurization valves for sequential depressurization of gaseous hydrogen (GH2) from the tanks concurrent with the sequential fill of LH2.

6. The thermodynamic pump as defined in claim 5 further comprising an accumulator condenser intermediate the dewar and tanks, said accumulator condenser providing LH2 to the fill manifold and receiving GH2 from the blowdown manifold.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 18, 2010
From: WATTS, DANIEL A.
To: THE BOEING COMPANY
Reel/Frame 025525/0534 →
Continuity (1)
Related Publication 20120156059A1 · Jun 21, 2012