IP Library Granted Patent US 9,309,882
Granted Patent B2
US 9,309,882 · App. 14/344,777 · Granted Apr 12, 2016

Method of determining whether to replace a high pressure pump in a hydraulic regulation system of a turbomachine

Inventors: Nicolas Potel (Maisons Alfort, FR); Nicolas Gomes (Melun, FR)
Assignee: SNECMA
F04B51/00F04D27/001F04D29/563G01D5/2291G01M15/14
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Quick Facts
Patent No.
US 9,309,882
App. No.
14/344,777
Granted
Apr 12, 2016
Kind
B2
Abstract

A method tracking positive displacement efficiency of a high pressure positive displacement pump in a hydraulic regulator system of a turbomachine delivering a flow rate based on an engine speed of the turbomachine, the flow rate delivered to an actuator actuating variable geometry vanes of the turbomachine and to a bypass valve feeding engines of the turbomachine, the method including: starting engines of the turbomachine at a low engine speed, the valve being closed; using a computer to order a movement of the actuator; progressively increasing the engine speed until the flow rate reaches a predetermined value sufficient for opening the valve; storing in the computer a position of the actuator and the engine speed corresponding to opening of the valve; repeating the preceding operations at successive instants during a lifetime of the engines; and replacing the high pressure positive displacement pump when the engine speed exceeds a predetermined value.

Claims (9)

1. A method of determing when to replace a high pressure pump in a hydraulic regulator system of a turbomachine including a high pressure positive displacement pump delivering a flow rate that is a function of an engine speed of the turbomachine as defined by a control computer, the flow rate being delivered to an actuator for actuating variable geometry vanes of the turbomachine and to a bypass valve arranged in a feed pipe for feeding fuel to engines of the turbomachine, the method comprising:

starting the engines of the turbomachine at a low engine speed, the valve being closed;

using the control computer to order a movement of the actuator;

progressively increasing the engine speed until the flow rate reaches a predetermined value that is sufficient for opening the valve;

storing in the control computer a position of the actuator and the engine speed corresponding to the opening of the valve;

repeating the preceding operations at successive instants during a lifetime of the engines of the turbomachine; and

replacing the high pressure positive displacement pump when the engine speed exceeds a predetermined value.

2. The method according to claim 1 , wherein the position of the actuator is measured by an LVDT sensor of the actuator.

3. The method according to claim 1 , wherein the predetermined value for the flow rate corresponds to a rated threshold of a spring of the valve.

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 29, 2014
From: POTEL, NICOLAS; GOMES, NICOLAS
To: SNECMA
Reel/Frame 033408/0813 →
Priority Claims (1)
FR 11 58133 · Sep 13, 2011 · national
Continuity (1)
Related Publication 20140373611A1 · Dec 25, 2014