An aircraft including a fuselage with one or more wings extending from the fuselage. The aircraft may include one or more apertures in a surface of at least one of the fuselage and the one or more wings. The one or more apertures may be configured to enable air to pass through the one or more apertures when the aircraft is flying.

An aircraft including a fuselage with one or more wings extending from the fuselage. The aircraft may include one or more apertures in a surface of at least one of the fuselage and the one or more wings. The one or more apertures may be configured to enable air to pass through the one or more apertures when the aircraft is flying.

A method and apparatus for testing a duct leak detection system of an aircraft is disclosed. A sensor of the duct leak detection system is selected at an interface of the duct leak detection system. An alternating current is sent through the selected sensor and a resistance of the selected sensor is measured using the alternating current. An indicative signal is generated at the interface when the measured resistance of the selected sensor is outside of a specification of the selected sensor.

A method for adjusting play in a high-lift system of an aircraft with several flaps, moved by a drive unit with the aid of driving stations connected to a driveshaft, includes disengaging the mechanical connections between the driveshaft and the driving stations in the first position, displacing the individual drive levers by mechanically driving a gear input of the associated rotary actuator such that the individual drive levers come into mechanical contact with a stop in a second position, spaced apart from the first position, and are pretensioned by a certain torque, rotationally fixing the gear inputs of the rotary actuators, adapting the length of connecting links between the respective drive levers and a support arm carrying the associated flap such that a position of the associated flap corresponding to the position of the stop is reached, and reconnecting the driving stations to the driveshaft pretensioned to have no play.

A portable programmable machine enhances efficiency and ergonomics associated with conducting otherwise manual operations within confined spaces. A main body supports a programmable telescoping arm configured to extend through an access port to reach a confined space. The arm includes an articulating wrist for holding and manipulating tools for autonomously processing work parts. The machine can also act semi-autonomously to accommodate interventions of an operator for overriding and fine-tuning interaction of a tool with a work part for proper processing of the part. The arm communicates with a computer in the main body for processing numerical data, and the operator may use a reference camera to fine tune any particular process. The machine incorporates multiple processing functions, for example collar swaging, nut running, cleaning, and/or application of sealants, all through an aircraft wing access port. The main body has lockable wheels for securing the main body near the access port.

A barrel assembly for a composite structure includes a barrel of composite material, a first end ring, and a mid support. The barrel of composite material has a first end, an interior surface and an outer surface, and the first end ring is removably attached to the first end. The first end ring has a perimeter that is substantially congruent with the first end, and is configured to maintain a shape of the barrel. The mid support is removably disposed within the barrel, and has a plurality of spokes extending outwardly from a central hub to contact the interior surface, to maintain a shape of the barrel.

A vehicle body includes a primary vehicle structure and interior vehicle fittings as well as a coupling device for fastening the interior vehicle fittings to the primary vehicle structure. The coupling device is configured to generate a magnetic field, so as to fasten the interior vehicle fittings to the primary vehicle structure without contact. Methods for assembling a vehicle body as well as an edifice are also described.

A vehicle body includes a primary vehicle structure and interior vehicle fittings as well as a coupling device for fastening the interior vehicle fittings to the primary vehicle structure. The coupling device is configured to generate a magnetic field, so as to fasten the interior vehicle fittings to the primary vehicle structure without contact. Methods for assembling a vehicle body as well as an edifice are also described.

A system for monitoring maintenance for manufacturing apparatuses in a facility is provided. The system includes at least one manufacturing apparatus, the manufacturing apparatus including an RF identification tag and a module, and a control system. The control system is configured to receive, from the module, operational status information that indicates time periods during which the manufacturing apparatus is in operation, determine a cumulative time duration of operation for the manufacturing apparatus, retrieve a predetermined maintenance interval for the manufacturing apparatus, determine whether the cumulative time duration of operation exceeds the predetermined maintenance interval, and in response to a determination that the cumulative time duration of operation exceeds the predetermined maintenance interval, i) output a signal that causes the manufacturing apparatus to discontinue operation, and ii) cause instructions for completing a required maintenance procedure to be displayed on a display device in communication with the control system.

A system for monitoring maintenance for manufacturing apparatuses in a facility is provided. The system includes at least one manufacturing apparatus, the manufacturing apparatus including an RF identification tag and a module, and a control system. The control system is configured to receive, from the module, operational status information that indicates time periods during which the manufacturing apparatus is in operation, determine a cumulative time duration of operation for the manufacturing apparatus, retrieve a predetermined maintenance interval for the manufacturing apparatus, determine whether the cumulative time duration of operation exceeds the predetermined maintenance interval, and in response to a determination that the cumulative time duration of operation exceeds the predetermined maintenance interval, i) output a signal that causes the manufacturing apparatus to discontinue operation, and ii) cause instructions for completing a required maintenance procedure to be displayed on a display device in communication with the control system.