EP1378634A2
|
|
Method of producing a bearing housing from a worn housing, and fixture implementing such a method
|
CA2411873A1
|
|
Bladed member, in particular for an axial turbine of an aircraft engine
|
US2003017051A1
|
|
Double-wall blade for a turbine, particularly for aeronautical applications
|
CA2378092A1
|
|
Method of detecting the position of an inner surface of a workpiece on a machine tool, and machine tool implementing such a method
|
EP1113193A2
|
|
Aircraft gear transmission
|
EP1189156A1
|
|
Computer-assisted design system
|
EP1070663A2
|
|
Drive system for a tiltrotor aircraft
|
CA2298144A1
|
|
Pin for connecting gears to a supporting member, and transmission featuring such a pin
|
EP0994280A2
|
|
Face gear transmission assembly, in particular for aircraft application
|
CA2256147A1
|
|
Gear-drive assembly
|
EP0971155A1
|
|
Face-gear transmission assembly with floating balance pinions
|
CA2240752A1
|
|
Face-gear transmission assembly with floating balance pinions
|
US6325109B1
|
|
Method and machine for producing a continuous-thread disk element, and disk element produced using such a method
|
EP0666140A1
|
|
A method and a machine for working a blade sector
|
EP0663256A1
|
|
A method and a machine for manufacturing crown or face gears
|
ITTO940749D0
|
|
Supporting device with oscillating bearing, particularly for connecting toothed gears to a supporting part
|
US5572910A
|
|
Application of face gears to helicopter transmissions
|
ITTO930686D0
|
|
Torque splitter applied to mechanical transmissions built with face gears
|