IP Library Granted Patent US 11,358,732
Granted Patent B2
US 11,358,732 · App. 16/380,358 · Granted Jun 14, 2022

Anti-overpressure fuel tank

Inventors: Patrick Epalle (Saint Chamond, FR); Michel Vacher (Roche la Moliere, FR)
Assignee: Zodiac Aerotechnics
B64D37/32B64D37/02F16K24/048F16K31/22B60K15/03519B60K2015/03289
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Quick Facts
Patent No.
US 11,358,732
App. No.
16/380,358
Granted
Jun 14, 2022
Kind
B2
Abstract

A fuel tank with a venting system includes a flap for closing and opening a vent made in the tank. The flap is coupled to a float. The flap includes a valve coupled to a second float mounted in a hinged manner in the tank so that the valve adopts a closed position, being pushed by the second float when the level of fuel in the tank reaches a certain threshold, and an open venting position in order to prevent overpressure within the tank, being driven by the second float when the level of fuel is below the threshold and the force exerted by the internal pressure on the valve is less than the sum of the forces exerted on the valve by the atmospheric pressure and by the weight of the second float.

Claims (9)

1. A fuel tank comprising:

a tank;

a venting system of said tank comprising:

a float mounted in a hinged manner in said tank;

a flap mechanically coupled to said float, said flap to close an opening in said tank in a closed flap position;

a valve disposed in said flap, said valve mechanically coupled to a second float mounted in a hinged manner in said tank, said valve comprising an open valve position to open an orifice in said flap and a closed valve position to close said orifice in said flap;

wherein said valve adopts a closed position, being pushed by the second float when a level of fuel in the tank reaches a certain threshold; and

wherein said valve adopts an open venting position during the closed flap position in order to prevent overpressure within said tank, being driven by the second float when the level of fuel is below said threshold and a force exerted by an internal pressure on the valve is less than a sum of forces exerted on said valve by an atmospheric pressure and by a weight of the second float.

2. The fuel tank according to claim 1 , wherein the second float is subjected to the valve by means of an arm forming a lever in order to increase the force exerted by the second float on the valve.

Assignments (4)
CORRECTIVE ASSIGNMENT TO CORRECT THE THE PREVIOUS RECORDED ASSIGNMENT PREVIOUSLY RECORDED AT REEL: 68238 FRAME: 929. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Apr 3, 2025
From: SAFRAN AEROTECHNICS
To: SAFRAN AEROSYSTEMS
Reel/Frame 070721/0187 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 9, 2024
From: SAFRAN AEROTECHNICS
To: SAFRAN AEROSYSTEMS
Reel/Frame 068238/0928 →
CHANGE OF NAME Recorded Jun 7, 2021
From: ZODIAC AEROTECHNICS
To: SAFRAN AEROTECHNICS SAS
Reel/Frame 056495/0329 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 14, 2019
From: EPALLE, PATRICK; VACHER, MICHEL
To: ZODIAC AEROTECHNICS
Reel/Frame 049468/0424 →
Priority Claims (1)
FR 1550916 · Feb 5, 2015 · national
Continuity (2)
Division 15545090
Related Publication 20190233131A1 · Aug 1, 2019