Composite tanks for reusable launch vehicles and methods of fabricating thereof

Patent metadata

Field	Value
Publication number	US-12059953-B2
Application number	US-202117405509-A
Country	US
Kind code	B2
Filing date	Aug 18, 2021
Priority date	Feb 17, 2021
Publication date	Aug 13, 2024
Grant date	Aug 13, 2024

Abstract

A composite tank for a reusable launch vehicle comprises a composite wall, having a first coefficient of thermal expansion. The composite wall comprises a first end, a second end, a central axis, which passes through the first end and through the second end, and a cylindrical interior surface. The composite tank also comprises slosh baffles, formed from a second material, having a second coefficient of thermal expansion that is different from the first coefficient of thermal expansion. Each of the slosh baffles is attached to the cylindrical interior surface of the composite wall. Each of the slosh baffles is annular and is separated from the cylindrical interior surface of the composite wall by a radial gap, selected, in part, based on a difference between the first coefficient of thermal expansion and the second coefficient of thermal expansion. The radial gap is configured to change responsive to changes in temperature of the composite tank.

First claim

What is claimed is:

1. A composite tank for a reusable launch vehicle, the composite tank comprising:
a composite wall, having a first coefficient of thermal expansion, wherein the composite wall comprises:
a first end;
a second end;
a central axis, which passes through the first end and through the second end; and
a cylindrical interior surface;

slosh baffles, formed from a second material, having a second coefficient of thermal expansion that is different from the first coefficient of thermal expansion,
wherein:
each of the slosh baffles is attached to the cylindrical interior surface of the composite wall,
each of the slosh baffles is annular and is separated from the cylindrical interior surface of the composite wall by a radial gap, selected, in part, based on a difference between the first coefficient of thermal expansion and the second coefficient of thermal expansion, and

attachment assemblies, coupling the slosh baffles to the cylindrical interior surface of the composite wall, and each comprising:
a fitting with a slot and a baffle fastener that is movable within such slot to enable movement between the slosh baffles and the cylindrical interior surface, which changes the radial gap therebetween; and

ground straps, wherein each of the ground straps is electrically coupled to a respective one of the slosh baffles and to the composite wall.

2. A composite tank for a reusable launch vehicle, the composite tank comprising:
a composite wall, having a first coefficient of thermal expansion, wherein the composite wall comprises:
a first end;
a second end;
a central axis, which passes through the first end and through the second end; and
a cylindrical interior surface;

slosh baffles, formed from a second material, having a second coefficient of thermal expansion that is different from the first coefficient of thermal expansion,
wherein:
each of the slosh baffles is attached to the cylindrical interior surface of the composite wall,
each of the slosh baffles is annular and is separated from the cylindrical interior surface of the composite wall by a radial gap, selected, in part, based on a difference between the first coefficient of thermal expansion and the second coefficient of thermal expansion, and

the radial gap is configured to change responsive to changes in temperature of the composite tank; and
attachment assemblies, coupling the slosh baffles to the cylindrical interior surface of the composite wall, and each attachment assembly comprising:
stud assemblies, each bonded to the cylindrical interior surface of the composite wall;
a first fitting, attached to the stud assemblies; and
a second fitting, attached to the first fitting and comprising a second-fitting slot, extending radially relative to the cylindrical interior surface of the composite wall.

3. The composite tank according to claim 2 , further comprising a baffle fastener, protruding through the second-fitting slot and coupling the second fitting to a corresponding one of the slosh baffles.

4. The composite tank according to claim 2 , wherein:
a subset of the attachment assemblies couple a single one of the slosh baffles to the cylindrical interior surface of the composite wall; and
the subset of the attachment assemblies are evenly circumferentially spaced relative to one another along the cylindrical interior surface of the composite wall.

5. The composite tank according to claim 4 , wherein the subset of the attachment assemblies comprises at least three of the attachment assemblies.

6. The composite tank according to claim 2 , wherein each of the stud assemblies comprises a metallic base and a composite base, which overlaps at least a portion of the metallic base.

7. The composite tank according to claim 6 , wherein each of the stud assemblies further comprises a threaded rod, extending from the metallic base through the composite base and through the first fitting.

8. The composite tank according to claim 7 , wherein each of the stud assemblies further comprises a nut, threaded onto the threaded rod such the nut biases the first fitting against the composite base of each of the stud assemblies.

9. The composite tank according to claim 6 , wherein the metallic base of each of the stud assemblies is formed from a nickel-iron alloy.

10. The composite tank according to claim 6 , wherein the metallic base and the composite base collectively form a wall-facing surface of each of the stud assemblies and the wall-facing surface is adhesively coupled to the cylindrical interior surface of the composite wall.

11. The composite tank according to claim 2 , wherein:
the first fitting comprises a center portion and two arms, extending from the center portion in opposite directions along a first axis;
the center portion is attached to the second fitting; and
each of the two arms is attached to a respective one of the stud assemblies.

12. The composite tank according to claim 11 , wherein:
each of the two arms of the first fitting comprises a slot, and

a portion of a respective one of the stud assemblies protrudes through the slot.

13. The composite tank according to claim 11 , wherein:
the first fitting further comprises two additional arms, extending from the center portion, in opposite directions, along a second axis, perpendicular to the first axis,
each of the two additional arms is attached to a respective one of the stud assemblies.

14. The composite tank according to claim 2 , wherein each one of the attachment assemblies further comprises a fitting fastener that interconnects the first fitting and the second fitting.

15. The composite tank according to claim 14 , wherein the fitting fastener protrudes through the first fitting and through the second fitting.

16. The composite tank according to claim 2 , wherein:
each of the slosh baffles comprises a petal and a stiffener; and
the stiffener comprises a base, in contact with the petal, and a rib, extending from the base along the central axis; and
the second fitting is in contact with the base of the stiffener and is coupled to the base and to the petal.

17. The composite tank according to claim 16 , wherein:
each of the slosh baffles comprises a second stiffener,
the second stiffener comprises a second-stiffener base and a second-stiffener rib, extending from the second-stiffener base along the central axis, and
a portion of the petal is sandwiched between the base of the stiffener and the second-stiffener base.

18. The composite tank according to claim 2 , wherein each of the slosh baffles comprises a petal, a second petal, and a petal connector, overlapping a portion of the petal and a portion of the second petal and interconnecting the petal and the second petal.

19. The composite tank according to claim 2 , wherein the slosh baffles are evenly spaced from one another along the central axis.

20. The composite tank according to claim 2 , wherein:
the attachment assemblies are evenly circumferentially spaced relative to one another along the cylindrical interior surface of the composite wall.

Assignees

• Boeing Co

Inventors

• Embler Jonathan David
• Nichols John Matthew
• Torres Glenn William
• Szczudlak Jacob Ryan
• Keith William Preston
• Luu Tin Anh
• Lewis Morgan Ashley
• Kreutztrager Keith Charles
• Toomey Jonathan Edward
• Guzman Juan Carlos

Classifications

• Y10T29/49346

  Rocket or jet device making · CPC title

• F17C2270/0197

  Rockets · CPC title

• B60K2015/0775

  for reducing movement or slash noise of fuel · CPC title

• F17C2260/016

  Preventing slosh · CPC title

• B23P2700/01

  Aircraft parts · CPC title