| SKF AEROSPACE FRANCE Patent applications |
| Patent application number | Title | Published |
|---|
| 20110277919 | METHOD OF MANUFACTURING A COMPOSITE PART, AND RESULTING PART - The invention relates to a method for manufacturing a composite part intended for being subjected, via at least one attachment point, to pulling and/or compression forces. The method includes: winding fibers on a hub so as to form a portion of the wall of the part, and creating an externally convex rounded area at the location intended to form the area for applying the pulling and/or compression forces. The forces are radial thereto. The method also includes placing an insert on the convex rounded area, the insert including the attachment point or a mechanism for rigidly connecting the attachment point, and continuing to wind fibers so as to form the rest of the wall, while covering a portion of the insert and leaving the attachment point or the mechanism for rigidly connecting the attachment point accessible. | 11-17-2011 |
| 20110272521 | FLIGHT UNIT CONTROL SYSTEM, FLIGHT CONTROL DEVICE INCLUDING SUCH A SYSTEM, AND USE OF SUCH A SYSTEM - The present invention relates to a flight unit control system (S), comprising at least one instrumented fastening bolt ( | 11-10-2011 |
| 20110214520 | FORCE TRANSMISSION ASSEMBLY AND A CONTROL ASSEMBLY INCLUDING SUCH AN ASSEMBLY - The invention relates to a force transmission unit ( | 09-08-2011 |
| 20110033225 | METHOD OF MANUFACTURING A LINK ROD FOR AERONAUTICAL CONSTRUCTION - According to this method, plastic welding is used to secure one longitudinal end ( | 02-10-2011 |
| 20090154990 | Light articulation ball-joint and method of manufacture of such a ball joint - The light articulation ball-joint comprises a metal inner ring and a metal outer ring, provided respectively with a spherical outer surface and a spherical inner surface. The ball-joint also comprises a first contact layer, applied to the spherical surface of one of the rings, and a second contact layer, applied to the spherical surface of the other ring. According to the invention, the first contact layer has a hardness which is less than the hardness of the second contact layer and a thickness which is greater than the thickness of the second contact layer, the first contact layer further being adapted to release particles of solid lubricant by friction with the second contact layer. | 06-18-2009 |
| 20090103998 | Anti-rotation lock device for a screwed assembly, an assembly including such a device, and the use of such an assembly in aircraft manufacture - This anti-rotation lock device ( | 04-23-2009 |
| 20090005184 | Shaft for transmitting rotational movements and/or forces - This shaft comprises firstly a tube made of a composite material having a plastic matrix and secondly a metallic tubular insert arranged fixedly around a longitudinal portion of the tube and designed to link the tube mechanically to a functional mechanical assembly which is supported by the insert and is for instance a pin. To significantly improve the mechanical performance of this shaft in torsion, the insert has in cross section a noncircular inner profile, for example an oblong shape, to which the outer surface of the tube is adapted in a substantially complementary manner. | 01-01-2009 |
