IP Library › Granted Patent US 12,313,081
Granted Patent B2
US 12,313,081 · App. 18/711,438 · Granted May 27, 2025

Module for mounting a turbomachine fan blade

Inventors: Caroline Marie Frantz (Moissy-Cramayel, FR); Vincent François Georges Millier (Moissy-Cramayel, FR); Jean Charles Olivier Roda (Moissy-Cramayel, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
F04D29/362B64C11/06F05D2220/36F05D2260/74
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Quick Facts
Patent No.
US 12,313,081
App. No.
18/711,438
Granted
May 27, 2025
Kind
B2
Abstract

Module for mounting a turbomachine fan blade, including: a blade force take-up device, a blade support able to pivot about a radial axis and configured to be engaged axially inside the device, the support and the device being mutually configured to ensure a clamping of the support against the device and an axial retention of the support inside the device; the support and the device each including, on their respective surfaces in cooperation, an alternation of conical seats and recesses making it possible alternatively, on the one hand, when the recesses of one surface are in geometric correspondence with the seats of the other surface, to axially slide the support relative to the device, and on the other hand, when the seats of both surfaces are in geometric correspondence with each other, to prevent any axial sliding movement of the support relative to the device.

Claims (20)

1. A module for mounting a turbomachine fan blade comprising:

a blade force take-up device,

a blade support intended to support a fan blade and able to pivot about a radial axis, the blade support being configured to be engaged axially along the radial axis inside the blade force take-up device, the blade support and the blade force take-up device being mutually configured to ensure both a clamping of the blade support against the device and an axial retention along the radial axis of the blade support inside the device in order to prevent any movement of axial disengagement of the blade support relative to the device, the blade support and the device each including, on their respective surfaces intended to cooperate with each other, an alternation of conical seats and recesses making it possible when the recesses of one of the two respective surfaces are in geometric correspondence with the conical seats of the other surface, to axially slide the blade support relative to the device and when the conical seats of the two respective surfaces are in geometric correspondence with each other, to prevent any axial sliding movement of the blade support relative to the device.

2. The mounting module according to claim 1 , wherein the blade force take-up device comprises an intermediate interface piece which includes, on an inner surface, a first plurality of conical seats disposed alternately with recesses circumferentially and coaxially with the radial axis of the blade support, the conical seats being oriented such that a top of the cone of each seat is directed towards a radial opening of the blade support.

3. The mounting module according to claim 2 , wherein the blade support includes, on an outer surface, a second plurality of conical seats disposed alternately with recesses circumferentially and coaxially with the radial axis of the blade support, the conical seats of the second plurality of conical seats having a same orientation as that of the first plurality of conical seats.

4. The mounting module according to claim 1 , wherein the mounting module includes at least one angular setting member on a first element of two elements among the blade support and the device, said at least one angular setting member being intended to cooperate with an angular setting pocket arranged on a second element of the two elements and extending transversely relative to the radial axis.

5. A variable-setting assembly for a turbomachine fan, comprising:

a hub extending circumferentially about a longitudinal axis of rotation of the hub and comprising a plurality of hub mouths distributed circumferentially on an outer periphery of the hub, each hub mouth internally delimiting an opening oriented radially relative to the longitudinal axis and allowing access to an inside of the hub mouth,

for each hub mouth, a module for mounting a fan blade according to claim 1 .

6. The assembly according to claim 5 , wherein it includes an eccentric system for controlling the pivoting of the blade support, which is configured to control the pivoting of the blade support about the radial axis of the hub mouth.

7. The assembly according to claim 6 , wherein the eccentric system for controlling the pivoting of the blade support comprises a piece forming an eccentric which is configured to engage with a lower part of the blade support which is opposite to an upper part of the blade support disposed in a radial position remote from the longitudinal axis and intended to receive a fan blade.

8. The assembly according to claim 7 , wherein the lower part of the blade support carries outer splines which are configured to mesh with inner splines of an engagement end of the eccentric.

9. The assembly according to claim 8 , wherein the engagement end of the eccentric has a general shape of a cylindrical pad open at its upper part oriented towards the radial opening of the mouth and which is provided, on its internal surface, with the inner splines.

10. The assembly according to claim 8 , wherein the outer splines of the lower part of the blade support are disposed at a distance, taken along the radial axis, from the conical seats of the blade support which is such that the outer splines are in geometric correspondence with the inner splines of the engagement end when the respective conical seats of the blade support and of the device are in geometric correspondence with each other.

11. The assembly according to claim 5 , wherein the mounting module includes at least one angular setting member on a first element of two elements among the blade support and the device, said at least one angular setting member being intended to cooperate with an angular setting pocket arranged on a second element of the two elements and extending transversely relative to the radial axis, the conical seats of the blade support being disposed between the angular setting member or angular setting pocket, depending on whether the member is carried by the blade support or the device, and outer splines.

12. The assembly according to claim 8 , wherein the engagement end of the eccentric is also configured to be removably mechanically coupled with a lower part of the hub mouth which is opposite to the radial opening of the latter.

13. The assembly according to claim 12 , wherein the engagement end of the eccentric includes an assembly of double concentric cylindrical walls open at its upper part towards the radial opening of the mouth and comprising both a first outer wall which is removably mechanically coupled with the lower part of the mouth and a second inner wall which is provided on its inner face with the splines configured to mesh with the outer splines of the lower part of the blade support.

14. A turbomachine fan, wherein it comprises a variable-setting assembly for a turbomachine fan according to claim 5 .

15. The turbomachine fan according to claim 14 , wherein the fan comprises a plurality of fan blades each mounted on a blade support of a mounting module of a hub mouth.

16. A turbomachine comprising a turbomachine fan according to claim 14 .

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 3, 2024
From: FRANTZ, CAROLINE MARIE; MILLIER, VINCENT FRANÇOIS GEORGES; RODA, JEAN CHARLES OLIVIER
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 067600/0756 →
Priority Claims (1)
FR 2112278 · Nov 19, 2021 · national
Continuity (1)
Related Publication 20250020139A1 · Jan 16, 2025
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Cited By (4)
US 12,692,873 US 12,709,398 US 12,735,188 US 12,741,747