IP Library Granted Patent US 10,830,628
Granted Patent B2
US 10,830,628 · App. 15/969,134 · Granted Nov 10, 2020

Oil level sensor tank for turbine engine

Inventors: Florian Cleyet (Liege, BE); Alain Beaujean (Oreye, BE); Stéphane Bougelet (Profondeville, BE)
Assignee: SAFRAN AERO BOOSTERS SA
G01F23/22B64D37/02B64D37/04B64D37/06F01D25/18F01M11/12F16N19/003G01F23/0061G01F23/26F05D2220/30F05D2230/60F05D2260/98F16N2210/02F16N2250/18G01F23/24G01F23/263
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Quick Facts
Patent No.
US 10,830,628
App. No.
15/969,134
Granted
Nov 10, 2020
Kind
B2
Abstract

An oil tank of a turbine engine, particularly of an aircraft turbojet includes an external wall forming a generally curved main cavity. This cavity includes an arched sensor for electrically measuring the oil level, for example in a capacitive manner. Said arched sensor matches the curvature of the main cavity in order to be integrated therein. Sensor supporting arms distributed along the curvature of the arched sensor and/or an arched sleeve with an arched cavity receive the arched sensor. A turbine engine is provided with an oil tank, as well as a method for mounting a sensor in an oil tank.

Claims (17)

1. An oil tank assembly for a turbine engine, comprising:

an external wall forming a generally curved main cavity;

an arched sensor for electrically measuring an oil level within the main cavity, said arched sensor matching the curvature of the main cavity; and

an arched sleeve within which the arched sensor is disposed, wherein the sleeve is hinged through pivot connections.

2. Assembly according to claim 1 , wherein the sleeve is directly connected to the external wall.

3. An oil tank assembly for a turbine engine, comprising:

an external wall forming a generally curved main cavity;

an arched sensor for electrically measuring an oil level within the main cavity, said arched sensor matching the curvature of the main cavity; and

an arched sleeve within which the arched sensor is disposed, wherein the sleeve comprises:

cut-outs, wherein the cut-outs divide the sleeve into several segments that are mobile with respect to one another.

4. Assembly according to claim 3 , wherein the sleeve is directly connected to the external wall.

5. Method for mounting a liquid level sensor in a tank of a turbine engine, the method comprising:

(a) providing a tank with an external wall forming a generally curved main cavity;

(b) providing an electrical, level measuring sensor that is arched along a radius of curvature, and disposing sensor supporting arms or an arched sleeve inside the main cavity;

(c) inserting the sensor into the cavity while contacting the sensor supporting arms and/or with the arched sleeve such as to match the curvature of the cavity,

wherein during the insertion step (c), the sensor retains its radius of curvature.

6. Method according to claim 5 , wherein the tank comprises an opening, particularly a filling upper opening, and during the insertion step (c), the arched sensor is inserted via said opening.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 15, 2018
From: CLEYET, FLORIAN; BOUGELET, STÉPHANE; BEAUJEAN, ALAIN
To: SAFRAN AERO BOOSTERS SA
Reel/Frame 046101/0775 →
Priority Claims (1)
BE 2017/5310 · May 3, 2017 · national
Continuity (1)
Related Publication 20180321073A1 · Nov 8, 2018