Cryogenic liquid tank

Patent metadata

Field	Value
Publication number	US-10584828-B2
Application number	US-201715823339-A
Country	US
Kind code	B2
Filing date	Nov 27, 2017
Priority date	Sep 23, 2008
Publication date	Mar 10, 2020
Grant date	Mar 10, 2020

Abstract

A hydrogen storage tank for a hydrogen fueled aircraft. The tank has a wall made of layers of aerogel sections around a hard shell layer, sealed within a flexible outer layer, and having the air removed to form a vacuum. The periphery of each layer section abuts other sections of that layer, but only overlies the periphery of the sections of other layers at individual points. The wall is characterized by a thermal conductivity that is lower near its gravitational top than its gravitational bottom. The tank has two exit passageways, one being direct, and the other passing through a vapor shield that extends through the wall between two layers of aerogel. A control system controls the relative flow through the two passages to regulate the boil-off rate of the tank.

First claim

What is claimed is:

1. A storage tank, comprising:
an inner-most layer that defines and substantially surrounds a fluid storage space;
a first set of one or more tubes configured to be used as a vapor shield around at least a portion of the inner-most layer, the first set of one or more tubes being adapted as a first passageway extending from within the fluid storage space to outside of the fluid storage space;
a second set of one or more tubes adapted as a second passageway extending from within the fluid storage space to outside of the fluid storage space; and
a switching device configured to control the relative flow rates from the first and second passageways.

2. The storage tank of claim 1 , wherein the switching device is located outside the fluid storage space.

3. The storage tank of claim 1 , wherein the second passageway is a direct exit that is not adapted to function as a vapor shield.

4. The storage tank of claim 1 , and further comprising a controller configured to vary the relative flow rates based on pressure requirements of the storage tank.

5. The storage tank of claim 1 , wherein the tank is configured to store a fluid as a cryogenic liquid, and further comprising a controller configured to vary the relative flow rates based on a desired flow rate of fluid vapor.

Assignees

• Aerovironment Inc

Inventors

• Brooks Alexander N
• Hibbs Bart D
• Thompson David R

Classifications

• F17C2250/043

  Pressure · CPC title

• F17C2203/0358

  in form of panels · CPC title

• F17C2221/012

  Hydrogen · CPC title

• F17C2260/012

  Reducing weight · CPC title

• F17C2209/221

  Welding · CPC title