B64F5/40

Reconfiguring a vehicle for transfer from a first operator to a second operator

A method is provided for reconfiguring a vehicle for transfer from a first operator to a second operator. The method includes accessing first datasets that define an initial configuration of the vehicle, importing second datasets that describe maintenance, repair or service of the vehicle during in-service operation with the first operator, and generating a first composite dataset defining a current configuration of the vehicle. The method also includes accessing third datasets that define requirements of the vehicle for in-service operation with the second operator, and generating a second composite dataset that defines a target configuration of the vehicle from the first composite dataset and based on data of the third datasets. The method includes comparing the first and second composite datasets to identify modifications to reconfigure the vehicle from the current configuration to the target configuration, and generating a visual presentation of the modifications to facilitate reconfiguration of the vehicle.

Secure wireless dataloading using in-flight entertainment connectivity systems

Devices, systems and methods for enhancing aircraft maintenance are disclosed. An exemplary method for improving dataloading in an airplane includes retrieving, from an in-flight entertainment connectivity (IFEC) system, at least one avionics software, the IFEC system comprising a mass storage device comprising a first storage segment and a second storage segment, the first storage segment being a secure storage segment configured to store the at least one avionics software, and the second storage segment being configured to store media content, and loading, using a wireless network converter coupled to a wired legacy port, the at least one avionics software onto a target avionics system.

DEVICE AND METHOD FOR MANAGING A FLEET OF INFORMATION-COMMUNICATING DEVICES FOR UPDATING A DIGITAL TWIN OF A TURBOMACHINE

The disclosure relates to a device and a method for managing a fleet of information communication devices with reversible attachment on aircraft turbomachines, having: an association of a device among the fleet of devices with a turbomachine among a fleet of turbomachines, an attachment, an acquisition of at least one turbomachine operating parameter, a development of at least one indicator that allows the update of a digital twin of the turbomachine based on the operating parameter acquired, a communication of the indicator that allows the update of the digital twin to a digital twin storage entity.

DEVICE AND METHOD FOR MANAGING A FLEET OF INFORMATION-COMMUNICATING DEVICES FOR UPDATING A DIGITAL TWIN OF A TURBOMACHINE

The disclosure relates to a device and a method for managing a fleet of information communication devices with reversible attachment on aircraft turbomachines, having: an association of a device among the fleet of devices with a turbomachine among a fleet of turbomachines, an attachment, an acquisition of at least one turbomachine operating parameter, a development of at least one indicator that allows the update of a digital twin of the turbomachine based on the operating parameter acquired, a communication of the indicator that allows the update of the digital twin to a digital twin storage entity.

PREDICTIVE MAINTENANCE OF AN UNMANNED AERIAL VEHICLE

Methods, systems, apparatuses, and computer program products for predictive maintenance of an unmanned aerial vehicle (UAV) are disclosed. In a particular embodiment, a method of predictive maintenance of a UAV includes a maintenance controller detecting a deviation in an expected behavior of a UAV and determining whether to attribute the deviation to any environmental interferences. In this example embodiment, after determining to not attribute the deviation to any environmental interferences, the maintenance controller schedules the UAV for maintenance.

PREDICTIVE MAINTENANCE OF AN UNMANNED AERIAL VEHICLE

Methods, systems, apparatuses, and computer program products for predictive maintenance of an unmanned aerial vehicle (UAV) are disclosed. In a particular embodiment, a method of predictive maintenance of a UAV includes a maintenance controller detecting a deviation in an expected behavior of a UAV and determining whether to attribute the deviation to any environmental interferences. In this example embodiment, after determining to not attribute the deviation to any environmental interferences, the maintenance controller schedules the UAV for maintenance.

Bond fixture for root end laminate or rotor blade

A bond assembly includes a fixture having a first section movably coupled to a second section. The first section and the second section are disposed opposite one another. A bladder assembly is mounted to at least one of the first section and the second section. The bladder assembly is configured to apply controlled, localized pressure and heat to a component receivable between the first section and the second section.

Bond fixture for root end laminate or rotor blade

A bond assembly includes a fixture having a first section movably coupled to a second section. The first section and the second section are disposed opposite one another. A bladder assembly is mounted to at least one of the first section and the second section. The bladder assembly is configured to apply controlled, localized pressure and heat to a component receivable between the first section and the second section.

Method of repair to compressor housing and repaired housing

A method of repairing a compressor outlet housing includes the steps of obtaining a damaged compressor outlet housing having a radially outer volute, a radially inwardly extending finger extending to an axially extending ledge, a radially inwardly extending web extending radially inwardly from the ledge, and a radially inner bearing support defining a bore. The method identifies a damaged section within at least one of the bearing support, the web, and the ledge, and removes at least the bearing support and the web to leave a remaining part. The method then inserts an insert having at least a replacement bearing support and a replacement web into the remaining part after the removal step. The method then welds the insert to the remaining part to provide a repaired compressor housing. A method of replacing a compressor outlet housing and a replacement compressor outlet housing are also disclosed.

METHOD FOR REPAIRING AN AIR INTAKE LIP
20220371133 · 2022-11-24 ·

A method for repairing a turbomachine air intake lip including a damaged area whose shape differs from the initial shape of the lip, includes identifying the damage; depositing a filler material on the damaged area so as to give it a shape identical to the initial shape; inspecting the shape of the lip; and inspecting the performed repair.