A mobile machine tool for segmentally machining, in situ, a component, in particular a component of a turbine, which is rotatable about an axis of rotation. The machine tool has a main body, a support element which is held on the main body so as to be movable about a C-axis along a circular-arc-shaped guide path, and a tool module which is held on the support element and is designed to receive a tool. The tool module is located on the support element so as to be linearly movable. A method segmentally machines, in-situ, a component which is mounted in a stationary body so as to be rotatable about an axis of rotation.

During an assembly process for an aircraft, segments of the fuselage are fabricated separately prior to joining the segments together to form the complete fuselage. In order to ensure that abutting ends of the segments mate together correctly, a machining process is performed along the edges of the segments at their ends. A trim-tool assembly includes an indexing cart mounted to a track secured to a surface of the workpiece, where a setting on the indexing cart varies a distance between a centerline of the track and an edge of a workpiece. The trim-tool assembly further includes a tool cart mounted to the track and translatable along the track. The tool cart includes a process tool that performs a machining process on the workpiece at a fixed distance from the centerline of the track.

A tool cabinet includes a cabinet body having two guide rails and a routing space that is proximate to one of the guide rails, a working platform unit having a protective tube, two lifting units, a driving unit, and a power supply unit having a transmission wire. The working platform unit includes two extension members respectively slidable relative to the guide rails. Each lifting units includes a threaded rod extending through a respective extension member. The driving unit is disposed for driving rotation of the threaded rod of a respective one of the lifting units. The transmission wire has an end connected to the driving unit, and an opposite end extending through the protective tube into the routing space.

In one example, an on-wing method for in-situ cutting on a wing-to-fuselage attachment includes attaching a first mount plate having a first linear bearing to provide movement in a first linear direction relative to the first mount plate, attaching a second mount plate having a second linear bearing to provide movement in a second linear direction relative to the second mount plate, attaching a tool mounting member to the second linear bearing to move with the second linear bearing, attaching a cutter to the tool mounting member to be adjustable relative to the second linear bearing, adjusting a depth position of a cut to be made on the wing-to-fuselage attachment, adjusting a width position of the cut, and moving the tool along a length direction of the cut to make the cut on the wing-to-fuselage attachment along the length direction at the adjusted depth position and the adjusted width position.

During an assembly process for an aircraft, segments of the fuselage are fabricated separately prior to joining the segments together to form the complete fuselage. In order to ensure that abutting ends of the segments mate together correctly, a machining process is performed along the edges of the segments at their ends. One embodiment comprises a trim-tool assembly for machining proximate to an edge of a workpiece. The trim-tool assembly includes an indexing cart configured to mount to a track secured to a surface of the workpiece, where a setting on the indexing cart varies a distance between a centerline of the track and the edge of the workpiece. The trim-tool assembly further includes a tool cart configured to mount to and translate along the track, where the tool cart includes a process tool that performs a machining process on the workpiece at a fixed distance from the centerline of the track.

In one example, an on-wing method for in-situ cutting on a wing-to-fuselage attachment includes attaching a first mount plate having a first linear bearing to provide movement in a first linear direction relative to the first mount plate, attaching a second mount plate having a second linear bearing to provide movement in a second linear direction relative to the second mount plate, attaching a tool mounting member to the second linear bearing to move with the second linear bearing, attaching a cutter to the tool mounting member to be adjustable relative to the second linear bearing, adjusting a depth position of a cut to be made on the wing-to-fuselage attachment, adjusting a width position of the cut, and moving the tool along a length direction of the cut to make the cut on the wing-to-fuselage attachment along the length direction at the adjusted depth position and the adjusted width position.

In one example, an on-wing apparatus for in-situ cutting on a wing-to-fuselage attachment includes a first linear bearing disposed on a first mount plate to move in a first direction. A second linear bearing is disposed on a second mount plate to move in a second direction. The second mount plate is attached to the first linear bearing. A tool mounting member is attached to the second linear bearing. A cutter is attached to the tool mounting member to be adjustable, relative to the second linear bearing, in a rotational direction around an adjustment axis. One of the first direction and the second direction is a depth direction of the cut parallel to the adjustment axis, and the other is a length direction of the cut. A width position of the cut is determined by rotational adjustment of the cutter with respect to the second linear bearing in the rotational direction.

Implementations of a miter jig are provided. The miter jig can be used to fabricate a non-perpendicular miter joint, the miter joint being formed by beveling each of two parts (e.g., wooden panels) to be joined to form a corner. By using a miter jig, each of the parts to be joined can be cut to have a bevel angle of up to 80. In this way, a corner having an acute angle or an obtuse angle can be formed. The miter jig is configured so that it can be secured to a workpiece and comprises a base plate connected to a top plate by a hinge, at least two adjustable brace assemblies configured to set the angle of the top plate relative to the base plate, and a cutting implement guide configured to guide a cutting implement to cut a workpiece at an angle.

Implementations of a miter jig are provided. The miter jig can be used to fabricate a non-perpendicular miter joint, the miter joint being formed by beveling each of two parts (e.g., wooden panels) to be joined to form a corner. In some implementations, by using a miter jig, each of the parts to be joined can be cut to have a bevel angle of up to 80. In this way, a corner having an acute angle or an obtuse angle can be formed. The miter jig is configured so that it can be secured to a workpiece and comprises a base plate connected to a top plate by a hinge, at least two adjustable brace assemblies configured to set the angle of the top plate relative to the base plate, and a cutting implement guide configured to guide a cutting implement to cut a workpiece at an angle.

A saw guide adapted to guide a cutting device as to make a straight cut in an object, comprising a base unit; a longitudinal track connected to the base unit; a track rider connected to the track adapted to be ridden longitudinally across the track; a coupling element with a first side connected to the track rider and a second side connected to the cutting device; and a stabilization handle attached to the base unit adapted to stabilize the saw guide when clung to an edge of the object.