IP Library Granted Patent US 7,395,655
Granted Patent B2
US 7,395,655 · App. 11/196,506 · Granted Jul 8, 2008

Regulator feeding control with two flow rate laws

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Quick Facts
Patent No.
US 7,395,655
App. No.
11/196,506
Granted
Jul 8, 2008
Kind
B2
Abstract

Hydromechanical regulator for controlling the flow of fuel injected into a turbomachine by means of a fuel feed unit ( 10 ), comprising a tachometric balance ( 20 ) having a beam consisting of two arms ( 24, 26 ), which beam can move about a pivot pin ( 22 ) under the action of at least a first force F 1 applied by a drive rod ( 18 ) of the fuel feed unit via a first elastic member ( 28 ), and a rod ( 36 ) associated with a drive piston ( 38 ) for applying, via a second elastic member ( 40 ), a force F 4 opposing the first force F 1 to the beam of the balance so as to cause the fuel feed unit to open further during the transition from a first engine acceleration law to a second engine acceleration law.

Claims (9)

1. A Hydromechanical regulator for controlling the flow of fuel injected into a turbomachine by means of a fuel feed unit ( 10 ), comprising

a force balance ( 20 ) having a beam consisting of two arms ( 24 , 26 ), which beam can move about a pivot pin ( 22 ) under the action of at least a first force (F 1 ) applied by a drive rod ( 18 ) of the fuel feed unit via a first elastic member ( 28 ), and

a rod ( 36 ) associated with a control piston ( 38 ) for applying, via a second elastic member ( 40 ), a force (F 4 ) opposing the first force to the beam of the balance so as to cause the fuel feed unit to open further during the transition from a first engine operating regime to a second engine operating regime,

wherein the rod of the control piston is furthermore coupled to an on/off pneumatic valve ( 44 ) for switching between the first engine operating regime and the second engine operating regime and connected, on one side, to a reference pressure P 0 and, on the other side, via air orifices S 0 and S 1 , to a pressure P 3 on the output side of a high-pressure compressor of the turbomachine.

2. A Hydromechanical regulator according to claim 1 , characterized in that the first force is applied to a fixed point on the first lever arm ( 24 ) at a distance L f from the pivot pin and in that the opposing force is applied to another fixed point on the first lever arm ( 24 ) at a distance L c from the pivot pin.

3. A Hydromechanical regulator according to claim 1 , characterized in that the pressure P 0 corresponds to the pressure on the inlet side of the high-pressure compressor or to atmospheric pressure.

4. A Hydromechanical regulator according to claim 1 , characterized in that one of the air orifices is adjustable in order to allow the second engine operating regime to be regulated.

5. A Fuel feed unit in conbination with the hydromechanical regulator of claim 1 for controlling the flow of fuel into a turbomachine, characterized in that the fuel feed unit includes a single feed opening ( 60 , 62 ) ensuring, for the flow of fuel injected into the turbomachine, a continuous variation upon passing from a first engine operating regime to a second engine operating regime.

6. A Turbomachine, which includes a hydromechanical regulator according to claim 1 .

Assignments (5)
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 Dec 17, 2012
From: SUIZA, HISPANO
To: SNECMA
Reel/Frame 029481/0429 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 4, 2011
From: SUIZA, HISPANO
To: SNECMA
Reel/Frame 027198/0499 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 25, 2005
From: POITOUT, SYLVAIN
To: HISPANO SUIZA
Reel/Frame 017138/0671 →