On-wing tool for in-situ cutting on wing-to-fuselage attachment of aircraft

An on-wing apparatus for in-situ cutting on a wing-to-fuselage attachment of a wing and a fuselage of an aircraft, the on-wing apparatus comprising:

• a first linear bearing disposed on a first mount plate to provide movement of the first linear bearing in a first linear direction with respect to the first mount plate, the first mount plate being configured to be attached to the aircraft in vicinity of the wing-to-fuselage attachment;
• a second linear bearing disposed on a second mount plate to provide movement of the second linear bearing in a second linear direction with respect to the second mount plate, the second mount plate being attached to the first linear bearing to move with the first linear bearing in the first linear direction with respect to the first mount plate;
• a tool mounting member attached to the second linear bearing to move with the second linear bearing in the second linear direction with respect to the second mount plate which moves with the first linear bearing in the first linear direction with respect to the first mount plate;
• and
• a cutter attached to the tool mounting member to be adjustable, relative to the second linear bearing, in a tool mount rotational direction around an adjustment axis;
• one of the first linear direction and the second linear direction being a depth direction of a depth of a cut to be made on the wing-to-fuselage attachment, which is parallel to the adjustment axis, and the other of the first linear direction and the second linear direction being a length direction of a length of the cut;
• and
• a width position of the cut being determined by a rotational adjustment of the cutter with respect to the second linear bearing in the tool mount rotational direction around the adjustment axis;
• the cutter including:
• a rotary motor that is attached to the tool mounting member to be adjustable, relative to the second linear bearing, in the tool mount rotational direction around the adjustment axis, the rotary motor providing rotational drive to a drive shaft oriented along a rotary motor axis;
• an endmill shank that is oriented along a rotational cutter axis and perpendicularly coupled to the drive shaft to be driven by the drive shaft, the rotational cutter axis being oriented parallel to the adjustment axis;
• an endmill cutting bit configured to be attached to an end of the endmill shank to cut an exposed area of the wing-to-fuselage attachment;
• and
• an undercut cutting bit configured to be attached to an end of the endmill shank to cut an overlapped area of the wing-to-fuselage attachment between a trailing-edge wing attachment fitting and a fuselage attachment fitting.

An on-wing apparatus for in-situ cutting on a wing-to-fuselage attachment of a wing and a fuselage of an aircraft, the on-wing apparatus comprising:

• a first linear bearing disposed on a first mount plate to provide movement of the first linear bearing in a first linear direction with respect to the first mount plate, the first mount plate being configured to be attached to the aircraft in vicinity of the wing-to-fuselage attachment;
• a second linear bearing disposed on a second mount plate to provide movement of the second linear bearing in a second linear direction with respect to the second mount plate, the second mount plate being attached to the first linear bearing to move with the first linear bearing in the first linear direction with respect to the first mount plate;
• a tool mounting member attached to the second linear bearing to move with the second linear bearing in the second linear direction with respect to the second mount plate which moves with the first linear bearing in the first linear direction with respect to the first mount plate;
• and
• cutting means attached to the tool mounting member to be adjustable, relative to the second linear bearing, in a tool mount rotational direction around an adjustment axis;
• one of the first linear direction and the second linear direction being a depth direction of a depth of a cut to be made on the wing-to-fuselage attachment, which is parallel to the adjustment axis, and the other of the first linear direction and the second linear direction being a length direction of a length of the cut;
• and
• a width position of the cut being determined by a rotational adjustment of the cutter with respect to the second linear bearing in the tool mount rotational direction around the adjustment axis;
• the tool mounting member including:
• a center portion attached to the second linear bearing to move with the second linear bearing;
• a first side panel rotatably attached to a first side of the center portion to rotate relative to the center portion around the adjustment axis;
• a second side panel rotatably attached to a second side of the center portion to rotate relative to the center portion around the adjustment axis;
• at least one first fastener to releasably fasten the first side panel to the center portion via at least one first slot, at any first position of a plurality of first positions along the at least one first slot, the plurality of first positions being selectable along the at least one first slot by rotational adjustment of the first side panel relative to the center portion around the adjustment axis, the at least one first slot being provided in the center portion or the first side panel;
• and
• at least one second fastener to releasably fasten the second side panel to the center portion via at least one second slot, at any second position of a plurality of second positions along the at least one second slot, the plurality of second positions being selectable along the at least one second slot by rotational adjustment of the second side panel relative to the center portion around the adjustment axis, the at least one second slot being provided in the center portion or the second side panel;
• the cutting means being attached (i) to the first side panel to move with the first side panel that is rotatably attached to the center portion, for cutting the wing-to-fuselage attachment located at a right side wing of the aircraft on an inboard side thereof for the first mount plate that is attached to the right side wing, or for cutting the wing-to-fuselage attachment located at a left-side wing of the aircraft on an outboard side thereof for the first mount plate that is attached to the left-side wing, or (ii) to the second side panel to move with the second side panel that is rotatably attached to the center portion, for cutting the wing-to-fuselage attachment located at the left-side wing on an inboard side thereof for the first mount plate that is attached to the left-side wing, or for cutting the wing-to-fuselage attachment located at the right side wing on an outboard side thereof for the first mount plate that is attached to the right side wing.