B23P23/02

Tooling assemblies for lathe machines, CNC threading lathes, and methods of milling threads in tubular workpieces

A tooling assembly for a lathe machine includes a tool platform configured to be mounted on the lathe machine, a milling tool holder fixedly secured to the tool platform and workable to releasably secure a thread milling tool therein, and a milling tool drive. The milling tool drive is operatively connected to the milling tool holder and operable to rotate the milling tool holder independently of a work holder to mill threads on the workpiece when a pipe thread milling tool is secured in the milling tool holder. Computer numerical control threading lathes and methods of milling threads in tubular workpieces are also described.

MOBILE TOOL-SUPPORT APPARATUS
20250360583 · 2025-11-27 ·

An example tool-support apparatus includes a frame having a first support member, a second support member, a third support member, and a fourth support member; a first host-mating plate affixed to the first support member; a second host-mating plate affixed to the second support member; a first stabilizer affixed to the third support member; a second stabilizer affixed to the fourth support member; a first rail extending between the first support member and the third support member; a second rail extending between the second support member and the fourth support member; and a tool support member having a first end slidably coupled to the first rail and having a second end slidably coupled to the second rail.

MOBILE TOOL-SUPPORT APPARATUS
20250360583 · 2025-11-27 ·

An example tool-support apparatus includes a frame having a first support member, a second support member, a third support member, and a fourth support member; a first host-mating plate affixed to the first support member; a second host-mating plate affixed to the second support member; a first stabilizer affixed to the third support member; a second stabilizer affixed to the fourth support member; a first rail extending between the first support member and the third support member; a second rail extending between the second support member and the fourth support member; and a tool support member having a first end slidably coupled to the first rail and having a second end slidably coupled to the second rail.

NUMERICAL CONTROL MACHINE TOOL
20250353124 · 2025-11-20 ·

A numerical control machine tool includes: a base; a movable shaft assembly, which is arranged on the base; a rotary shaft assembly, which is arranged on the base, wherein a portion of a structure of the rotary shaft assembly is configured to move under the action of a portion of a structure of the movable shaft assembly, thereby performing turn-milling compound machining on a part; and a clamping assembly, which is arranged on the base and is used for clamping and fixing the part. The clamping assembly includes a first fixing member, a mounting member, a driving member and a flipping member.

NUMERICAL CONTROL MACHINE TOOL
20250353124 · 2025-11-20 ·

A numerical control machine tool includes: a base; a movable shaft assembly, which is arranged on the base; a rotary shaft assembly, which is arranged on the base, wherein a portion of a structure of the rotary shaft assembly is configured to move under the action of a portion of a structure of the movable shaft assembly, thereby performing turn-milling compound machining on a part; and a clamping assembly, which is arranged on the base and is used for clamping and fixing the part. The clamping assembly includes a first fixing member, a mounting member, a driving member and a flipping member.

Combined working machine
12551951 · 2026-02-17 · ·

There is provided a combined working machine including: a bed in which a front inclined surface which is inclined forward is formed; a first workpiece main spindle device and a second workpiece main spindle device disposed on the front inclined surface of the bed to be opposite to each other and including a main spindle stand configured to rotatably hold a main spindle about an axis and a driving mechanism configured to move the main spindle in an axial direction of the main spindle; a first turret device and a second turret device including a turret configured to attach multiple turret tools disposed above the main spindle on the bed; and a tool main spindle device disposed between the first turret device and the second turret device on the bed and including a main spindle head configured to exchangeably and rotatably hold a main spindle head tool.

Combined working machine
12551951 · 2026-02-17 · ·

There is provided a combined working machine including: a bed in which a front inclined surface which is inclined forward is formed; a first workpiece main spindle device and a second workpiece main spindle device disposed on the front inclined surface of the bed to be opposite to each other and including a main spindle stand configured to rotatably hold a main spindle about an axis and a driving mechanism configured to move the main spindle in an axial direction of the main spindle; a first turret device and a second turret device including a turret configured to attach multiple turret tools disposed above the main spindle on the bed; and a tool main spindle device disposed between the first turret device and the second turret device on the bed and including a main spindle head configured to exchangeably and rotatably hold a main spindle head tool.

HINGE STRUCTURE
20260042529 · 2026-02-12 ·

A spar structure for connecting a moveable component to an aircraft includes a continuous body of material defining a plurality of attachment and actuation brackets. The spar structure includes a pair of continuous hinge lines extending through the body. The spar structure is formed by drilling a pair of elongate bores into a block or billet of material to define the pair of continuous hinge lines and by machining the block or billet of material according to a predetermined machining profile to form the spar structure around the pair of continuous hinge lines.

HINGE STRUCTURE
20260042529 · 2026-02-12 ·

A spar structure for connecting a moveable component to an aircraft includes a continuous body of material defining a plurality of attachment and actuation brackets. The spar structure includes a pair of continuous hinge lines extending through the body. The spar structure is formed by drilling a pair of elongate bores into a block or billet of material to define the pair of continuous hinge lines and by machining the block or billet of material according to a predetermined machining profile to form the spar structure around the pair of continuous hinge lines.

End effector and methods of use

An end effector is presented. The end effector comprises a torque wrench and a first vacuum source. The torque wrench is configured to hold a collar and apply a single-sided clamp-up to a structure. The first vacuum source is pneumatically connected to the torque wrench and configured to supply a vacuum for the single-sided clamp-up.