IP Library Granted Patent US 9,115,647
Granted Patent B2
US 9,115,647 · App. 13/552,066 · Granted Aug 25, 2015

Method for monitoring a pressure relief valve of a fuel injection circuit for a turbomachine

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Quick Facts
Patent No.
US 9,115,647
App. No.
13/552,066
Granted
Aug 25, 2015
Kind
B2
Abstract

A detection method of a breakdown of a pressure relief valve of a fuel injection circuit for a turbomachine, the injection circuit including a low pressure stage and a high pressure stage, the low pressure stage having an inlet and an outlet, the high pressure stage having an inlet and an outlet, the low pressure stage being connected to the high pressure stage, the pressure relief valve being connected in parallel with respect to the high pressure stage, the injection circuit further including a recirculation loop including an inlet connected to the outlet of the high pressure stage and an outlet connected to the outlet of the low pressure stage, the method including measuring a differential pressure in the injection circuit.

Claims (8)

1. A detection method of a breakdown of a pressure relief valve of a fuel injection circuit for a turbomachine, the injection circuit including a fuel pump including a low pressure stage and a high pressure stage, the low pressure stage having an inlet and an outlet, the high pressure stage having an inlet and an outlet, the low pressure stage being connected to the high pressure stage, the pressure relief valve being connected in parallel with respect to the high pressure stage, the injection circuit further including a recirculation loop including an inlet connected to the outlet of the high pressure stage and an outlet connected to the outlet of the low pressure stage, the method comprising measuring a differential pressure in the injection circuit between the outlet of the recirculation loop and the inlet of the high pressure stage.

2. The detection method according to claim 1 , wherein the low pressure stage is connected to the high pressure stage with a duct.

3. The detection method according to claim 2 , wherein the differential pressure is measured between two points of the duct.

4. The detection method according to claim 1 , wherein the low pressure stage is connected to the high pressure stage using an equipment configured to generate a pressure drop, the differential pressure being measured at the terminal points of the equipment.

5. The detection method according to claim 4 , wherein the equipment is a fuel filter.

6. The detection method according to claim 5 , wherein the differential pressure is measured by a pressure difference sensor connected to the terminal points of the fuel filter.

7. The method according to claim 6 , comprising issuing a warning message when the pressure relief valve is locked in the open position.

8. The method according to claim 1 , comprising comparing the measured differential pressure in the injection circuit to a threshold value to determine whether the pressure relief valve is in a closed or open position.

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 Jul 18, 2012
From: ANDRE, BRICE; POTEL, NICOLAS
To: SNECMA
Reel/Frame 028581/0111 →