Methods of performing assembly or maintenance on an aircraft, systems for performing desired assembly or maintenance on an aircraft, and mobile work stations useful for such systems and methods, where the mobile work stations include a work platform, including an accessway providing access to the work platform; and a moveable base supporting the work platform with one or more platform jacks that can adjustably raise and lower the work platform.

Methods of performing assembly or maintenance on an aircraft, systems for performing desired assembly or maintenance on an aircraft, and mobile work stations useful for such systems and methods, where the mobile work stations include a work platform, including an accessway providing access to the work platform; and a moveable base supporting the work platform with one or more platform jacks that can adjustably raise and lower the work platform.

An electronic vertical takeoff and landing (eVTOL) multicopter which includes a communications interface configured to establish a communication channel between a site local server and the eVTOL multicopter and send a vehicle identifier and vehicle state information from the eVTOL multicopter to the site local server. The eVTOL multicopter also includes a processor configured to perform a management operation received from the site local server, wherein the site local server is configured to determine the management operation based at least in part on the vehicle identifier and the vehicle state information.

Methods and apparatus for performing repair operations using an unmanned aerial vehicle (UAV). A UAV carries a repair patch ensemble containing all repair materials (including a repair patch, a heating blanket and other ensemble materials) in a prepackaged form to the repair area. During flight of the UAV, the repair patch is vacuum adhered to the heating blanket. Vacuum pressure is also used to hold the repair patch ensemble in position on the composite surface of the structure. Then the hot bond process is enacted to bond the repair patch to the repair area. In accordance with one embodiment, the hot bond process involves heating the repair patch to adhesively bond the repair patch while applying vacuum pressure to consolidate the composite material. Then the repair patch is released from the ensemble and residual ensemble materials (heating blanket, bleeder material, and release films) are removed by the UAV.

Systems and methods relating to automated handline of aerial vehicles are disclosed. The described systems and methods can include a plurality of robots operating on a continuous, closed-loop track. A plurality of aerial vehicle handling stations can be disposed along the continuous, closed-loop track, and each of the plurality of robots can engage an aerial vehicles and transport it to the aerial vehicle handling station, as needed, in accordance with a workflow associated with the aerial vehicle. The described systems and methods can provide a fully automated system for the ground handling of multiple aerial vehicles simultaneously.

Systems and methods relating to automated handline of aerial vehicles are disclosed. The described systems and methods can include a plurality of robots operating on a continuous, closed-loop track. A plurality of aerial vehicle handling stations can be disposed along the continuous, closed-loop track, and each of the plurality of robots can engage an aerial vehicles and transport it to the aerial vehicle handling station, as needed, in accordance with a workflow associated with the aerial vehicle. The described systems and methods can provide a fully automated system for the ground handling of multiple aerial vehicles simultaneously.

A method is provided for use in maintenance of a vehicle. The method includes an onboard computer including an onboard reasoner diagnosing a failure mode onboard the vehicle using an onboard diagnostic model. The onboard reasoner further determines a service recommendation of a service action to address the failure mode. The method also includes an off-board computer including an off-board copy of the onboard reasoner receiving a measure of fix effectivity of the service action as performed to address the failure mode. The off-board copy diagnoses the failure mode or an alternate failure mode, from the measure of fix effectivity of the service action, and using an off-board copy of the onboard diagnostic model. Responsive to diagnosis of the alternate failure mode, the off-board copy determines a maintenance recommendation of a maintenance action to address the alternate failure mode, and generating a maintenance message including the maintenance recommendation.

A method for installing a replacement electrical heat sensor in a heatable aircraft window laminate structure comprising the steps of: drilling a blind hole in the edge of the window laminate; routing a channel in the edge of the window laminate from the blind hole to a terminal block of an originally installed heat sensor; inserting the replacement heat sensor into the hole; filling the hole with a material to seal the hole and the heat sensor from contamination; heating the window laminate; photographing the window laminate using an infrared camera to determine uniformity of heat distribution; placing a heated plate against the exterior surface of the window laminate directly over the position of the replacement heat sensor; measuring an electrical resistance of the replacement heat sensor to confirm proper operation of the replacement heat sensor.

A method for installing a replacement electrical heat sensor in a heatable aircraft window laminate structure comprising the steps of: drilling a blind hole in the edge of the window laminate; routing a channel in the edge of the window laminate from the blind hole to a terminal block of an originally installed heat sensor; inserting the replacement heat sensor into the hole; filling the hole with a material to seal the hole and the heat sensor from contamination; heating the window laminate; photographing the window laminate using an infrared camera to determine uniformity of heat distribution; placing a heated plate against the exterior surface of the window laminate directly over the position of the replacement heat sensor; measuring an electrical resistance of the replacement heat sensor to confirm proper operation of the replacement heat sensor.

A method of dissipating heat from a surface of a first thermoplastic composite (TPC) being inductively welded with a second thermoplastic composite (TPC) includes flexing a heat sink during placement to conform to the surface of the first TPC, cooling the heat sink, applying inductive heat to a weld interface area between the first TPC and the second TPC, and drawing off heat via the heat sink from the surface of the first TPC.