Granted Patent B2

US 12,644,565 · App. 17/883,895 · Granted Jun 2, 2026

Inventors: Ernst Wolfgang Stautner (Niskayuna, NY); Constantinos Minas (Slingerlands, NY)

Assignee: General Electric Company

F17C1/12F17C2201/0109F17C2203/0391F17C2203/0629F17C2205/0308F17C2209/22F17C2221/012F17C2221/033F17C2223/0161F17C2265/066F17C2270/0189

Abstract

Claims (30)

1 . A cryogenic system, comprising:

a cryogenic tank containing a liquid cryogen;

a vacuum vessel surrounding the cryogenic tank and providing a vacuum space between an inner surface of the vacuum vessel and an outer surface of the cryogenic tank; and

a suspension system arranged within the vacuum space so as to support the cryogenic tank within the vacuum vessel and to maintain the cryogenic tank within the vacuum vessel in a desired position, the suspension system comprising:

a pair of axial suspension members disposed at axially opposite ends of the cryogenic tank; and

a plurality of radial suspension members radially spaced and arranged circumferentially around the cryogenic vessel, each of the pair of axial suspension members and the plurality of radial suspension members comprising a plurality of roller elements arranged within the vacuum space and having a rounded outer surface in simultaneous point contact with the inner surface of the vacuum vessel and the outer surface of a tank wall of the cryogenic tank that bounds an interior volume containing the liquid cryogen.

2 . The cryogenic system of claim 1 , wherein the one or more axial suspension members comprise one or more locking features configured to lock the one or more axial suspension members with respect to the one or more radial suspension members.

3 . The cryogenic system of claim 1 , wherein the plurality of roller elements are connected together via one or more guide rails, and wherein the plurality of roller elements comprise cylindrical roller elements connected together via the one or more guide rails.

4 . The cryogenic system of claim 1 , wherein the plurality of roller elements comprise ball bearings.

5 . The cryogenic system of claim 4 , wherein the one or more radial suspension members extend through the ball bearings.

6 . The cryogenic system of claim 1 , wherein the suspension system further comprises one or more insulation members arranged between one or more of the plurality of roller elements.

7 . The cryogenic system of claim 1 , wherein the suspension system further comprises at least one ring member connecting the plurality of rows of roller elements together.

8 . The cryogenic system of claim 1 , wherein the cryogenic tank is slidable with respect to the vacuum vessel.

9 . The cryogenic system of claim 1 , wherein the vacuum vessel comprises a removable cap, wherein the removable cap is disposed adjacent to one of the axial suspension members of the pair of axial suspension members.

10 . The cryogenic system of claim 1 , wherein the cryogenic system is part of one of a turbojet engine or a superconducting generator.

11 . The cryogenic system of claim 1 , wherein the cryogenic tank and the vacuum vessel are each constructed of a composite material.

12 . A method of assembling a cryogenic system, the method comprising:

securing a suspension system having a plurality of roller elements circumferentially around a cryogenic tank containing a liquid cryogen;

arranging the plurality of roller elements in an axial direction in the vacuum space via one or more axial suspension members and in a radial direction in the vacuum space via one or more radial suspension members;

sliding the cryogenic tank into a vacuum vessel via the plurality of roller elements such that a radial space is created between an inner surface of the vacuum vessel and an outer surface of the cryogenic tank and a rounded outer surface of each roller element of the plurality of roller elements is in simultaneous point contact with the inner surface of the vacuum vessel and the outer surface of a tank wall of the cryogenic tank that bounds an interior volume containing the liquid cryogen; and

creating a vacuum within the radial space, wherein the suspension system supports the cryogenic tank within the vacuum vessel and maintains the cryogenic tank within the vacuum vessel in a desired position.

13 . The method of claim 12 , further comprising opening a removable cap of the vacuum vessel prior to sliding the cryogenic tank into the vacuum vessel via the plurality of roller elements and subsequently closing the removable cap once the cryogenic tank is slid into place.

14 . The method of claim 12 , further comprising connecting the plurality of roller elements together via one or more guide rails, wherein the plurality of roller elements comprise cylindrical roller elements connected together via the one or more guide rails.

15 . The method of claim 12 , wherein the plurality of roller elements comprise ball bearings.

16 . The method of claim 12 , further comprising:

securing the one or more axial suspension members to the one or more radial suspension members via one or more locking features on the one or more axial suspension members.

17 . A cryogenic fuel system for a turbojet engine, the cryogenic fuel system comprising:

a cryogenic tank containing a liquid cryogen fuel for the turbojet engine;

a vacuum vessel surrounding the cryogenic tank and providing a vacuum space between an inner surface of the vacuum vessel and an outer surface of the cryogenic tank; and

a plurality of roller elements arranged within the vacuum space and having a rounded outer surface in simultaneous point contact with the inner surface of the vacuum vessel and the outer surface of a tank wall of the cryogenic tank that bounds an interior volume containing the liquid cryogen fuel at a plurality of different points along a radial length and an axial length of the cryogenic tank so as to support the cryogenic tank within the vacuum vessel and maintain the cryogenic tank within the vacuum vessel in a desired position.

Assignments (1)

Continuity (1)

References Cited (175)