IP Library Granted Patent US 9,944,382
Granted Patent B2
US 9,944,382 · App. 14/489,635 · Granted Apr 17, 2018

Tightening and oil discharging nut, and a turbine engine

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Quick Facts
Patent No.
US 9,944,382
App. No.
14/489,635
Granted
Apr 17, 2018
Kind
B2
Abstract

A device for controlling the pitch of the blades of a rotor is provided. The device includes a radial shaft, the rotation of which controls the pitch of the blades; a guiding bearing for guiding the radial shaft; a nut which tightens the guiding bearing along the radial axis; and a circumferential rib extending as a protrusion towards the outside of the nut, for guiding a lubrication oil towards the outside of the nut.

Claims (26)

1. A device for controlling a pitch of blades of a rotor, comprising:

a radial shaft, wherein rotation of said radial shaft controls the pitch of the blades,

a guiding bearing, for guiding the radial shaft,

a nut configured to tighten the guiding bearing along a radial axis,

a circumferential rib extending as a protrusion towards an outside of the nut, for guiding a lubrication oil of the guiding bearing towards the outside of the nut, and

a circumferential groove capped by the circumferential rib, said circumferential groove comprising one or more oil discharge holes, for discharging oil out of the nut.

2. The device according to claim 1 , wherein the circumferential rib extends as a protrusion towards an inside of the nut.

3. The device according to claim 2 , comprising a circumferential cavity capped by a portion of the rib protruding towards the inside of the nut.

4. The device according to claim 3 , wherein:

the circumferential rib extends as a protrusion towards the inside of the nut so as to cap the cavity, and

the nut comprises one or more oil discharge holes facing the cavity,

so as to ensure guiding of the oil from the cavity towards the outside of the nut.

5. The device according to claim 1 , wherein:

the nut surrounds the radial shaft, and

a portion of the rib protruding towards an inside of the nut caps a junction area between the radial shaft and the nut.

6. The device according to claim 1 , wherein:

the nut comprises a circumferential joint in contact with a ferrule supporting the guiding bearing, and

a portion of the rib protruding towards the outside of the nut caps a contact area between the ferrule and the circumferential joint of the nut.

7. A turbine engine, comprising:

a rotor, comprising blades with variable pitch;

a device for controlling the pitch of the blades, according to claim 1 .

8. The turbine engine according to claim 7 , further comprising:

a first enclosure comprising air, and

a second pressurized enclosure, separated from the first enclosure by a ferrule having junction areas configured to allow oil to pass from the first enclosure to the second enclosure,

wherein:

the nut is configured for guiding the oil towards the first enclosure out of the junction areas.

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 Oct 14, 2014
From: BELMONTE, OLIVIER; PATSOURIS, EMMANUEL PIERRE DIMITRI
To: SNECMA
Reel/Frame 033943/0403 →