IP Library › Granted Patent US 12,234,794
Granted Patent B2
US 12,234,794 · App. 17/833,517 · Granted Feb 25, 2025

Jet fuel filter assembly

Inventor: Abdullah Mohammed Al-Zahrani (Jeddah, SA)
Assignee: SAUDI ARABIAN OIL COMPANY
F02M29/06B01D35/30
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Quick Facts
Patent No.
US 12,234,794
App. No.
17/833,517
Granted
Feb 25, 2025
Kind
B2
Abstract

Described is a jet fuel filter assembly. The jet fuel filter assembly includes an elongated filter cartridge and a filter element formed to fit within the bottom of the filter cartridge. The filter element consists of a hollow tube member and flow vanes extending from an interior wall of the hollow tube member toward a center of the hollow tube member. The flow vanes redirect jet fuel entering the filter cartridge in a helical path, thereby preventing premature rupturing of the filter cartridge due to jet fuel surges.

Claims (31)

1. A jet fuel filter assembly, comprising:

an elongated filter cartridge having a top, a bottom, a length extending from the top to the bottom, an exterior, an interior, and a diameter, the filter cartridge comprising a material having a plurality of pores, the filter cartridge formed to separate water from jet fuel entering the bottom of the filter cartridge; and

a filter element residing in only a bottom region of the filter cartridge, the filter element comprising:

a hollow tube member comprised of a durable material having a top, a bottom, a length extending from the top to the bottom, an interior wall, an exterior wall, and a diameter less than the diameter of the filter cartridge; and

a plurality of flow vanes extending from the interior wall of the hollow tube member toward a center of the hollow tube member,

wherein the plurality of flow vanes are positioned within the filter element to direct the jet fuel entering the bottom of the filter cartridge in a helical path through the filter element and upward toward the top of the filter cartridge, thereby reducing pressure of the jet fuel as the jet fuel travels through the filter cartridge from the bottom of the filter cartridge to the top of the filter cartridge,

wherein the durable material of the filter element is formed to physically block the plurality of pores in only the bottom region of the filter cartridge.

2. The jet fuel filter assembly as set forth in claim 1 , wherein the length of the hollow tube member is less than the length of the filter cartridge.

3. The jet fuel filter assembly as set forth in claim 1 , wherein each flow vane is substantially wing-shaped.

4. The jet fuel filter assembly as set forth in claim 1 , wherein the plurality of flow vanes are positioned along the length of the hollow tube member.

5. The jet fuel filter assembly as set forth in claim 1 , wherein the plurality of flow vanes are positioned proximate the bottom of the hollow tube member.

6. The jet fuel filter assembly as set forth in claim 1 , wherein the plurality of flow vanes are positioned symmetrically around the center of the hollow tube member along the interior wall.

7. The jet fuel filter assembly as set forth in claim 1 , wherein the plurality of flow vanes are comprised of a flexible material.

8. The jet fuel filter assembly as set forth in claim 2 , wherein the length of the hollow tube member is less than half of the length of the filter cartridge.

9. A jet fuel filtration system, comprising:

a filter vessel, having a top and a bottom, formed to receive jet fuel at the bottom;

a plurality of filter cartridges housed at the bottom of the filter vessel,

wherein each filter cartridge comprises a top, a bottom, a length extending from the top to the bottom, an exterior, an interior, and a diameter,

wherein each filter cartridge is comprised of a material having a plurality of pores and is formed to filter the jet fuel as the jet fuel travels from the filter vessel through each filter cartridge from the bottom of each filter cartridge to the top of each filter cartridge; and

a plurality of filter elements, each filter element formed to reside in only a bottom region of each filter cartridge,

wherein each filter element comprises:

a hollow tube member comprised of a durable material having a top, a bottom, a length extending from the top to the bottom, an interior wall, an exterior wall, and a diameter less than the diameter of each filter cartridge; and

a plurality of flow vanes extending from the interior wall of the hollow tube member toward a center of the hollow tube member,

wherein the durable material of each filter element is formed to physically block the plurality of pores in only the bottom region of each filter cartridge.

10. The jet fuel filtration system as set forth in claim 9 , wherein the length of the hollow tube member is less than the length of each filter cartridge.

11. The jet fuel filtration system as set forth in claim 9 , wherein each flow vane is substantially wing-shaped.

12. The jet fuel filtration system as set forth in claim 9 , wherein the plurality of flow vanes are positioned along the length of the hollow tube member.

13. The jet fuel filtration system as set forth in claim 9 , wherein the plurality of flow vanes are positioned proximate the bottom of the hollow tube member.

14. The jet fuel filtration system as set forth in claim 9 , wherein the plurality of flow vanes are positioned symmetrically around the center of the hollow tube member along the interior wall.

15. The jet fuel filtration system as set forth in claim 9 , wherein the plurality of flow vanes are comprised of a flexible material.

16. The jet fuel filtration system as set forth in claim 10 , wherein the length of the hollow tube member is less than half of the length of each filter cartridge.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 8, 2022
From: AL-ZAHRANI, ABDULLAH MOHAMMED
To: SAUDI ARABIAN OIL COMPANY
Reel/Frame 060141/0796 →
Continuity (1)
Related Publication 20230392568A1 · Dec 7, 2023
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