IP Library Granted Patent US 7,258,524
Granted Patent B2
US 7,258,524 · App. 11/279,812 · Granted Aug 21, 2007

Method of regulating the flow rate of air in a rotary shaft of a turbomachine

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,258,524
App. No.
11/279,812
Granted
Aug 21, 2007
Kind
B2
Abstract

A device applied to regulating the flow rate of air flowing in a rotary shaft of a turbomachine, the shaft including at least one through orifice for passing air. The device at least one shutter member for shutting the orifice and secured to a deformable blade presenting bi-linear behavior, the blade being secured to the shaft and being suitable for deforming under the effect of the centrifugal force that results from the shaft rotating such that the shutter member is suitable for taking up two different positions depending on the speed of rotation of the shaft: one position in which it shuts the orifice; and another position in which it releases the orifice to allow air to pass through.

Claims (7)

1. A device for regulating the flow rate of air flowing in a rotary shaft of a turbomachine, the shaft including at least one orifice passing therethrough to pass the air, the device comprising at least one shutter member for shutting the orifice and secured to a deformable blade presenting bi-linear behavior, the blade being secured to the shaft and being suitable for deforming under the effect of the centrifugal force that results from the shaft rotating such that the shutter member is suitable for taking up two different positions depending on the speed of rotation of the shaft: one position in which it shuts the orifice; and another position in which it releases the orifice to allow air to pass through.

2. A device according to claim 1 , wherein the deformable blade presents a right section that is curved perpendicularly to its direction of deformation.

3. A device according to claim 2 , wherein the section of the deformable blade that is curved is substantially parallel to an axis of rotation of the shaft.

4. A device according to claim 1 , further comprising an abutment element for enabling the shutter member to be held in position once it has released the orifice in the shaft.

5. A device according to claim 1 , wherein the deformable blade and the shutter member are located outside the shaft, the shutter member being disposed in such a manner as to shut the orifice in the shaft at a speed below a predetermined speed of rotation of the shaft, and to release the orifice at a speed above the predetermined speed of rotation.

6. A device according to claim 1 , wherein the deformable blade and the shutter member are located inside the shaft, the shutter member being disposed in such a manner as to release the orifice in the shaft at speeds below a predetermined speed of rotation of the shaft, and to open the orifice at speeds above the predetermined speed of rotation.

7. A turbomachine compressor shaft, including a device for regulating air flow rate according to claim 1 .

Assignments (2)
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 →