A fluid delivery device is provided. The fluid delivery device includes a melter having a loading chamber and a hopper disposed in communication with the loading chamber, the loading chamber having one or more heating elements. The hopper includes a second heating element. The melter also includes a container handling system for lifting a container a predetermined height and moving the container from a position remote of the melter to a position within the loading chamber. The container includes contents stored within. The heating elements heat the contents so that the contents may be received in the hopper. The hopper may continue to heat the contents to provide a fluid. The fluid may be discharged from the hopper by way of a pump assembly. A pressure of fluid may be regulated at the pump assembly.

A lifting unit for a vehicle can include a mounting assembly configured to pivotally couple to a lifting boom of the vehicle, a coupler assembly configured to releasably couple with equipment positionable by the lifting unit, and a rotary actuator assembly coupled between the mounting assembly and the coupler assembly. The mounting assembly includes a mount, a travelling frame coupled to the mount, and an extension actuator configured to displace the travelling frame along an extension axis relative to the mount. The rotary actuator assembly is configured to rotate the coupler assembly about a rotational axis.

A side lift spreader main beam (22) comprises a vertical carrier plate (58) having a first vertical height (H1) and being made of steel plate having a first thickness (T1); a C-beam (60) comprising a first horizontal flange (64) and a second horizontal flange (66) interconnected by a vertical web portion (68), the C-beam (60) having a second vertical height (H2) lower than the first vertical height (H1) and being made of steel plate having a second thickness (T2) thinner than the first thickness (T1), wherein the C-beam (60) defines, together with the carrier plate (58), a closed channel beam with a first flange (74) of the carrier plate (58) extending vertically from the closed channel beam; and an inclined support plate (62) welded to the carrier plate, and to an outer face of the first flange (64) of the C-beam (60) at a distance from the carrier plate (58).

Presented are corner attachment assemblies for cargo suspension systems, methods for making/using such assemblies, and aircraft equipped with underbody suspension systems using corner attachment assemblies for securing payload containers. Mounting assemblies are presented for securing objects to tether cables of suspension systems. A representative cargo mounting assembly includes a pair of shoulder clamps, each of which includes a flap that projects from a cup. Each shoulder clamp flap mechanically attaches, e.g., via a flap through-hole with a structurally reinforcing grommet, to a respective segment of a tether cable of a cargo suspension system. In addition, each shoulder clamp cup includes multiple noncoplanar, mutually adjoining contact surfaces. For instance, the cup may have a tetrahedral geometry with three mutually orthogonal, triangular-shaped contact surfaces. Each contact surface attaches, e.g., via a high-strength adhesive, to a respective surface of a corner of a cargo container.

Controlling a container, such as a spreader, is described for engaging, retaining, and moving containers, as well as for unloading containers, particularly bottom-unloading containers. A spreader includes a frame having mounted thereon twistlocks, an actuator, a movable engagement mechanism, and force transmission means connecting the actuator and the movable engagement mechanism. The actuator and the force transmission means are substantially disposed along the long sides of the frame, and the movable engagement mechanism is substantially disposed on the short sides of the frame. The actuator allows the movable engagement mechanism to move reciprocally primarily in a direction perpendicular to the plane of the frame. The spreader significantly expands the functionality of devices used for engaging, retaining, moving, and unloading containers, makes it possible to unload a bottom-unloading container, and also allows the automation, simplification, and acceleration of the unloading process of such a container.

The present disclosure relates to an apparatus and method for loading and unloading cargo of air mobility, in which cargo loading and unloading may be automated without the aid of human resources, as well as enabling loading and unloading of cargo in a required location without an air mobility landing. The apparatus includes a winch installed in a cargo hold of an air mobility, a multiarticulated robot arm suspended from the winch, and a gripper provided on an end of the multiarticulated robot arm and capable of gripping a container.

The disclosure relates to a lifting vehicle frame and an aerial transportation vehicle. The aerial transportation vehicle includes a lifting vehicle frame, which includes an upper vehicle frame (1), a lower vehicle frame (2), a lifting assembly (a) and a locking device (b), wherein the upper vehicle frame (1) and the lower vehicle frame (2) are connected through the lifting assembly (a); at least two lifting assemblies (a) are provided opposite to each other in a first direction; the lower vehicle frame (2) and the upper vehicle frame (1) can move close to or apart from each other by operating the at least two lifting assemblies (a); the locking device (b) is disposed on the lower vehicle frame (2); when the lower vehicle frame (2) and the upper vehicle frame (1) move close to each other, the lower vehicle frame (2) and the upper vehicle frame (1) are locked together by operating the locking device (b). The aerial transportation vehicle of the disclosure can achieve connection and assembly with a container by its own devices, which is simple in operation, and has high automatic level and good practicability.

The invention provides a container manipulation device comprising a frame, two container engagement members, two pivoting mechanisms for pivoting the engagement members with respect to the frame, the pivoting mechanisms each include a coupler, pivotally connected with a first end to the engagement member at a first distance from the engagement member pivot axis, a rocker, pivotally connected with a first end to the frame and with a second end to a second end of the coupler, and an actuator for pivoting the rocker about the rocker pivot axis such that the engagement member pivots between the first and second orientation. The invention also provides a hoisting device comprising such a container manipulation device.

A lifting rig includes a cradle and a load transfer device. The load transfer device is arranged to draw in a payload to the cradle or deliver a payload from the cradle. The lifting rig is arranged to be lifted to an elevated space and the load transfer device is arranged to draw in or deliver the payload within the elevated space.

The system (1) for lifting and controlling the horizontal orientation and/or position of components (90), such as wind turbine main components, during installation and/or dismounting of said components comprises: a crane boom arrangement (3) and one or more lifting lines (3a) guided by said crane boom arrangement (3) for lifting said components. The system moreover comprises a lifting device (10) comprising a crane connection arrangement (11) connected to said one or more lifting lines (3a), a frame arrangement (12) connected to said crane connection arrangement (11), a first and a second steering wire guide (13a, 13b) configured for guiding steering wires (20a, 20b), and a component connection arrangement (30) connected to said frame arrangement and configured to be connected directly or indirectly to the component to be lifted. The system (1) further comprises a guiding arrangement (4) connected to said crane boom arrangement (3), and said steering wires (20a, 20b) are connected to said guiding arrangement (4) and extend from the guiding arrangement (4) in a direction towards the lifting device (10) with a mutual angle (a1) between the steering wires (20a, 20b). A relative displacement between said frame arrangement (12) and one or both of the first and second steering wire guides (13a, 13b) is configured to be provided to control the mutual angle (a1) between the steering wires (20a, 20b).