An aircraft lifting assembly includes a jack, a load cell, and a jack adapter. The jack includes an extendable arm having a distal end portion for exerting a force to lift an object. The distal end portion defines a cavity. The jack adapter couples the extendable arm to the load cell and includes a base portion, a cradle portion, and a projection. The base portion defines a jack arm support surface and a load cell support surface. The jack arm support surface opposes the distal end portion of the extendable arm and the load cell support surface opposes the load cell. The cradle portion extends from the base portion to circumscribe a portion of the load cell to secure the jack adapter to the load cell. The projection extends from the base portion into the cavity to secure the jack adapter to the extendable arm of the jack.

An aircraft lifting assembly includes a jack, a load cell, and a jack adapter. The jack includes an extendable arm having a distal end portion for exerting a force to lift an object. The distal end portion defines a cavity. The jack adapter couples the extendable arm to the load cell and includes a base portion, a cradle portion, and a projection. The base portion defines a jack arm support surface and a load cell support surface. The jack arm support surface opposes the distal end portion of the extendable arm and the load cell support surface opposes the load cell. The cradle portion extends from the base portion to circumscribe a portion of the load cell to secure the jack adapter to the load cell. The projection extends from the base portion into the cavity to secure the jack adapter to the extendable arm of the jack.

The blade support apparatus involves storing and transporting helicopter blades until the blades are needed for reassembly to the helicopter. The blade support apparatus comprises a lid, a container, a root attachment, and a plurality of attachment bars. One end of the helicopter blade is the root. The blade root is secured to the root plug. A multiplicity of supports secure the container to a transport. The height and angle of each blade in the container can be adjusted, enabling them to conform to the blade curvature which spirals from the blade root to the tip of the blade. Height adjustment to a helicopter blade is achieved by a plurality of contoured pads mounted in the container at varying points along the helicopter blade. Angle adjustment is achieved by a plurality of pivot supports mounted in the container at varying points along the helicopter blade.

The blade support apparatus involves storing and transporting helicopter blades until the blades are needed for reassembly to the helicopter. The blade support apparatus comprises a lid, a container, a root attachment, and a plurality of attachment bars. One end of the helicopter blade is the root. The blade root is secured to the root plug. A multiplicity of supports secure the container to a transport. The height and angle of each blade in the container can be adjusted, enabling them to conform to the blade curvature which spirals from the blade root to the tip of the blade. Height adjustment to a helicopter blade is achieved by a plurality of contoured pads mounted in the container at varying points along the helicopter blade. Angle adjustment is achieved by a plurality of pivot supports mounted in the container at varying points along the helicopter blade.

A wheel dolly for lifting and transporting a flat tire attached to an aircraft is comprised of a frame assembly having first and second laterally spaced frame members and a telescopic frame structure interposed between the laterally spaced frame members. A pair of tire lifting assemblies are fixedly coupled the frame assembly. A pair of actuators is coupled between the tire lifting assemblies to force the tire lifting assemblies toward one another in order to raise a flat tire on an aircraft. A plurality of wheels is coupled to the frame assembly to allow the frame assembly to roll in any direction.

A wheel dolly for lifting and transporting a flat tire attached to an aircraft is comprised of a frame assembly having first and second laterally spaced frame members and a telescopic frame structure interposed between the laterally spaced frame members. A pair of tire lifting assemblies are fixedly coupled the frame assembly. A pair of actuators is coupled between the tire lifting assemblies to force the tire lifting assemblies toward one another in order to raise a flat tire on an aircraft. A plurality of wheels is coupled to the frame assembly to allow the frame assembly to roll in any direction.

An attachment for an end effector. The attachment may include a clamp and a foot adhesively bonded to an edge of the clamp and having a set of interlocking features that form a mechanical interlock with the clamp.

An attachment for an end effector. The attachment may include a clamp and a foot adhesively bonded to an edge of the clamp and having a set of interlocking features that form a mechanical interlock with the clamp.

A trolley support system (100) includes at least one intelligent trolley (102) designed for use onboard passenger transportation vehicles such as aircraft. The trolley (102) includes a housing (106) with an internal compartment (108) and a door (110) that provides selective access to the internal compartment. The door is movable between a closed position and an unclosed position. The trolley also includes a control sensor (116) that configured to detect at least one characteristic of the trolley and a visual indicator (122) configured to emit a visual transmission based on the at least one detected characteristic. A trolley node (104) having a controller may be included with the trolley and may be communicatively coupled to the control sensor and the visual indicator.

An arm removal system for removing an arm. The system includes an anvil, and a removal assembly with at least two jackscrews. The arm has an extension radially extending from the arm and an arm outer surface. The arm is disposed within a wedge shaped collet that is disposed within a socket in an aircraft with an aircraft outer surface. The removal assembly includes an extension engaging surface and threaded jackscrew holes for accepting the jackscrews, such that when the jackscrews are tightened within the jackscrew holes, the jackscrews apply force on the anvil and the aircraft outer surface in the direction away from the removal assembly such that the arm is eventually removed entirely from the aircraft.