IP Library Granted Patent US 10,293,953
Granted Patent B2
US 10,293,953 · App. 15/545,090 · Granted May 21, 2019

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 10,293,953
App. No.
15/545,090
Granted
May 21, 2019
Kind
B2
Abstract

The invention relates to a tank for receiving fuel, said tank comprising a venting system comprising a flap for closing an opening made in the tank, said flap being subjected to a float and mounted in a hinged manner in the tank so as to adopt a closed position, pushed by the float when the level of fuel in the tank reaches a certain threshold, and an open, venting position, driven by the float when the level of fuel is below said threshold. According to the invention, the flap comprises a valve controlled by means that can open the valve when the flap is in a closed position and the level of fuel is below said threshold.

Claims (8)

1. An anti-overpressure 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 comprising a rod mounted sliding within an orifice of said flap, said valve comprising an open valve position and a closed valve position, said rod comprising a first end with a shoulder intended to act as a stop for the closed valve position of said rod to block said orifice, and a second end with another shoulder forming a seat for a compression spring arranged around said rod and pressed against said flap to spring bias said rod in the closed valve position;

wherein the flap adopts the flap closed position, by being pushed by said float when a level of fuel in the tank reaches a certain threshold, and an open flap venting position, by being driven by the float when the level of fuel is below said certain threshold; and

wherein said tank is vented when a force exerted by an internal pressure on said valve exceeds a sum of forces exerted on said valve by an atmospheric pressure and by said compression spring, and said valve is pushed into the open valve position against said compression spring.

Assignments (4)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 8, 2024
From: SAFRAN AEROTECHNICS
To: SAFRAN AEROSYSTEMS
Reel/Frame 069124/0604 →
CORRECTIVE ASSIGNMENT TO CORRECT THE THE NAME OF RECEIVING PARTY, SAFRAN AEROTECHNICS SAS; PLEASE REMOVE 'SAS' FROM THE NAME PREVIOUSLY RECORDED ON REEL 055556 FRAME 0867. ASSIGNOR(S) HEREBY CONFIRMS THE SAFRAN AEROTECHNICS. Recorded May 25, 2022
From: ZODIAC AEROTECHNICS
To: SAFRAN AEROTECHNICS
Reel/Frame 060177/0282 →
CHANGE OF NAME Recorded Jan 26, 2021
From: ZODIAC AEROTECHNICS
To: SAFRAN AEROTECHNICS SAS
Reel/Frame 055556/0867 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 6, 2017
From: EPALLE, PATRICK; VACHER, MICHEL
To: ZODIAC AEROTECHNICS
Reel/Frame 043806/0088 →
Priority Claims (1)
FR 15 50916 · Feb 5, 2015 · national
Continuity (1)
Related Publication 20180009544A1 · Jan 11, 2018