In an aspect there are disclosed examples systems (10, 110) for the landing and handling of a drone (1), the system (10, 100) may include a moveable platform (16, 116) on which the drone (1) is supportable in a landed state; a space (14, 114) dimensioned to receive the platform (16, 116) and drone (1) in the landed state, a first closable barrier (17, 117) arranged between the drone (1) in the landed state and an external environment; a second closable barrier (18, 118) arranged between the drone (1) in the landed state and a passenger zone adjacent the space (22, 122); and a control arrangement (205) configured to selectively operate the platform (16, 116), the first closable barrier (17, 117) and the second closable barrier (18, 118) between: a first condition, in which the first closable barrier (17, 117) is in an open condition, the second closable barrier (18, 118) is in a closed condition and the drone (1) is landable on the platform (16, 116), and a second condition, in which the platform (16, 116) and drone (1) in the landed state are receivable by the space (22, 122), the first closable barrier (17, 117) is movable to a closed condition, and the second closable barrier (18, 118) is moveable to an open condition.

In an aspect there are disclosed examples systems (10, 110) for the landing and handling of a drone (1), the system (10, 100) may include a moveable platform (16, 116) on which the drone (1) is supportable in a landed state; a space (14, 114) dimensioned to receive the platform (16, 116) and drone (1) in the landed state, a first closable barrier (17, 117) arranged between the drone (1) in the landed state and an external environment; a second closable barrier (18, 118) arranged between the drone (1) in the landed state and a passenger zone adjacent the space (22, 122); and a control arrangement (205) configured to selectively operate the platform (16, 116), the first closable barrier (17, 117) and the second closable barrier (18, 118) between: a first condition, in which the first closable barrier (17, 117) is in an open condition, the second closable barrier (18, 118) is in a closed condition and the drone (1) is landable on the platform (16, 116), and a second condition, in which the platform (16, 116) and drone (1) in the landed state are receivable by the space (22, 122), the first closable barrier (17, 117) is movable to a closed condition, and the second closable barrier (18, 118) is moveable to an open condition.

An unmanned vehicle module can include, in some aspects, a landing platform including a landing area for receiving an unmanned vehicle, wherein the landing area includes a predetermined charging region; a first charging plate; a second charging plate, wherein the first charging plate and the second charging plate are positioned in the predetermined charging region; an electrical energy storage device for connecting electrically with the first charging plate and with the second charging plate; and an unmanned vehicle alignment mechanism configured to move the unmanned vehicle into the predetermined charging region; wherein the unmanned vehicle alignment mechanism includes a first beam, a second beam, a third beam, a fourth beam, and an actuation device for actuating at least two of the first beam, the second beam, the third beam, and the fourth beam to push the unmanned vehicle into the charging region.

An unmanned vehicle module can include, in some aspects, a landing platform including a landing area for receiving an unmanned vehicle, wherein the landing area includes a predetermined charging region; a first charging plate; a second charging plate, wherein the first charging plate and the second charging plate are positioned in the predetermined charging region; an electrical energy storage device for connecting electrically with the first charging plate and with the second charging plate; and an unmanned vehicle alignment mechanism configured to move the unmanned vehicle into the predetermined charging region; wherein the unmanned vehicle alignment mechanism includes a first beam, a second beam, a third beam, a fourth beam, and an actuation device for actuating at least two of the first beam, the second beam, the third beam, and the fourth beam to push the unmanned vehicle into the charging region.

Systems for landing and handling of a drone may include a platform on which the drone is supportable in a landed state; a space to receive the platform and drone in the landed state, a first closable barrier arranged between the drone in the landed state and an external environment; a second closable barrier arranged between the drone in the landed state and a passenger zone; and a control arrangement configured to operate the platform, the first closable barrier and the second closable barrier between: a first condition, in which the first closable barrier is in an open condition, the second closable barrier is in a closed condition and the drone is landable on the platform, and a second condition, in which the platform and drone in the landed state are receivable by the space, the first closable barrier is movable to a closed condition, and the second closable barrier is moveable to an open condition.

Systems for landing and handling of a drone may include a platform on which the drone is supportable in a landed state; a space to receive the platform and drone in the landed state, a first closable barrier arranged between the drone in the landed state and an external environment; a second closable barrier arranged between the drone in the landed state and a passenger zone; and a control arrangement configured to operate the platform, the first closable barrier and the second closable barrier between: a first condition, in which the first closable barrier is in an open condition, the second closable barrier is in a closed condition and the drone is landable on the platform, and a second condition, in which the platform and drone in the landed state are receivable by the space, the first closable barrier is movable to a closed condition, and the second closable barrier is moveable to an open condition.

The subject matter described herein includes a tube for use in creating a support for a roof line of a structure. The tube comprises an inner flexible bladder, a seamless woven cylinder formed from fibers woven to form a seamless tubular arch shape when the cylinder is inflated, the cylinder engaged with the flexible bladder, and an outer weather shield coating engaged with the cylinder, wherein, in operation a plurality of tubes are used to form the roof line of a structure to define a housing for containing an article, wherein the plurality of tubes maintains flexibility so that the plurality of tubes can be inflated, deflated, and re-deployed.

A system and methods for the storage, and preservation of mechanical assets, including collectable automobiles, small airplanes and watercraft in a storage unit. The storage unit includes a plurality of asset modules. The volume of each asset module is variable. The atmosphere of each asset module may be controlled by a control system. Control of the atmosphere of each asset module includes control of parameters including the type of gas each atmosphere is composed of and the temperature, the pressure and relative humidity of each atmosphere. These parameters may be monitored and controlled from a remote location.

A system and methods for the storage, and preservation of mechanical assets, including collectable automobiles, small airplanes and watercraft in a storage unit. The storage unit includes a plurality of asset modules. The volume of each asset module is variable. The atmosphere of each asset module may be controlled by a control system. Control of the atmosphere of each asset module includes control of parameters including the type of gas each atmosphere is composed of and the temperature, the pressure and relative humidity of each atmosphere. These parameters may be monitored and controlled from a remote location.

A beam system and method of erecting a supporting arch enables large roofed structures to be erected quickly and economically. The method includes aligning a plurality of structural elements longitudinally; connecting upper corners of the structural elements to upper corners of adjacent structural elements, wherein adjacent lower corners of the structural elements remain unconnected; elevating first and second structural elements in a middle of the supporting arch; connecting lower corners of the first and second structural elements together; elevating third and fourth structural elements adjacent the first and second structural elements, respectively; and connecting lower corners of the third and fourth structural elements to lower corners of the first and second structural elements, respectively.