Method for producing a corrugated foil bearing stiffener and obtained stiffener

Patent metadata

Field	Value
Publication number	US-10144098-B2
Application number	US-201414888534-A
Country	US
Kind code	B2
Filing date	Apr 29, 2014
Priority date	May 16, 2013
Publication date	Dec 4, 2018
Grant date	Dec 4, 2018

Abstract

A method for producing a corrugated foil bearing stiffener involves starting with an austenitic nickel superalloy sheet (15) having an elasticity limit higher than 500 MPa, and subjecting the sheet (15) to at least one step of press bending plastic deformation of the entire thickness of same with a deformation energy higher than 10 kJ in a time shorter than 10−5 s in such a way as to create corrugations.

First claim

The invention claimed is:

1. A method for producing a corrugated foil-bearing stiffener, comprising:
providing a sheet ( 15 ) of nickel-based austenitic metallic superalloy exhibiting a yield strength greater than 500 MPa; and
subjecting the sheet ( 15 ) to at least one step of plastic flexural deformation by stamping along an entire thickness of the sheet with a deformation energy greater than 10 kJ within a period shorter than 10 −5 s, so as to create flexural corrugations,
wherein in the course of said at least one step of plastic flexural deformation, the sheet ( 15 ) is subjected to a deformation energy of less than 35 kJ within a period longer than 10 −10 s,
wherein the sheet ( 15 ) is wound in the form of a cylindrical solid of revolution between an external die ( 17 ), exhibiting an internal cylindrical face ( 18 ) endowed with patterns ( 19 ) in the form of troughs corresponding to the corrugations to be formed, and a cylindrical punch ( 16 ) consisting of rubber elastomer, and
wherein said cylindrical punch ( 16 ) is axially compressed, the radial expansion of the cylindrical punch ( 16 ) bringing about the radial stamping of the sheet ( 15 ) in the die to form said flexural corrugations.

2. The method as claimed in claim 1 , wherein the sheet ( 15 ) is nickel-based austenitic metallic superalloy exhibiting a yield strength greater than 700 MPa, a tensile strength greater than 1000 MPa, and an elongation at break greater than 20%.

3. The method as claimed in claim 2 , wherein the sheet ( 15 ) is nickel-based austenitic metallic superalloy comprising between 5% and 9% iron, more than 70% nickel and cobalt, of which at most 1% is cobalt, between 14% and 17% chromium.

4. The method as claimed in claim 2 ,
wherein the sheet ( 15 ) is planar with a thickness between 0.05 mm and 0.4 mm, and
wherein flexural corrugations are produced having a height of each corrugation of between 0.2 mm and 1 mm, a length of each corrugation of between 3 mm and 10 mm, and a pitch between the corrugations of between 4 mm and 10 mm.

5. The method as claimed in claim 2 , wherein in the course of said at least one step of plastic flexural deformation, a coupling fold ( 23 ) is also realized, forming an outer edge ( 22 ) of the stiffener ( 13 ).

6. The method as claimed in claim 2 , wherein the sheet ( 15 ) is deformed by stamping in a direction at least normal to the sheet.

7. The method as claimed in claim 1 , wherein the sheet ( 15 ) is nickel-based austenitic metallic superalloy comprising between 5% and 9% iron, more than 70% nickel and cobalt, of which at most 1% is cobalt, between 14% and 17% chromium.

8. The method as claimed in claim 7 , wherein the nickel-based austenitic metallic superalloy has less than 0.08% carbon, less than 0.3% manganese, less than 0.5% silicon, less than 0.01% sulfur, between 0.4% and 1% aluminum, between 2.25% and 2.70% titanium, less than 0.5% copper, and between 0.7% and 1.2% niobium and tantalum.

9. The method as claimed in claim 7 ,
wherein the sheet ( 15 ) is planar with a thickness between 0.05 mm and 0.4 mm, and
wherein flexural corrugations are produced having a height of each corrugation of between 0.2 mm and 1 mm, a length of each corrugation of between 3 mm and 10 mm, and a pitch between the corrugations of between 4 mm and 10 mm.

10. The method as claimed in claim 1 ,
wherein the sheet ( 15 ) is planar with a thickness between 0.05 mm and 0.4 mm, and
wherein flexural corrugations are produced having a height of each corrugation of between 0.2 mm and 1 mm, a length of each corrugation of between 3 mm and 10 mm, and a pitch between the corrugations of between 4 mm and 10 mm.

11. The method as claimed in claim 1 , wherein in the course of said at least one step of plastic flexural deformation, a coupling fold ( 23 ) is also realized, forming an outer edge ( 22 ) of the stiffener ( 13 ).

12. The method as claimed in claim 1 , wherein the sheet ( 15 ) is deformed by stamping in a direction at least normal to the sheet.

13. The method as claimed in claim 1 , wherein said cylindrical punch ( 16 ) is axially compressed with the aid of at least one piston ( 20 ) having a mass greater than or equal to 200 g, which is driven axially at a speed greater than 10 m/s.

14. A method for producing a foil bearing, comprising:
producing a corrugated stiffener by implementation of the method as claimed in claim 1 , with a shape and dimensions configured for mounting directly in the foil bearing; and
mounting the produced corrugated stiffener in the foil bearing.

Assignees

• Liebherr Aerospace Toulouse Sas

Inventors

• Rocchi Jerome
• Grau Gregory
• Letrange Frederic

Classifications

• B21D15/02

  longitudinally · CPC title

• F16C33/14

  Special methods of manufacture; Running-in · CPC title

• F16C17/024 Primary

  with flexible leaves to create hydrodynamic wedge, e.g. radial foil bearings · CPC title

• B23P15/003 Primary

  bearings (see also F16C33/00) · CPC title