IP Library Granted Patent US 9,599,121
Granted Patent B2
US 9,599,121 · App. 14/436,199 · Granted Mar 21, 2017

Device and method for controlling the pitch of blades

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Quick Facts
Patent No.
US 9,599,121
App. No.
14/436,199
Granted
Mar 21, 2017
Kind
B2
Abstract

The invention concerns a device ( 1 ) for controlling the pitch of the blades of a fan ( 4 ) rotor ( 3 ), comprising a radial shaft ( 6 ) linked to the blade, a connection rod ( 8 ) of which the axial movement controls the rotation of the radial shaft ( 6 ), characterized in that it comprises:—a first part ( 10 ) that is mobile in rotation with the rotor ( 3 ) about the axis ( 11 ) of the fan ( 4 ), and on which one end of each connection rod ( 8 ) is secured,—a second part ( 12 ) linked to the first part ( 10 ), and—at least three cylinders ( 14 ) capable of moving said second part ( 12 ) in axial translation, and of varying the tilt of said second part, the translation and tilt of the second part ( 12 ) driving a corresponding translation and tilt of the first part ( 10 ), such that, when the first part ( 10 ) rotates, each connection rod ( 8 ) is subject to axial displacement of which the amplitude is variable and is a function of the tilt of the first part ( 10 ), making it possible to vary the pitch of the blade during the rotation of same. The invention also concerns a fan, and a method for controlling the pitch of blades.

Claims (19)

1. Device for controlling the pitch of the blades of a fan rotor comprising a radial shaft linked to the blade, a connecting rod the axial displacement of which controls rotation of the radial shaft, comprising:

a first part that is mobile in rotation with the rotor about the fan axis and on which one end of each connecting rod is secured,

a second part linked to the first part, and

at least three cylinders capable of moving said second part in axial translation and varying its tilt, translation and tilt of the second part leading to a corresponding translation and tilt of the first part,

such that when the first part rotates, each connecting rod follows an axial displacement with a variable amplitude that depends on the tilt of the first part in order to vary the pitch of the blade during its revolution.

2. Device according to claim 1 , in which the second part is linked to the first part by a mechanical bearing.

3. Device according to claim 1 , comprising a connecting bearing linking the cylinders to the rotor.

4. Device according to claim 3 , further comprising an elastic damper linking the cylinders to a duct of the fan.

5. Device according to claim 1 , in which the first part is linked to the rotor by connecting elements comprising a universal joint.

6. Device according to claim 5 , in which the connecting elements further comprise keys for axial guidance of the first part relative to the rotor.

7. Device according to claim 6 , comprising grooves complementary to the keys, one surface of which is tilted to enable cooperation with a tilted part of the rotor.

8. Device according to claim 1 , comprising stops limiting the tilt of the first and/or the second parts.

9. Fan of a turbomachine comprising:

at least one rotor and variable pitch blades, and a control device to set the pitch of its blades according to claim 1 .

10. Method for controlling the pitch of the blades of a fan rotor, using the control device, according to claim 1 , comprising a step consisting of controlling the cylinders to modify the tilt of the first part,

such that during rotation of the first part, each connecting rod is moved along an axial displacement with a variable amplitude that depends on the tilt of the first part, the blade pitch varying during its revolution about the axis of the fan.

11. Method according to claim 10 , comprising a step of imposing a tilt on the first part of a device of a rotor located on the upstream side of a fan that is different from the tilt of the first part of another device of a rotor located on the downstream side of the fan.

12. Method according to claim 11 , in which the step of imposing a tilt includes a step of fluctuating the tilt of the first part of the device or the upstream rotor or the downstream rotor about a nominal position.

13. Method according to claim 10 , comprising the step of fluctuating the tilt of the first part of the device at a frequency higher or lower than the rotation speed of the rotor.

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 23, 2015
From: FABRE, ADRIEN JACQUES PHILIPPE; LARTIGUE, NORBERT
To: SNECMA
Reel/Frame 036168/0456 →