IP Library › Granted Patent US 12,135,092
Granted Patent B2
US 12,135,092 · App. 18/027,205 · Granted Nov 5, 2024

Fuel-isolation system having rupture diaphragm

Inventor: Matthew Jakubek (Seattle, WA)
Assignee: AEROJET ROCKETDYNE, INC.
F16K17/1626F16K31/002F16K17/1613H01M50/333H01M50/375
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Quick Facts
Patent No.
US 12,135,092
App. No.
18/027,205
Granted
Nov 5, 2024
Kind
B2
Abstract

A fuel-isolation system includes a valve body that defines a flow passage that extends from an inlet to an outlet, a rupture diaphragm in the flow passage and fluidly sealing the inlet from the outlet, and an actuator situated adjacent the rupture diaphragm. The rupture diaphragm is integral with the valve body. The actuator includes a plunger that is configured to move and cause breach of the rupture diaphragm and thereby fluidly connect the inlet and the inlet.

Claims (27)

1. A fuel-isolation system, comprising:

a valve body defining a flow passage extending from an inlet to an outlet, and in addition to the inlet and the outlet, the valve body defining a test port that opens into the flow passage and is fluidly connected with the outlet but not the inlet;

a rupture diaphragm integral to the valve body, the rupture diaphragm in the flow passage and fluidly sealing the inlet from the outlet;

an actuator situated adjacent the rupture diaphragm, the actuator including a plunger that is configured to move and cause breach of the rupture diaphragm and thereby fluidly connect the inlet and the outlet; and

a propellant tank having an outlet attached to or integral to the inlet of the valve body.

2. The fuel-isolation system as recited in claim 1 , wherein the actuator is a thermal actuator.

3. The fuel-isolation system as recited in claim 1 , wherein the actuator is a wax actuator.

4. The fuel-isolation system as recited in claim 1 , wherein the plunger is a piston.

5. The fuel-isolation system as recited in claim 1 , wherein the plunger is configured to pierce the rupture diaphragm.

6. The fuel-isolation system as recited in claim 1 , wherein the rupture diaphragm has at least one score line.

7. The fuel-isolation system as recited in claim 1 , wherein the rupture diaphragm is curved.

8. The fuel-isolation system as recited in claim 1 , further comprising a knife edge adjacent the rupture diaphragm and located on an opposite side of the diaphragm from the actuator.

9. The fuel-isolation system as recited in claim 1 , wherein the rupture diaphragm is welded to the valve body.

10. The fuel-isolation system as recited in claim 1 , wherein the rupture diaphragm is metallic.

11. The fuel-isolation system as recited in claim 1 , wherein the outlet contains a filter.

12. The fuel-isolation system as recited in claim 11 , wherein the outlet contains a venturi.

13. The fuel-isolation system as recited in claim 1 , further comprising a fuel tank connected with the inlet.

14. The fuel-isolation system as recited in claim 13 , wherein the propellant tank contains pressurized hydrazine.

15. A vehicle comprising the fuel isolation system as recited in claim 1 .

16. A fuel-isolation system, comprising:

a valve body defining a flow passage extending from an inlet to an outlet;

a test port that is fluidly connected with the outlet but not the inlet;

a rupture diaphragm integral to the valve body, the rupture diaphragm in the flow passage and fluidly sealing the inlet from the outlet;

an actuator situated adjacent the rupture diaphragm, the actuator including a plunger that is configured to move and cause breach of the rupture diaphragm and thereby fluidly connect the inlet and the outlet; and

a propellant tank having an outlet attached to or integral to the inlet of the valve body.

17. The fuel-isolation system as recited in claim 16 , wherein the actuator is a wax actuator.

18. The fuel-isolation system as recited in claim 17 , wherein the rupture diaphragm is curved.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 27, 2026
From: L3HARRIS TECHNOLOGIES, INC.; AEROJET ROCKETDYNE, INC.; AEROJET ROCKETDYNE OF DE, INC.; L3HARRIS CINCINNATI ELECTRONICS CORPORATION
To: ROCKETFORCE TECHNOLOGIES LLC
Reel/Frame 076068/0283 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 20, 2023
From: JAKUBEK, MATTHEW
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 063118/0626 →
Continuity (1)
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