IP Library Granted Patent US 8,443,654
Granted Patent B2
US 8,443,654 · App. 13/163,141 · Granted May 21, 2013

Device for monitoring the obstruction of at least two filters of a fluid circulation system of an aircraft gas turbine engine

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Quick Facts
Patent No.
US 8,443,654
App. No.
13/163,141
Filed
Jun 17, 2011
Granted
May 21, 2013
Kind
B2
Art Unit
2856
USPC
73/112.01
Abstract

A device monitors an obstruction of two fluid filters of a fluid circulation system of a gas turbine engine of an aircraft. A first obstruction sensor sends a first detection signal of an obstruction of a first filter. A second obstruction sensor sends a second detection signal of an obstruction of a second filter. A processor includes a monitoring input to measure the first and second detection signals. The first obstruction sensor includes a Wheatstone bridge including a strain gauge resistor. The second obstruction sensor is connected in parallel with the strain gauge resistor. The first detection signal is sent over a first predetermined variation range. The second detection signal is sent over a second predetermined variation range, distinct from the first variation range. The processor identifies the obstruction of one of the fluid filters as a function of one of the variation ranges of the detection signals.

Claims (17)

1. A device for monitoring an obstruction of at least two fluid filters of a fluid circulation system of a gas turbine engine of an aircraft, the device comprising:

a first obstruction sensor to monitor a first fluid filter, and set up to send a first detection signal of an obstruction of the first filter, the first obstruction sensor including a Wheatstone bridge comprising at least one strain gauge resistor;

a processor comprising a monitoring input linked to said first sensor to measure the first detection signal; and

a second obstruction sensor to monitor a second fluid filter, and set up to send a second detection signal of an obstruction of the second filter, said monitoring input of the processor being connected to the second obstruction sensor to measure said second detection signal, the second obstruction sensor being connected in parallel with said strain gauge resistor;

wherein the first detection signal is sent over a first predetermined variation range, the second detection signal is sent over a second predetermined variation range, distinct from said first variation range, and the processor is set up to identify the obstruction of one of the fluid filters as a function of one of the variation ranges of the first and second detection signals measured at the monitoring input.

2. The device according to claim 1 , wherein the second obstruction sensor is linked to the first obstruction sensor such that the second detection signal from the second obstruction sensor is incorporated into the first detection signal of the first obstruction sensor.

3. The device according to claim 1 , wherein the second obstruction sensor is a passive sensor and comprises an electrical contact.

4. The device according to claim 1 , wherein the second obstruction sensor is a proximity sensor.

5. A device for monitoring an obstruction of at least two fluid filters of a fluid circulation system of a gas turbine engine of an aircraft, the device comprising:

a first obstruction sensor to monitor a first fluid filter, and set up to send a first detection signal of an obstruction of the first filter;

a processor comprising a monitoring input linked to said first sensor to measure the first detection signal;

a second obstruction sensor to monitor a second fluid filter, and set up to send a second detection signal of an obstruction of the second filter, said monitoring input of the processor being connected to the second obstruction sensor to measure said second detection signal; and

a fusion block of said detection signals set up to

receive as an input the first detection signal from the first obstruction sensor and the second detection signal from the second obstruction sensor; and

send the first detection signal and the second detection signal alternately to the monitoring input of the processor, wherein

the first detection signal is sent over a first predetermined variation range, the second detection signal is sent over a second predetermined variation range, distinct from said first variation range, and the processor is set up to identify the obstruction of one of the fluid filters as a function of one of the variation ranges of the first and second detection signals measured at the monitoring input.

6. The device according to claim 5 , wherein the second obstruction sensor is a Wheatstone bridge.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 17, 2011
From: BADER, NICOLAS ALAIN; POIX, THIERRY; POTEL, NICOLAS
To: SNECMA
Reel/Frame 026464/0414 →