Patent classifications
B23Q35/26
Automated jigsaw
A system for making curved cuts of a work piece, the system including a template including a profiled groove spanning from a first end to a second end, the groove dividing the template into distal and proximal halves, at least one profile of a curved cut is part of the groove; a saw including a saw blade; a turntable including a platform and a base upon which the platform is rotatably supported; and a mobility mechanism to which the platform is attached, the mobility mechanism is configured to allow the turntable to traverse between the two ends and a direction transverse to a direction defined by the two ends, wherein the work piece is disposed under the groove of the template and the saw blade is configured to be guided through the groove to cut the work piece according to the at least one profile of a curved cut.
AUTOMATED JIGSAW
A system for making curved cuts of a work piece, the system including a template including a profiled groove spanning from a first end to a second end, the groove dividing the template into distal and proximal halves, at least one profile of a curved cut is part of the groove; a saw including a saw blade; a turntable including a platform and a base upon which the platform is rotatably supported; and a mobility means to which the platform is attached, the mobility means is configured to allow the turntable to traverse between the two ends and a direction transverse to a direction defined by the two ends, wherein the work piece is disposed under the groove of the template and the saw blade is configured to be guided through the groove to cut the work piece according to the at least one profile of a curved cut.
Method for machining an attachment flange of an aircraft turbomachine case
A method of machining an attachment flange of an aircraft turbomachine case, the method also including a system to machine the two opposite surfaces of the flange, and including a shape follower machining module, this module being designed to follow the shape of the flange and including a first structure equipped with a first machining tool, and a second structure equipped with a second machining tool, the flange fitting between the structures such that its two opposite surfaces are machined by tools, the module also including shape follower elements carried by the structures; and a device to drive movement of the machining module along a circumferential direction of the flange.
Method for machining an attachment flange of an aircraft turbomachine case
A method of machining an attachment flange of an aircraft turbomachine case, the method also including a system to machine the two opposite surfaces of the flange, and including a shape follower machining module, this module being designed to follow the shape of the flange and including a first structure equipped with a first machining tool, and a second structure equipped with a second machining tool, the flange fitting between the structures such that its two opposite surfaces are machined by tools, the module also including shape follower elements carried by the structures; and a device to drive movement of the machining module along a circumferential direction of the flange.
METHOD FOR MACHINING AN ATTACHMENT FLANGE OF AN AIRCRAFT TURBOMACHINE CASE
A method of machining an attachment flange of an aircraft turbomachine case, the method also including a system to machine the two opposite surfaces of the flange, and including a shape follower machining module, this module being designed to follow the shape of the flange and including a first structure equipped with a first machining tool, and a second structure equipped with a second machining tool, the flange fitting between the structures such that its two opposite surfaces are machined by tools, the module also including shape follower elements carried by the structures; and a device to drive movement of the machining module along a circumferential direction of the flange.
METHOD FOR MACHINING AN ATTACHMENT FLANGE OF AN AIRCRAFT TURBOMACHINE CASE
A method of machining an attachment flange of an aircraft turbomachine case, the method also including a system to machine the two opposite surfaces of the flange, and including a shape follower machining module, this module being designed to follow the shape of the flange and including a first structure equipped with a first machining tool, and a second structure equipped with a second machining tool, the flange fitting between the structures such that its two opposite surfaces are machined by tools, the module also including shape follower elements carried by the structures; and a device to drive movement of the machining module along a circumferential direction of the flange.