A machining tool assembly is provided for machining a blank to form a firearm lower receiver. The assembly includes a pair of side plates positionable on opposed sides of the blank to capture the blank therebetween. A template plate having a template aperture is adapted to be removeably attachable to the side plates. The template aperture is aligned with a top surface of the blank and is adapted for machining a cavity within the blank having a peripheral contour complimentary to a peripheral contour of the template aperture. A centering mechanism is adapted to be removeably attachable to the template plate, with the centering mechanism including an opening aligned with a corresponding void formed on the blank to align the blank with the template plate.

A holding device (100) for a round dental blank (200), comprising an open ring element (101) for laterally gripping the dental blank (200); and a closing element (103) for closing the ring element (101) at various positions.

Systems and methods are provided for shape controlled gripping of a workpiece. A layer jamming structure includes a membrane defining an internal cavity containing a number of overlapping material layers. A pressure system includes a pump coupled with the internal cavity. A shape conforming tool includes at least one part configured to move to apply a force to the layer jamming structure. The shape conforming tool, by operation of the part, conforms the layer jamming structure to the workpiece. The pressure system, with operation of the pump, changes a pressure in the internal cavity to impart rigidity to the layer jamming structure.

A system for post-cure processing a composite workpiece includes a tool. The tool includes a tool surface. The tool surface supports the composite workpiece located on the tool. The system also includes a drill template. The drill template defines a drilling location for drilling a hole through the composite workpiece while the composite workpiece is on the tool.

An assembling device for manufacturing a panel assembly, which includes at least two tooling systems, which both include wooden slat gripping, positioning and securing means, and insulation panel gripping and positioning means, and a tooling controller communicatively coupled to the tooling systems, wherein the tooling systems are instructed so that, if the length of a wooden slat exceeds a predetermined threshold, the wooden slat gripping means grip the wooden slat at different parts, and are moved relatively to each other in order to align their centerlines and to correct the straightness of the wooden slat.

A locating pin for positioning one or more workpieces on a mounting member is provided. The locating pin includes at least one cam being radially moveable between an extended position and a retracted position. The at least one cam engages the workpiece while in the extended position to hold the workpiece in place. The at least one cam is spaced from the workpiece while in the retracted position to allow the workpiece to be positioned on, or removed from the locating pin.

Systems and methods are provided for assembling an aircraft. The method includes receiving a lower half barrel section of fuselage that is inverted to a keel-up orientation; and installing a floor grid into the lower half barrel section while inverted.

A wheel fixture is disclosed. A main shaft drives a first positioning pull rod on a chuck body to extend and contract in the radial direction via a tightening screw, a clamping jaw is at a position within the travel range of extension and contraction, a wheel is positioned and clamped by the fixture, airtight support blocks are pressed down by the wheel and flush with the support plane of the clamping jaw, at this time, airtight ejector rods press second O rings to prevent air from flowing out of the airtight detection position, a detection system of a machine tool detects a preset air pressure value which indicate that the wheel has been placed correctly, and if the wheel is not placed correctly on the fixture, the machine tool will alarm through the detected pressure feedback.

A clamping mechanism for machining a composite component. The clamping mechanism comprising two or more opposing clamping plates, each clamping plate comprising a clamping surface; and wherein each clamping surface is adaptable to follow the microstructural surface of the composite component being clamped. The clamping surface may comprise a plurality of deformable micropillars featuring a body that extends to a base on the clamping plates and a head that deforms to follow the microstructural surface of the composite component. The clamping surface in use may be an exact negative of the microstructural surface of the component clamping surface. Each clamping surface may comprise a disposable insert that replicates exclusively at the point of contact the microstructural surface of the component being clamped.

A method of bonding a blade cuff to a rotor blade includes installing the blade cuff to a root end of the rotor blade. The method includes mounting the rotor blade within a plurality of supports. The method includes coupling the blade cuff to a first fixture. The method includes installing a second fixture about the blade cuff. The method further includes applying localized and constant heat and pressure to the blade cuff via the second fixture.