The invention relates to a method for manufacturing an inlet lip skin part according to a nominal definition comprising dimensions of the lip skin and associated tolerances, the method comprising the steps of: a) obtaining at least one blank from at least one metal sheet; b) deforming the at least one blank into an intermediate part; and c) machining a first surface of the intermediate part with a first machining path, said first machining path being independent of the real dimensions of the intermediate part, and being based on the nominal definition of the lip skin part, so as to obtain a semi-machined part, and d) machining a second surface of the semi-machined part with a second machining path, said second machining path being based on real dimensions of the semi-machined part and the nominal definition of the lip skin part.

A method and a device for manufacturing a part starting from a cushion made of deformable material, in particular for an edge of an element of an aircraft. The device includes a preparation unit to create a cushion with two plates and, between the plates, an internal space with an opening, and a molding unit comprising a mold in which the cushion is positioned, the mold comprising two shells and an imprint corresponding to the shape of the part to be manufactured, the molding unit configured to inject a pressurized fluid into the internal space of the cushion through the opening to deform the cushion such that it matches the imprint and forms the part, the device being capable of manufacturing one-piece parts of various sizes, and in particular parts having complex shapes, in particular non-developable shapes.

A tolerance ring including a sidewall having a first and a second opposite major surfaces spaced apart by a thickness, wherein the first major surface defines an inner diameter of the tolerance ring at a first location of the sidewall and an outer diameter of the tolerance ring at a second location of the sidewall. A method of forming a tolerance ring including providing a strip of material comprising a first, a second, a third, and a fourth edge, shaping the first edge of the strip toward the third edge, and shaping the second edge of the strip toward the fourth edge.

A tolerance ring including a sidewall having a first and a second opposite major surfaces spaced apart by a thickness, wherein the first major surface defines an inner diameter of the tolerance ring at a first location of the sidewall and an outer diameter of the tolerance ring at a second location of the sidewall. A method of forming a tolerance ring including providing a strip of material comprising a first, a second, a third, and a fourth edge, shaping the first edge of the strip toward the third edge, and shaping the second edge of the strip toward the fourth edge.

Machine (10) for the production of coiled gaskets from continuous strips, i.e. a master backing strip (1a) and sealing filler strip (1b), to be spirally wound onto rings, templates or inner rings (11), comprising at least: means (2) for feeding the strips (1a,1b) to be wound, a unit (100) for straightening and forming the backing strip (1a), a unit (200) for making incisions in and cutting the backing strip (1a), arranged downstream of the forming unit (100), a unit (300) for joining together the master strip (1a) and filler strip (1b) so as to form a combined strip (1) and cutting the filler strip (1b), a rotating spindle unit (400) for winding the combined strip (1), arranged downstream of the strip joining unit (300); a unit (500) for driving the ring or inner-ring (11) arranged downstream of the spindle (400), and a unit (600) for welding the master strip (1a), said units being designed to be able to produce automatically and in sequence a finished gasket, in accordance with a program managed by means (1000) for programming, controlling and actuating the operations.

Machine (10) for the production of coiled gaskets from continuous strips, i.e. a master backing strip (1a) and sealing filler strip (1b), to be spirally wound onto rings, templates or inner rings (11), comprising at least: means (2) for feeding the strips (1a,1b) to be wound, a unit (100) for straightening and forming the backing strip (1a), a unit (200) for making incisions in and cutting the backing strip (1a), arranged downstream of the forming unit (100), a unit (300) for joining together the master strip (1a) and filler strip (1b) so as to form a combined strip (1) and cutting the filler strip (1b), a rotating spindle unit (400) for winding the combined strip (1), arranged downstream of the strip joining unit (300); a unit (500) for driving the ring or inner-ring (11) arranged downstream of the spindle (400), and a unit (600) for welding the master strip (1a), said units being designed to be able to produce automatically and in sequence a finished gasket, in accordance with a program managed by means (1000) for programming, controlling and actuating the operations.

A tolerance ring including a sidewall having a first and a second opposite major surfaces spaced apart by a thickness, wherein the first major surface defines an inner diameter of the tolerance ring at a first location of the sidewall and an outer diameter of the tolerance ring at a second location of the sidewall. A method of forming a tolerance ring including providing a strip of material comprising a first, a second, a third, and a fourth edge, shaping the first edge of the strip toward the third edge, and shaping the second edge of the strip toward the fourth edge.

A tolerance ring including a sidewall having a first and a second opposite major surfaces spaced apart by a thickness, wherein the first major surface defines an inner diameter of the tolerance ring at a first location of the sidewall and an outer diameter of the tolerance ring at a second location of the sidewall. A method of forming a tolerance ring including providing a strip of material comprising a first, a second, a third, and a fourth edge, shaping the first edge of the strip toward the third edge, and shaping the second edge of the strip toward the fourth edge.

A medical examination or treatment facility includes a C-arm, arranged on a support bracket of a robot configured to move the C-arm in space. In an embodiment, the C-arm is made up of a plurality of arm elements in the form of sheet metal parts and at least one coupling unit including at least one cast metal part for coupling the C-arm to the support bracket.

Machine (10) for the production of coiled gaskets from continuous strips, i.e. a master backing strip (1a) and sealing filler strip (1b), to be spirally wound onto rings, templates or inner rings (11), comprising at least: means (2) for feeding the strips (1a,1b) to be wound, a unit (100) for straightening and forming the backing strip (1a), a unit (200) for making incisions in and cutting the backing strip (1a), arranged downstream of the forming unit (100), a unit (300) for joining together the master strip (1a) and filler strip (1b) so as to form a combined strip (1) and cutting the filler strip (1b), a rotating spindle unit (400) for winding the combined strip (1), arranged downstream of the strip joining unit (300); a unit (500) for driving the ring or inner-ring (11) arranged downstream of the spindle (400), and a unit (600) for welding the master strip (1a), said units being designed to be able to produce automatically and in sequence a finished gasket, in accordance with a program managed by means (1000) for programming, controlling and actuating the operations.