The invention discloses a double-layer sealed box having an activated carbon circulation sealing device, comprising an outer layer box, an inner layer box, and an activated carbon input device. The inner layer box is wrapped in the outer layer box, a first activated carbon transport chamber is formed at the top of the the inner layer box, between the outer layer box and the inner layer box, and a second activated carbon transport chamber is formed at least one side of the the inner layer box, between the outer layer box and the inner layer box.

The invention discloses a double-layer sealed box having an activated carbon circulation sealing device, comprising an outer layer box, an inner layer box, and an activated carbon input device. The inner layer box is wrapped in the outer layer box, a first activated carbon transport chamber is formed at the top of the the inner layer box, between the outer layer box and the inner layer box, and a second activated carbon transport chamber is formed at least one side of the the inner layer box, between the outer layer box and the inner layer box.

A storage silo has a cylindrical wall formed with a plurality of ring structures stacked one upon another. Each ring structure is formed with a plurality of sidewall panels connected end to end with a vertical joint between horizontally adjacent sidewall panels. The plurality of ring structures have at least one upper ring structure and at least one lower ring structure positioned below the upper ring structure, with a portion of the upper ring structure overlapping the lower ring structure to form a horizontal joint. The upper lower ring structure are formed with sidewall panels in a layered arrangement. Each sidewall panel has a middle portion, an offset upper portion and an offset lower portion. The offset upper portion and the offset lower portion of the sidewall panel are offset from the middle portion.

A storage silo has a cylindrical wall formed with a plurality of ring structures stacked one upon another. Each ring structure is formed with a plurality of sidewall panels connected end to end with a vertical joint between horizontally adjacent sidewall panels. The plurality of ring structures have at least one upper ring structure and at least one lower ring structure positioned below the upper ring structure, with a portion of the upper ring structure overlapping the lower ring structure to form a horizontal joint. The upper lower ring structure are formed with sidewall panels in a layered arrangement. Each sidewall panel has a middle portion, an offset upper portion and an offset lower portion. The offset upper portion and the offset lower portion of the sidewall panel are offset from the middle portion.

Embodiments of a large container may include a container base and a circumferential container wall. An upper end of the wall is closed by a container cover in the form of a metal disc. An annular, circumferential support element is secured at an upper end region of the wall. The disc spans the upper open end of the container wall. A lower side of the disc is welded to the support element and/or to the upper end region of the container wall by a continuous first welding seam. An upper side and/or an edge of the disc is welded to the support element by a continuous second welding seam. The first and second weld seams have respective first and second roots which merge into one another or at least come together.

Embodiments of a large container may include a container base and a circumferential container wall. An upper end of the wall is closed by a container cover in the form of a metal disc. An annular, circumferential support element is secured at an upper end region of the wall. The disc spans the upper open end of the container wall. A lower side of the disc is welded to the support element and/or to the upper end region of the container wall by a continuous first welding seam. An upper side and/or an edge of the disc is welded to the support element by a continuous second welding seam. The first and second weld seams have respective first and second roots which merge into one another or at least come together.

A pneumatic motor propulsion source including a friction welding apparatus, a gas accumulator tank operably coupled to the friction welding apparatus, and an air compressor operably coupled to the gas accumulator tank.

A pneumatic motor propulsion source including a friction welding apparatus, a gas accumulator tank operably coupled to the friction welding apparatus, and an air compressor operably coupled to the gas accumulator tank.

In an example, a transformable cargo container for use with ground and air transportation vehicles is disclosed. The cargo container includes a main container body defining a storage chamber. The cargo container also includes a transformable assembly coupled to the main container body and positioned at an exterior of the main container body. The transformable assembly includes one or more supplemental containers and is movable between an aircraft configuration and a ground configuration. Based on the transformable assembly being in the aircraft configuration, the transformable cargo container has a non-rectangular cross-sectional area and is configured to occupy a partially-radial cross-sectional storage area of a fuselage of an aircraft. And based on the transformable assembly being in the ground configuration, the transformable cargo container is configured to occupy a rectangular cross-sectional storage area on a ground transportation vehicle.

In an example, a transformable cargo container for use with ground and air transportation vehicles is disclosed. The cargo container includes a main container body defining a storage chamber. The cargo container also includes a transformable assembly coupled to the main container body and positioned at an exterior of the main container body. The transformable assembly includes one or more supplemental containers and is movable between an aircraft configuration and a ground configuration. Based on the transformable assembly being in the aircraft configuration, the transformable cargo container has a non-rectangular cross-sectional area and is configured to occupy a partially-radial cross-sectional storage area of a fuselage of an aircraft. And based on the transformable assembly being in the ground configuration, the transformable cargo container is configured to occupy a rectangular cross-sectional storage area on a ground transportation vehicle.